EP1844173B1 - Procede de fabrication de toles d'acier austenitique fer-carbone-manganese et toles ainsi produites - Google Patents
Procede de fabrication de toles d'acier austenitique fer-carbone-manganese et toles ainsi produites Download PDFInfo
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- EP1844173B1 EP1844173B1 EP06709055A EP06709055A EP1844173B1 EP 1844173 B1 EP1844173 B1 EP 1844173B1 EP 06709055 A EP06709055 A EP 06709055A EP 06709055 A EP06709055 A EP 06709055A EP 1844173 B1 EP1844173 B1 EP 1844173B1
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- 229910052751 metal Inorganic materials 0.000 title claims abstract description 24
- 239000002184 metal Substances 0.000 title claims abstract description 13
- LAUCTMALVHLLAL-UHFFFAOYSA-N [Mn].[C].[Fe] Chemical compound [Mn].[C].[Fe] LAUCTMALVHLLAL-UHFFFAOYSA-N 0.000 title claims abstract description 8
- 238000004519 manufacturing process Methods 0.000 title claims description 18
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 72
- 239000010959 steel Substances 0.000 claims abstract description 72
- 229910052720 vanadium Inorganic materials 0.000 claims abstract description 38
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims abstract description 36
- 239000010955 niobium Substances 0.000 claims abstract description 35
- 239000010936 titanium Substances 0.000 claims abstract description 35
- 239000011651 chromium Substances 0.000 claims abstract description 34
- 239000000203 mixture Substances 0.000 claims abstract description 34
- 239000011572 manganese Substances 0.000 claims abstract description 23
- 150000001247 metal acetylides Chemical class 0.000 claims abstract description 22
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 18
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 17
- 229910052758 niobium Inorganic materials 0.000 claims abstract description 17
- 150000004767 nitrides Chemical class 0.000 claims abstract description 17
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims abstract description 16
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims abstract description 16
- 229910052750 molybdenum Inorganic materials 0.000 claims abstract description 16
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims abstract description 16
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 15
- 239000011733 molybdenum Substances 0.000 claims abstract description 14
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims abstract description 13
- 239000010949 copper Substances 0.000 claims abstract description 12
- 229910052742 iron Inorganic materials 0.000 claims abstract description 10
- 239000000126 substance Substances 0.000 claims abstract description 9
- 239000012535 impurity Substances 0.000 claims abstract description 7
- 238000003723 Smelting Methods 0.000 claims abstract 3
- 239000002244 precipitate Substances 0.000 claims description 63
- 238000000137 annealing Methods 0.000 claims description 27
- 238000010438 heat treatment Methods 0.000 claims description 20
- 229910052757 nitrogen Inorganic materials 0.000 claims description 12
- 239000011265 semifinished product Substances 0.000 claims description 12
- 229910052782 aluminium Inorganic materials 0.000 claims description 11
- 238000000034 method Methods 0.000 claims description 11
- 230000008569 process Effects 0.000 claims description 10
- 229910052802 copper Inorganic materials 0.000 claims description 9
- 229910052759 nickel Inorganic materials 0.000 claims description 9
- 238000005096 rolling process Methods 0.000 claims description 9
- 229910052799 carbon Inorganic materials 0.000 claims description 7
- 238000001816 cooling Methods 0.000 claims description 7
- 230000009467 reduction Effects 0.000 claims description 7
- 229910052710 silicon Inorganic materials 0.000 claims description 7
- 229910052717 sulfur Inorganic materials 0.000 claims description 7
- 229910052698 phosphorus Inorganic materials 0.000 claims description 6
- 230000003014 reinforcing effect Effects 0.000 claims description 4
- 229910000617 Mangalloy Inorganic materials 0.000 claims description 3
- 238000001556 precipitation Methods 0.000 description 31
- 239000012071 phase Substances 0.000 description 19
- 230000003111 delayed effect Effects 0.000 description 18
- 229910052739 hydrogen Inorganic materials 0.000 description 16
- 239000001257 hydrogen Substances 0.000 description 16
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 14
- 238000005336 cracking Methods 0.000 description 14
- 229910052748 manganese Inorganic materials 0.000 description 13
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 12
- 238000005266 casting Methods 0.000 description 12
- 239000000047 product Substances 0.000 description 12
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 11
- 238000005097 cold rolling Methods 0.000 description 10
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 10
- 238000001953 recrystallisation Methods 0.000 description 10
- 238000007792 addition Methods 0.000 description 9
- 230000035945 sensitivity Effects 0.000 description 8
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 6
- -1 aluminum nitrides Chemical class 0.000 description 6
- 238000005098 hot rolling Methods 0.000 description 6
- 239000011159 matrix material Substances 0.000 description 6
- 229910052775 Thulium Inorganic materials 0.000 description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 4
- 230000015572 biosynthetic process Effects 0.000 description 4
- 230000007423 decrease Effects 0.000 description 4
- 238000009826 distribution Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 238000004804 winding Methods 0.000 description 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 3
- 239000010960 cold rolled steel Substances 0.000 description 3
- 230000007547 defect Effects 0.000 description 3
- 238000007872 degassing Methods 0.000 description 3
- 238000009792 diffusion process Methods 0.000 description 3
- 238000012360 testing method Methods 0.000 description 3
- 238000011282 treatment Methods 0.000 description 3
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 229910052796 boron Inorganic materials 0.000 description 2
- 229910001567 cementite Inorganic materials 0.000 description 2
- 230000006866 deterioration Effects 0.000 description 2
- 238000000605 extraction Methods 0.000 description 2
- 150000002431 hydrogen Chemical class 0.000 description 2
- KSOKAHYVTMZFBJ-UHFFFAOYSA-N iron;methane Chemical compound C.[Fe].[Fe].[Fe] KSOKAHYVTMZFBJ-UHFFFAOYSA-N 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 229910000734 martensite Inorganic materials 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 238000007493 shaping process Methods 0.000 description 2
- 238000005482 strain hardening Methods 0.000 description 2
- 238000004627 transmission electron microscopy Methods 0.000 description 2
- YZCKVEUIGOORGS-UHFFFAOYSA-N Hydrogen atom Chemical compound [H] YZCKVEUIGOORGS-UHFFFAOYSA-N 0.000 description 1
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- 238000009825 accumulation Methods 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 238000009749 continuous casting Methods 0.000 description 1
- 230000002542 deteriorative effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000005530 etching Methods 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 238000003475 lamination Methods 0.000 description 1
- 238000011418 maintenance treatment Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- ZLANVVMKMCTKMT-UHFFFAOYSA-N methanidylidynevanadium(1+) Chemical class [V+]#[C-] ZLANVVMKMCTKMT-UHFFFAOYSA-N 0.000 description 1
- QMQXDJATSGGYDR-UHFFFAOYSA-N methylidyneiron Chemical compound [C].[Fe] QMQXDJATSGGYDR-UHFFFAOYSA-N 0.000 description 1
- 230000005012 migration Effects 0.000 description 1
- 238000013508 migration Methods 0.000 description 1
- 239000002105 nanoparticle Substances 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 230000001376 precipitating effect Effects 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000003763 resistance to breakage Effects 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 230000002000 scavenging effect Effects 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000007790 solid phase Substances 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 239000011593 sulfur Substances 0.000 description 1
- 230000009747 swallowing Effects 0.000 description 1
- 238000007669 thermal treatment Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
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
- C21D6/00—Heat treatment of ferrous alloys
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- 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
- 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
-
- 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
- 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
Definitions
- the invention relates to the manufacture of hot and cold rolled sheets of austenitic iron-carbon-manganese steels having very high mechanical characteristics, and in particular a high mechanical strength combined with an excellent resistance to delayed cracking.
- the patent FR 2 829 775 discloses, for example, austenitic alloys having as main elements: iron-carbon (up to 2%) manganese (between 10 and 40%) capable of being hot-rolled or cold-rolled, exhibiting a resistance that may exceed 1200 MPa.
- the deformation mode of these steels depends only on the stacking fault energy: for a sufficiently high stacking fault energy, a mechanical deformation mode is observed by twinning, which makes it possible to obtain a large capacitance. hardening.
- the twins participate in increasing the flow limit.
- the stacking fault energy exceeds a certain threshold, the sliding of the perfect dislocations becomes the dominant deformation mechanism and the work hardening capacity is less.
- the aforementioned patent therefore discloses Fe-C-Mn steel grades whose stacking failure energy is such that a high work-hardening is observed, combined with a very high mechanical strength.
- the object of the invention is therefore to provide a hot-rolled or cold-rolled steel sheet or product of economical manufacture, having a resistance greater than 900 MPa, an elongation at break greater than 50%, particularly suitable for cold forming and having a very high resistance to delayed cracking, without the particular need for a specific heat treatment for degassing.
- the subject of the invention is an austenitic iron-carbon-manganese steel sheet, the chemical composition of which comprises the contents being expressed by weight: 0.45% ⁇ C ⁇ 0.75%, 15% ⁇ Mn ⁇ 26%, Si ⁇ 3%, Al ⁇ 0.050%, S ⁇ 0.030%, P ⁇ 0.080%, N ⁇ 0.1% at least one metal element selected from vanadium, titanium, niobium, chromium, molybdenum: 0.050% ⁇ V ⁇ 0.50%, 0.040% ⁇ Ti ⁇ 0.50%, 0.070% ⁇ Nb ⁇ 0, 50%, 0.070% ⁇ Cr ⁇ 2%, 0.14% ⁇ Mo ⁇ 2% and optionally one or more elements selected from 0.0005% ⁇ B ⁇ 0.003%, Ni ⁇ 1%, Cu ⁇ 5%, the remainder of the composition consisting of iron and unavoidable impurities resulting from the preparation, the quantity of metal elements in the form of carbides, nitri
- the composition of the steel comprises: 0.50% ⁇ C ⁇ 0.70% According to a preferred embodiment, the composition of the steel comprises: 17% ⁇ Mn ⁇ 24%
- the composition of the steel comprises 0.070% ⁇ V ⁇ 0.40%, the amount of vanadium in the form of carbides, nitrides or carbonitrides precipitated being 0.070% ⁇ V p ⁇ 0.140%
- the composition of the steel comprises 0.060% ⁇ Ti ⁇ 0.40%, the amount of titanium in the form of carbides, nitrides or carbonitrides precipitated being: 0.060% ⁇ Ti p ⁇ 0.110%
- composition of the steel advantageously comprises 0.090% ⁇ Nb ⁇ 0.40%, the amount of niobium in the form of carbides, nitrides or carbonitrides precipitated being: 0.090% ⁇ Nb p ⁇ 0.200%
- the composition of the steel comprises 0.20% ⁇ Cr ⁇ 1.8%, the amount of chromium in the form of precipitated carbides being 0.20% ⁇ Cr p ⁇ 0.5%
- the composition of the steel comprises 0.20% ⁇ Mo ⁇ 1.8%, the quantity in molybdenum in the form of precipitated carbides being 0.20% ⁇ Mo p ⁇ 0.35%
- the average size of the precipitates is between 5 and 25 nanometers, and more preferably between 7 and 20 nanometers
- at least 75% of the population of said precipitates is located in intragranular position.
- the invention also relates to a method of manufacturing a sheet metal cold-rolled austenitic iron-carbon-manganese steel according to which is supplied a steel whose chemical composition comprises, the contents being expressed by weight:
- the parameters Vc, Tm, tm, Vr, Tu, t u are adjusted so that the average size of the carbide, nitride or carbonitride precipitates after the annealing is between 5 and 25 nanometers, and preferentially between 7 and 20 nanometers.
- Vc, Tm, tm, Vr, Tu, t u are advantageously adjusted such that at least 75% of the population of the precipitates after the annealing is located in the intragranular position.
- a steel whose chemical composition comprises 0.050% ⁇ V ⁇ 0.50% is supplied with heat, the semi-finished product is heated to a rolling end temperature of greater than or equal to 950.degree. the sheet is reeled at a temperature below 500 ° C., the sheet is cold-rolled with a reduction ratio greater than 30%, an annealing heat treatment is carried out with a heating rate Vc of between 2 and 10 ° C / s, at a temperature Tm between 700 and 870 ° C for a time between 30 and 180 s, and the sheet is cooled at a speed between 10 and 50 ° C / s.
- the heating rate Vc is preferably between 3 and 7 ° C./s.
- the holding temperature Tm is between 720 and 850 ° C.
- the casting of the semi-finished product is advantageously carried out in the form of casting slabs or thin strips between counter-rotating steel rolls.
- the invention also relates to the use of an austenitic steel sheet described above or manufactured by a method described above, for the manufacture of structural parts, reinforcing elements or external parts. , in the automotive field.
- carbon plays a very important role in the formation of the microstructure and the mechanical properties: it increases the stacking fault energy and promotes the stability of the austenitic phase. In combination with a manganese content ranging from 15 to 26% by weight, this stability is obtained for a carbon content greater than or equal to 0.45%. However, for a carbon content greater than 0.75%, it becomes difficult to avoid excessive precipitation of carbides during certain thermal cycles during industrial manufacture, a precipitation which degrades the ductility.
- the carbon content is between 0.50 and 0.70% by weight so as to obtain sufficient strength combined with optimum precipitation of carbides or carbonitrides.
- the manganese content is between 17 and 24% so as to optimize the stacking fault energy and to avoid the formation of martensite under the effect of a deformation. Moreover, when the manganese content is greater than 24%, the mode of deformation by twinning is less favored compared to the sliding mode of perfect dislocations.
- Aluminum is a very effective element for the deoxidation of steel. Like carbon, it increases the stacking fault energy. However, its excessive presence in steels with a high manganese content has a disadvantage: in fact, manganese increases the solubility of nitrogen in the liquid iron. If too much aluminum is present in the steel, the nitrogen combining with the aluminum precipitates in the form of aluminum nitrides hindering the migration of the grain boundaries during the hot transformation and increases very significantly the risk of occurrence of cracks in continuous casting. In addition, as will be explained later, a sufficient amount of nitrogen must be available to form fine carbo-nitride precipitates for the most part. An Al content less than or equal to 0.050% avoids precipitation of AlN and maintains a sufficient nitrogen content for the precipitation of the elements mentioned below.
- the nitrogen content must be less than or equal to 0.1% in order to prevent this precipitation and the formation of volume defects (blowholes) during solidification.
- the nitrogen content in the presence of elements capable of precipitating in the form of nitrides, such as vanadium, niobium or titanium, the nitrogen content must not exceed 0.1% otherwise the risk of obtaining an ineffective coarse precipitation will be observed. with respect to the trapping of hydrogen.
- Silicon is also an effective element for deoxidizing steel as well as for hardening in the solid phase. However, beyond a content of 3%, it decreases the elongation, tends to form undesirable oxides during certain assembly processes and must therefore be kept below this limit.
- Sulfur and phosphorus are impurities that weaken the grain boundaries. Their respective content must be less than or equal to 0.030 and 0.080% in order to maintain sufficient hot ductility.
- boron may be added in an amount of from 0.0005 to 0.003%. This element segregates at the austenitic grain boundaries and reinforces their cohesion. Below 0.0005%, this effect is not obtained. Above 0.003%, boron precipitates as borocarbons, and the effect is saturated.
- Nickel can be used as an option to increase the strength of the steel by hardening in solid solution. Nickel contributes to a high elongation break and increases in particular the toughness. However, it is also desirable for cost issues to limit the nickel content to a maximum content of less than or equal to 1%.
- addition of copper to a content of less than or equal to 5% is a means of hardening the steel by precipitation of metallic copper. However, beyond this content, copper is responsible for the appearance of surface defects hot sheet.
- the metal elements capable of forming precipitates such as vanadium, titanium, niobium, chromium, molybdenum, play an important role in the context of the invention.
- delayed cracking is caused by an excessive local concentration of hydrogen, in particular at the austenitic grain boundaries.
- the inventors have demonstrated that certain types of precipitates, the nature, quantity, size and distribution of which are precisely defined according to the invention, significantly reduce the sensitivity to delayed cracking, and this without reducing the properties ductility and tenacity.
- the inventors firstly demonstrated that carbides, nitrides or carbonitrides precipitated from vanadium, titanium or niobium, were very effective as hydrogen traps. Chromium carbides or molybdenum carbides can also play this role. At room temperature, the hydrogen is then irreversibly trapped at the interface between these precipitates and the matrix. It is however necessary, in order to ensure the trapping of the residual hydrogen which could be encountered under certain industrial conditions, that the quantity of metal elements in the form of precipitates is greater than or equal to a critical content, depending on the nature of the precipitates.
- the quantity of metal elements in the form of precipitates of carbides, nitrides, or carbonitrides is designated by V p , Ti p , Nb p , respectively for vanadium, titanium and niobium, and Cr p , Mo p for chromium and molybdenum carbides.
- the minimum value expressed for these various elements corresponds to a quantity of addition necessary to form precipitates taking into account the thermal cycles of manufacture.
- a preferred minimum content (for example 0.070% for vanadium) is recommended, so as to obtain a larger quantity of precipitates.
- the maximum value expressed for these various elements corresponds to excessive precipitation, or in an inappropriate form, deteriorating the mechanical properties, or to an uneconomic implementation of the invention.
- a preferred maximum content (for example of 0.40% for vanadium) is recommended, so as to optimize the addition of the element.
- the minimum value of metallic elements in the form of precipitates corresponds to a quantity of precipitates for very effectively reducing the sensitivity to delayed cracking.
- a preferred minimum amount (for example 0.070% in the case of vanadium) is recommended, so as to obtain a particularly high resistance to delayed cracking.
- the maximum value of metallic elements in the form of precipitates marks a deterioration of the ductility or the tenacity, the rupture starting on the precipitates. Moreover, beyond this maximum value, intense precipitation occurs, which can prevent total recrystallization during thermal treatments of continuous annealing after cold rolling.
- a preferred maximum content in the form of precipitates (for example 0.140% for vanadium) is recommended, so that the ductility is preserved as much as possible and that the precipitation obtained is compatible with the recrystallization under the usual annealing conditions. recrystallization.
- mean size of precipitates is the size that can be measured, for example, from replicates with extraction, followed by observations by transmission electron microscopy: the diameter is measured (in the case of spherical or quasi-spherical precipitates) or the largest length (in the case of irregularly shaped precipitates) of each precipitate, then establishes a histogram of size distribution of these precipitates, the average of which is calculated from the count of a statistically representative number of particles. Beyond an average size of 25 nanometers, the efficiency of hydrogen scavenging decreases due to the decrease in the interface between precipitates and matrix.
- an average size of precipitates exceeding 25 nanometers also decreases the density of precipitates present, thereby excessively increasing the inter-site trapping distance.
- the trapping interfacial surface for hydrogen is also reduced.
- the average size of precipitates is less than 20 nanometers in order to trap the largest amount of hydrogen possible.
- the precipitates are advantageously located in the intragranular position in order to reduce the sensitivity to delayed cracking: in fact, when at least 75% of the population of precipitates is located in the intragranular position, the distribution of hydrogen possibly present is more homogeneous, without accumulation at the austenitic grain boundaries which are potential sites of embrittlement.
- the addition of one of the aforementioned elements, in particular chromium, makes it possible to obtain a precipitation of various carbides such as MC, M 7 C 3 , M 23 C 6 , M 3 C where M denotes not only the metallic element but also Fe or Mn, elements present in the matrix.
- M denotes not only the metallic element but also Fe or Mn, elements present in the matrix.
- the presence of iron and manganese within the precipitates makes it possible to increase the quantity of precipitates at a lower cost, thus reinforcing the efficiency of the precipitation.
- the object of the invention is to simultaneously dispose of steels with very high mechanical characteristics and insensitive to delayed fracture.
- the steel should be completely recrystallized after the annealing cycle. Too early precipitation, for example at the stage of casting, hot rolling or winding, will be a potential brake on recrystallization and may harden the metal and increase the hot or cold rolling forces. It will also be less effective because it will intervene significantly on the austenitic grain boundaries. The size of these precipitates formed at high temperature will be larger, often greater than 25 nanometers.
- vanadium additions are particularly desirable insofar as the precipitation of this element hardly occurs during hot rolling or winding.
- the precipitation takes place in the form of VC and in the form of nanometric VN or V (CN) homogeneously distributed, the vast majority of the precipitates being located in the intragranular position, ie in the most desirable form for the entrapment of the nanoparticles. 'hydrogen.
- this fine precipitation limits the growth of the grain, a finer austenitic grain size can thus be obtained after annealing.
- a steel is produced whose composition comprises: 0.45% ⁇ C ⁇ 0.75% 15% ⁇ Mn ⁇ 26%, Si ⁇ 3%, Al ⁇ 0.050%, S ⁇ 0.030, P ⁇ 0.080%, N ⁇ 0.1%, one or more elements selected from 0.050% ⁇ V ⁇ 0.50%, 0.040% ⁇ Ti ⁇ 0.50%, 0.070% ⁇ Nb ⁇ 0.50%, 0.070% ⁇ Cr ⁇ 2%, 0.14% ⁇ Mo ⁇ 2%, and optionally one or more elements selected from 0.0005% ⁇ B ⁇ 0.003%, Ni ⁇ 1%, Cu ⁇ 5%, the rest being iron and unavoidable impurities from the elaboration.
- This development can be followed by casting in ingots, or continuously in the form of slabs of thickness of the order of 200 mm. It is also possible to advantageously perform the casting in the form of thin slabs, a few tens of millimeters thick, or thin strips of a few millimeters.
- certain addition elements according to the invention such as titanium or niobium are present, the casting in the form of thin products will lead more particularly to a precipitation of nitrides or very thin and thermally stable carbonitrides, the presence of which reduces sensitivity to delayed cracking.
- These cast half-products are first brought to a temperature of between 1100 and 1300 ° C. This is intended to achieve in all points temperature areas favorable to high deformations that will undergo the steel during rolling.
- the reheat temperature must not be higher than 1300 ° C, otherwise it will be too close to the solidus temperature that could be reached in any zones enriched locally with manganese and / or carbon and cause a passage local by a liquid state that would be harmful for hot shaping.
- the hot rolling step of these semi-products starting between 1300 and 1000 ° C can be done directly after casting without going through the intermediate heating step.
- the semi-finished product is hot-rolled, for example to obtain a thickness of hot rolled strip 2 to 5 millimeters thick, or even 1 to 5 mm in the case of semi-finished product from a thin slab casting. , or 0.5 to 3 mm in the case of a casting of thin strips.
- the low aluminum content of the steel according to the invention makes it possible to avoid excessive precipitation of AlN which would adversely affect the hot deformability during rolling.
- the end-of-lamination temperature In order to avoid any problem of cracking due to lack of ductility, the end-of-lamination temperature must be greater than or equal to 890 ° C.
- the strip After rolling, the strip must be wound at a temperature such that a precipitation of carbides, essentially intergranular cementite (Fe, Mn) 3 C), does not take place significantly, which would lead to a reduction of certain mechanical properties. This is achieved when the winding temperature is below 580 ° C.
- the conditions of elaboration will also be chosen so that the product obtained is completely recrystallized.
- the product Before the optional phase of keeping the temperature Tu, the product can be optionally cooled to room temperature. This phase of maintaining the temperature You can possibly be carried out within a separate device, for example a furnace for the static annealing of steel coils.
- Vc, Tm, tm, Vr, Tu, t u is usually carried out in such a way that the desired mechanical properties are obtained, in particular thanks to a complete recrystallization.
- the person skilled in the art will adjust in particular according to the cold rolling ratio, these so that the amount of metal elements (V, Ti, Nb, Cr, Mo) present in the form of carbides, nitrides or carbonitrides precipitated after annealing is included within the contents mentioned above ((V p , Ti p , Nb p , Cr p , Mo p )
- a composition steel will be produced: 0.45% ⁇ C ⁇ 0.75%, 15% ⁇ Mn ⁇ 26%, Si ⁇ 3%, Al ⁇ 0.050%, S ⁇ 0.030%, P 0,0 0.080%, N ⁇ 0.1%, 0.050% ⁇ V ⁇ 0.50%, and optionally one or more elements selected from 0.0005% ⁇ B ⁇ 0.003%, Ni ⁇ 1%, Cu ⁇ 5%, optimally a steel sheet according to the invention by casting a half-product, bringing it to a temperature of between 1100 and 1300 ° C, by hot rolling this half-product to a temperature of end of rolling greater than or equal to 950 ° C and then winding at a temperature below 500 ° C.
- the sheet is cold rolled with a reduction rate greater than 30% (the reduction ratio being defined by: (thickness of the sheet before cold rolling - thickness of the sheet after cold rolling) / (thickness of the front plate
- the rate of 30% corresponds to a minimum deformation so as to obtain a recrystallization.
- An annealing heat treatment is then carried out with a heating rate Vc of between 2 and 10 ° C./s (preferably between 3 and 7 ° C.). ° C / s), at a temperature Tm between 700 and 870 ° C (preferably between 720 and 850 ° C) for a time between 30 and 180s and the sheet will be cooled at a speed between 10 and 50 ° C / s
- compositions expressed as a weight percentage in addition to the steels I1 and I2 according to the invention, the composition of reference steels was indicated by way of comparison:
- R1 steel has a very low vanadium content
- Table 1 Composition of steels Steel VS mn Yes S P al Cu Or NOT B V 11 0,635 21.79 0.01 0,003 0,007 0.005 ⁇ 0.002 ⁇ 0.01 0,003 ⁇ 0.0005 0,160 12 0.595 21,80 0,200 0.006 0,007 0,004 ⁇ 0.002 ⁇ 0.01 0,003 0.0023 0,225 R1 0,600 21.84 0.198 0,007 0.006 0.005 ⁇ 0.002 ⁇ 0.01 0,003 ⁇ 0.0005 0,013 R2 0.625 21.65 0.01 0,003 0,007 0.005 ⁇ 0.002 ⁇ 0.01 0,003 ⁇ 0.0005 0.405 R3 0.625 21.64 0.01 0,003 0,007 0.005 ⁇ 0.002 ⁇ 0.01 0,003 ⁇ 0.0005 0.865 I1-2: according to the invention.
- R1-3 Reference
- Semi-finished products of these steels were heated to 1180 ° C, hot rolled to a temperature of 950 ° C to bring them to a thickness of 3 mm and then wound at a temperature of 500 ° C.
- the steel sheets thus obtained were then cold-rolled with a reduction rate of 50% to a thickness of 1.5 mm, and then annealed under the conditions presented in Table 2.
- Table 3 shows the mechanical tensile properties: strength and elongation at break, obtained under these conditions.
- circular blanks with a diameter of 55 mm were cut in the cold-rolled and annealed sheets. These blanks were then embossed by swallowing in the form of flat-bottomed cups (swift shrinkage tests) using a 33mm diameter punch.
- the factor ⁇ characterizing the severity of the test is 1.66.
- the possible presence of micro-cracks was then noted either immediately after shaping, or after a waiting period of 3 months, thus characterizing a possible sensitivity to delayed cracking. The results of these observations were also reported in Table 3.
- Table 3 Mechanical tensile characteristics obtained on cold-rolled and annealed sheets, and characteristics of drawability and sensitivity to delayed cracking Steel Strength (MPa) Elongation at break (%) observed after stamping Cracks observed after a waiting time of 3 months I1 1071 55 No No I2 1090 58 No No R1 1074 63 No Yes R2 1168 35 No No R3 1417 28 nd nd nd: not determined
- the steels I1 and I2 according to the invention comprise precipitates of suitable size and nature. These are located at more than 75% in intragranular position. These steels combine excellent mechanical characteristics (resistance greater than 1000 MPa, elongation greater than 55% and a high resistance to delayed fracture. This last property is obtained even without specific heat treatment of degassing.
- the hot-rolled or cold-rolled sheets according to the invention are advantageously used in the automobile industry in the form of structural parts, reinforcing elements or external parts which, because of their very high strength and their high ductility, contribute to a very effective reduction of vehicle weight while increasing safety in case of impact.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Physics & Mathematics (AREA)
- Heat Treatment Of Sheet Steel (AREA)
- Heat Treatment Of Steel (AREA)
- Battery Electrode And Active Subsutance (AREA)
- Treatment Of Steel In Its Molten State (AREA)
- Heat Treatment Of Strip Materials And Filament Materials (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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PL06709055T PL1844173T3 (pl) | 2005-01-21 | 2006-01-10 | Sposób wytwarzania blach ze stali austenicznej żelazo-węgiel-mangan, oraz blachy wytwarzane tym sposobem |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0500637A FR2881144B1 (fr) | 2005-01-21 | 2005-01-21 | Procede de fabrication de toles d'acier austenitique fer-carbone-manganese a haute resistance a la fissuration differee, et toles ainsi produites |
PCT/FR2006/000043 WO2006077301A1 (fr) | 2005-01-21 | 2006-01-10 | Procede de fabrication de toles d'acier austenitique fer-carbone-manganese et toles ainsi produites |
Publications (2)
Publication Number | Publication Date |
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EP1844173A1 EP1844173A1 (fr) | 2007-10-17 |
EP1844173B1 true EP1844173B1 (fr) | 2009-03-11 |
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EP06709055A Active EP1844173B1 (fr) | 2005-01-21 | 2006-01-10 | Procede de fabrication de toles d'acier austenitique fer-carbone-manganese et toles ainsi produites |
Country Status (17)
Country | Link |
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US (1) | US7799148B2 (ja) |
EP (1) | EP1844173B1 (ja) |
JP (1) | JP5111119B2 (ja) |
KR (1) | KR100938790B1 (ja) |
CN (1) | CN101107377B (ja) |
AT (1) | ATE425274T1 (ja) |
BR (1) | BRPI0606487A2 (ja) |
CA (1) | CA2595609C (ja) |
DE (1) | DE602006005614D1 (ja) |
ES (1) | ES2321974T3 (ja) |
FR (1) | FR2881144B1 (ja) |
MX (1) | MX2007008726A (ja) |
PL (1) | PL1844173T3 (ja) |
RU (1) | RU2361931C2 (ja) |
UA (1) | UA84377C2 (ja) |
WO (1) | WO2006077301A1 (ja) |
ZA (1) | ZA200705233B (ja) |
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DE102010034161B4 (de) * | 2010-03-16 | 2014-01-02 | Salzgitter Flachstahl Gmbh | Verfahren zur Herstellung von Werkstücken aus Leichtbaustahl mit über die Wanddicke einstellbaren Werkstoffeigenschaften |
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DE102016121902A1 (de) * | 2016-11-15 | 2018-05-17 | Salzgitter Flachstahl Gmbh | Verfahren zur Herstellung von Fahrwerksteilen aus mikrolegiertem Stahl mit verbesserter Kaltumformbarkeit |
TWI630277B (zh) * | 2016-12-19 | 2018-07-21 | 杰富意鋼鐵股份有限公司 | High manganese steel plate and manufacturing method thereof |
KR101889185B1 (ko) * | 2016-12-21 | 2018-08-16 | 주식회사 포스코 | 성형성 및 피로특성이 우수한 열연강판 및 그 제조방법 |
CN109487178B (zh) * | 2018-12-29 | 2020-06-16 | 广西长城机械股份有限公司 | 高纯净超高锰钢及其制备工艺 |
JP7380655B2 (ja) * | 2020-08-07 | 2023-11-15 | Jfeスチール株式会社 | 鋼材およびその製造方法 |
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FR2796083B1 (fr) * | 1999-07-07 | 2001-08-31 | Usinor | Procede de fabrication de bandes en alliage fer-carbone-manganese, et bandes ainsi produites |
FR2829775B1 (fr) * | 2001-09-20 | 2003-12-26 | Usinor | Procede de fabrication de tubes roules et soudes comportant une etape finale d'etirage ou d'hydroformage et tube soude ainsi obtenu |
JP4718782B2 (ja) * | 2003-02-06 | 2011-07-06 | 新日本製鐵株式会社 | 合金化溶融亜鉛めっき鋼板、およびその製造方法 |
FR2857980B1 (fr) * | 2003-07-22 | 2006-01-13 | Usinor | Procede de fabrication de toles d'acier austenitique fer-carbone-manganese, a haute resistance, excellente tenacite et aptitude a la mise en forme a froid, et toles ainsi produites |
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2005
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- 2006-01-10 KR KR1020077016758A patent/KR100938790B1/ko active IP Right Grant
- 2006-01-10 PL PL06709055T patent/PL1844173T3/pl unknown
- 2006-01-10 EP EP06709055A patent/EP1844173B1/fr active Active
- 2006-01-10 US US11/814,329 patent/US7799148B2/en active Active
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- 2006-01-10 MX MX2007008726A patent/MX2007008726A/es active IP Right Grant
- 2006-01-10 DE DE602006005614T patent/DE602006005614D1/de active Active
- 2006-01-10 AT AT06709055T patent/ATE425274T1/de active
- 2006-01-10 CA CA2595609A patent/CA2595609C/fr active Active
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- 2006-01-10 WO PCT/FR2006/000043 patent/WO2006077301A1/fr active Application Filing
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Also Published As
Publication number | Publication date |
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RU2007131590A (ru) | 2009-02-27 |
KR20070094801A (ko) | 2007-09-21 |
US7799148B2 (en) | 2010-09-21 |
ATE425274T1 (de) | 2009-03-15 |
EP1844173A1 (fr) | 2007-10-17 |
ZA200705233B (en) | 2008-06-25 |
CN101107377B (zh) | 2011-03-23 |
RU2361931C2 (ru) | 2009-07-20 |
CA2595609A1 (fr) | 2006-07-27 |
JP5111119B2 (ja) | 2012-12-26 |
JP2008528796A (ja) | 2008-07-31 |
CA2595609C (fr) | 2011-04-12 |
BRPI0606487A2 (pt) | 2009-06-30 |
UA84377C2 (ru) | 2008-10-10 |
US20080035249A1 (en) | 2008-02-14 |
DE602006005614D1 (de) | 2009-04-23 |
MX2007008726A (es) | 2008-03-04 |
FR2881144B1 (fr) | 2007-04-06 |
ES2321974T3 (es) | 2009-06-15 |
PL1844173T3 (pl) | 2009-08-31 |
FR2881144A1 (fr) | 2006-07-28 |
CN101107377A (zh) | 2008-01-16 |
KR100938790B1 (ko) | 2010-01-27 |
WO2006077301A1 (fr) | 2006-07-27 |
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