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EP3274483A1 - Parts with a bainitic structure having high strength properties and manufacturing process - Google Patents

Parts with a bainitic structure having high strength properties and manufacturing process

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Publication number
EP3274483A1
EP3274483A1 EP16718723.6A EP16718723A EP3274483A1 EP 3274483 A1 EP3274483 A1 EP 3274483A1 EP 16718723 A EP16718723 A EP 16718723A EP 3274483 A1 EP3274483 A1 EP 3274483A1
Authority
EP
European Patent Office
Prior art keywords
content
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weight
percentage
part according
Prior art date
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Granted
Application number
EP16718723.6A
Other languages
German (de)
French (fr)
Other versions
EP3274483B1 (en
Inventor
Marie-Thérèse PERROT-SIMONETTA
Bernard Resiak
Ulrich Voll
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ArcelorMittal SA
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ArcelorMittal SA
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Priority to PL16718723T priority Critical patent/PL3274483T3/en
Publication of EP3274483A1 publication Critical patent/EP3274483A1/en
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    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/52Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for wires; for strips ; for rods of unlimited length
    • C21D9/525Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for wires; for strips ; for rods of unlimited length for wire, for rods
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    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/18Hardening; Quenching with or without subsequent tempering
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    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/004Heat treatment of ferrous alloys containing Cr and Ni
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    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/005Heat treatment of ferrous alloys containing Mn
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    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/008Heat treatment of ferrous alloys containing Si
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    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
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    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0247Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
    • C21D8/0263Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment following hot rolling
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    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/06Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of rods or wires
    • C21D8/065Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of rods or wires of ferrous alloys
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
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    • C22C38/001Ferrous alloys, e.g. steel alloys containing N
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    • C22C38/002Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
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    • C22C38/28Ferrous alloys, e.g. steel alloys containing chromium with titanium or zirconium
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    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/38Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of manganese
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    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/42Ferrous alloys, e.g. steel alloys containing chromium with nickel with copper
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    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/44Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
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    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/46Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
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    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/48Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum
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    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/50Ferrous alloys, e.g. steel alloys containing chromium with nickel with titanium or zirconium
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    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/54Ferrous alloys, e.g. steel alloys containing chromium with nickel with boron
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    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/58Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
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    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/60Ferrous alloys, e.g. steel alloys containing lead, selenium, tellurium, or antimony, or more than 0.04% by weight of sulfur
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    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/001Austenite
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    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/002Bainite
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    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/005Ferrite

Definitions

  • the present invention covers a parts manufacturing high strength properties while being machineable, obtained from steels simultaneously having good hot ductility for performing hot forming operations and such that n hardenability It is not useful to perform tempering and tempering operations to obtain the advertised properties.
  • the invention relates more precisely to parts having, whatever the shape and complexity of the part, a mechanical strength greater than or equal to 1100 MPa, having a yield strength greater than or equal to 700 MPa, an elongation at break A greater than or equal to 12 and a necking with Z-breaking greater than 30%,
  • each part, bar, any form, wire or complex piece obtained by hot forming process is defined as, for example, rolling, or forging with or without subsequent partial or total reheating operations. , thermal or thermochemical treatment and / or shaping with or without removal of material, or even with addition of material as for welding.
  • hot forming of a steel is meant any process that modifies the primary form of a product by an operation which is carried out at a temperature of the material such that the crystalline structure of the steel is predominantly austenitic.
  • EP0787812 describes a process for the manufacture of forged parts whose chemical composition comprises, by weight: 0.1% ⁇ C ⁇ 0.4%; 1% ⁇ Mn ⁇ 1, 8%; 1, 2% ⁇ Si ⁇ 1, 7%; 0% ⁇ Ni ⁇ 1%; 0% ⁇ Cr ⁇ 1, 2%; 0% ⁇ Mo ⁇ 0.3%; 0% ⁇ V ⁇ 0.3%; Cu ⁇ 0.35% optionally from 0.005% to 0.06% aluminum, optionally boron in contents of between 0.0005% and 0.01%, optionally between 0.005% and 0.03% titanium, optionally between 0.005 % and 0.06% of niobium, optionally from 0.005% to 0.1% of sulfur, optionally up to 0.006% of calcium, optionally up to 0.03% of tellurium, optionally up to 0.05% of selenium, optionally up to 0.05% bismuth, optionally up to 0.1% lead, the balance being iron and impurities resulting from the preparation.
  • This method involves subjecting the workpiece to a heat treatment having a cooling from a temperature at which the steel is fully austenitic to a temperature Tm of between Ms + 100 D ° C and Ms-20 ° C at a temperature of cooling rate Vr greater than 0.5 ° C / s, followed by holding the workpiece between Tm and Tf, with Tf> Tm-100 ° C, and preferably Tf> Tm-60 ° C, for at least 2 minutes to obtain a structure comprising at least 15%, and preferably at least 30% of bainite formed between Tm and Tf.
  • This technique requires many process steps that are detrimental to productivity.
  • the object of the present invention is to solve the problems mentioned above. It aims to provide a steel for hot formed parts with high strength properties, simultaneously having a mechanical strength and a deformation capacity to perform hot forming operations.
  • the invention more specifically relates to steels having a mechanical strength greater than or equal to 1100 MPa (ie a hardness greater than or equal to 300 Hv), having a yield strength greater than or equal to 700 MPa, and a higher breaking elongation or equal to 12%, with a failure greater than 30%.
  • the invention also aims to provide a steel with an ability to be produced in a robust manner that is to say without large variations in properties depending on the manufacturing parameters and machinable with commercially available tools without loss of strength. productivity during implementation.
  • the subject of the invention is a part according to claims 1 to 12 and a part manufacturing method according to claim 13.
  • the chemical composition in percentage by weight, must be the following:
  • the carbon content is between 0.10 and 0.30%. If the carbon content is below 0.10% by weight, there is a risk of forming pro-eutectoid ferrite and insufficient mechanical strength. Beyond 0.30%, the weldability becomes more and more reduced because it is possible to form low-tenacity microstructures in the heat-affected zone (ZAT) or in the melted zone. Within this range, the weldability is satisfactory, and the mechanical properties are stable and consistent with the targets of the invention. According to a preferred embodiment, the carbon content is between 0.15 and 0.27% and preferably between 0.17 and 0.25%.
  • the manganese is between 1, 6 and 2.1% and preferably between 1.7% and 2.0%. It is a hardening element with solid solution of substitution, it stabilizes the austenite and lowers the transformation temperature Ac3. Manganese therefore contributes to an increase in mechanical strength. A minimum content of 1.6% by weight is necessary to obtain the desired mechanical properties. However, beyond 2.1%, its gammagenic character leads to a significant slowing down of the bainitic transformation kinetics occurring during final cooling and the bainite fraction would be insufficient to achieve a yield strength greater than or equal to 700 MPa. . This combines a satisfactory mechanical strength without increasing the risk of decreasing the bainite fraction and thus reducing the yield strength, nor increasing the quenchability in welded alloys, which would adversely affect the weldability of steel according to the invention.
  • the chromium content should be between 0.5% and 1.7% and preferably between 1.0 and 1.5%.
  • This element makes it possible to control the formation of ferrite on cooling from a completely austenitic structure, because this ferrite, in a large quantity, reduces the mechanical strength required for the steel according to the invention.
  • This element also makes it possible to harden and refine the bainitic microstructure, which is why a minimum content of 0.5% is necessary.
  • this element considerably slows down the kinetics of the bainitic transformation, so, for contents greater than 1.7%, the bainite fraction may be insufficient to reach a yield strength greater than or equal to 700 MPa.
  • a range of chromium content of between 1.0% and 1.5% is chosen to refine the bainitic microstructure.
  • the silicon must be between 0.5 and 1.0%. In this range, the residual austenite stabilization is made possible by the addition of silicon which considerably slows the precipitation of carbides during bainitic transformation. This has been corroborated by the inventors who have noted that the bainite of the invention is virtually free of carbides. This is because the solubility of silicon in cementite is very low and this element increases carbon activity in austenite. Any formation of cementite will therefore be preceded by a step of rejection of Si at the interface. The enrichment of the austenite carbon, therefore leads to its stabilization at room temperature on the steel according to this first embodiment.
  • the application of an external stress at a temperature below 200 ° C may lead to the transformation of part of this austenite in martensite. This transformation will result in increasing the yield point.
  • the minimum silicon content should be set at 0.5% by weight to achieve the stabilizing effect on the austenite and retard carbide formation.
  • the yield strength does not reach the required minimum of 700 MPa.
  • an addition of silicon in an amount greater than 1.0% will induce an excess of residual austenite which will reduce the yield strength.
  • the silicon content will be between 0.75 and 0.9% in order to optimize the aforementioned effects.
  • the niobium should be between 0.065% and 0.15%. It is a micro-alloy element that has. the particularity of forming hardeners precipitating with carbon and / or nitrogen. II. also makes it possible to delay the bainitic transformation, in synergy with the micro-alloy elements such as boron and molybdenum present in the invention.
  • the niobium content must nevertheless be limited to 0.15% to avoid the formation of large precipitates which may be crack initiation sites and to avoid the problems of loss of hot ductility associated with a possible intergranular precipitation of nitrides.
  • the niobium content must be greater than or equal to 0.065% which, combined with titanium, makes it possible to have a stabilizing effect on the final mechanical properties, ie a lower sensitivity to the speed of cooling. Indeed, it can form mixed carbonitrides with titanium and remain stable at relatively high temperatures, which makes it possible to avoid the abnormal magnification of the grains at high temperature, or even allowing sufficiently high refinement of the austenitic grain.
  • the maximum content of Nb is in the range 0.065% and 0, 0% to optimize the aforementioned effects.
  • the titanium content should be such that 0.010 ⁇ Ti ⁇ 0.1%.
  • a content maximum of 0.1% is tolerated, above titanium will have the effect of increasing the price and generate harmful precipitates for fatigue resistance and machinability.
  • a minimum of 0.010% is required to control the austenitic grain size and to protect the boron from nitrogen.
  • a titanium content range of between 0% and 0.20% and 0.03% is chosen.
  • the boron content should be between 10 ppm (0.0010%) and 50 ppm (0.0050%).
  • This element makes it possible to control the formation of ferrite on cooling from a completely austenitic structure, because this ferrite, in a large quantity, would reduce the mechanical strength and the elastic limit targeted by the invention. This is a soaking element.
  • a minimum content of 10 ppm is necessary to avoid the formation of ferrite during natural cooling, so generally below 2 ° C / s for the types of parts covered by the invention.
  • above 50 ppm boron will have the effect of forming iron borides that may be harmful to ductility.
  • a range of boron content of between 20 ppm and 30 ppm is chosen to optimize the above-mentioned effects.
  • the nitrogen content should be between 10 ppm (0.0010%) and 130 ppm (0.0130%).
  • a minimum content of 10 ppm is required to form the abovementioned carbonitrides.
  • the nitrogen may cause the bainitic ferrite to become too hard to harden, with possible reduction in the resilience of the finished part.
  • a range of nitrogen content between 50 ppm and 120 ppm is chosen to optimize the aforementioned effects.
  • the aluminum content must be less than or equal to 0.050% and preferably less than or equal to 0.040%, or even less than or equal to 0.020%.
  • the Al content is such that 0.003% ⁇ Al 0,0 0.015%. This is a residual element whose content we wish to limit.
  • High levels of aluminum are considered to increase erosion of refractories and the risk of clogging of the nozzles during steel casting.
  • aluminum segregates negatively and, it can lead to macro-segregations. In excessive amounts, aluminum can reduce hot ductility and increase the risk of defects in continuous casting. Without a strong control of the casting conditions, the defects of the micro and macro segregation type ultimately give rise to segregation on the forged part.
  • This band structure consists of alternating bainitic strips with different hardnesses which can adversely affect the formability of the material.
  • the molybdenum content must be less than or equal to 1.0%, preferably less than or equal to 0.5%. Preferably, a range of molybdenum content of between 0.03 and 0.15% is chosen. Its presence is favorable for the formation of bainite by synergistic effect with boron and niobium. It thus makes it possible to guarantee the absence of pro-eutectoid ferrite at the grain boundaries. Beyond a content of 1.0%, it promotes the appearance of martensite which is not sought.
  • the nickel content must be less than or equal to 1.0%. A maximum content of 1.0% is tolerated, above the nickel will have the effect of increasing the price of the proposed solution, which may reduce its viability from an economic point of view.
  • a range of nickel content between 0 and 0.55% is chosen.
  • the vanadium content must be less than or equal to 0.3%. A maximum content of 0.3% is tolerated, above vanadium will have the effect of increasing the price of the solution and affect the resilience.
  • a vanadium content range of between 0 and 0.2% is selected.
  • Sulfur can be at different levels depending on the desired machinability. There will always be a small quantity because it is a residual element whose value can not be reduced to an absolute zero, but it can also be added voluntarily. A lower S content will be aimed if the desired fatigue properties are very high. In general, we will target between 0.015 and 0.04%, knowing that it is possible to add up to 0.1% to improve machinability. Alternatively, it is also possible to add in combination with sulfur one or more elements selected from tellurium, selenium, lead and bismuth in amounts of less than or equal to 0.1% for each element.
  • the phosphorus must be less than or equal to 0.050% and preferably less than or equal to 0.025%. It is an element that hardens in solid solution but significantly reduces weldability and hot ductility, especially due to its ability to segregate at grain boundaries or its tendency to co-segregate with manganese. . For these reasons, its content should be limited to 0.025% in order to obtain good weldability.
  • the copper content must be less than or equal to 0.5% A maximum content of 0.5% is tolerated because above the copper will have the effect of reducing the fitness of the product.
  • the remainder of the composition consists of iron and unavoidable impurities resulting from processing, such as for example arsenic or tin.
  • compositions according to the invention may furthermore fulfill the following conditions, taken alone or in combination:
  • Vr400 represents the cooling rate in the temperature range between 420 and 380 ° C.
  • Vr600 represents the cooling rate in the temperature range between 620 and 580 ° C.
  • the criterion S1 is correlated with the robustness of the mechanical properties compared to the variations of cooling conditions in general and in the face of Vr600 variations in particular.
  • the respect of the value ranges of this criterion thus makes it possible to guarantee a very low sensitivity of the grade to the manufacturing conditions.
  • 0.200 ⁇ S1 ⁇ 0.4 0.200 ⁇ S1 ⁇ 0.4, which further improves the robustness.
  • the criteria S2 to S4 are correlated with obtaining a predominantly bainitic structure with more than 70% for the grades according to the invention, thus making it possible to guarantee the attainment of the intended mechanical properties.
  • the microstructure of the steel may contain, in surface proportion after the final cooling:
  • bainite in a content between 70 and 100%.
  • bainite means a bainite comprising less than 5% carbide surface and whose inter-slab phase is austenite.
  • the steel according to the invention will have a lower mechanical strength than the 1100 MPa referred to.
  • the steel according to the invention may be manufactured by the method described below:
  • a steel of composition according to the invention is supplied in the form of a bloom, a billet of rectangular or round square section, or in the form of an ingot, then
  • This steel is rolled as a semi-finished product, in the form of a bar or wire and
  • one carries the semi-finished product to a reheating temperature (T rec h) of between 00 ° C and 1300 ° C to obtain a semi-finished product heated, then the heated half-product is shaped while hot, the hot-forming end temperature being greater than or equal to 850 ° C. in order to obtain a hot-formed part;
  • T rec h reheating temperature
  • said hot formed part is cooled to a temperature of between 620 and 580 ° C. at a cooling rate Vr600 of between 0.10 ° C./s and 10 ° C./s.
  • said part is cooled down to a temperature between 420 and 380 ° C. at a cooling rate Vr 400 of less than 4 ° C./s, and then the part is cooled between 380 ° C. and 300 ° C. at a lower speed. or equal to 0.3 ° C / s, then
  • the part is cooled to ambient temperature at a speed of less than or equal to 4 ° C./s, then
  • the heat-formed part which is cooled down to ambient temperature is optionally subjected to heat treatment at a temperature of between 300 ° C. and 450 ° C. for a period of between 30 minutes and 120 minutes; then
  • the heat treatment of income is carried out to ensure the obtaining of very good properties of the parts after cooling.
  • the chemical compositions of the steels used in the tests were collated in Table 1.
  • the reheating temperature of these grades was 1250 ° C.
  • the end temperature of hot shaping was 1220 ° C.
  • Cooling rates Vr600 and Vr400 are shown in Table 2.
  • FIG. 1 shows the variation of the mechanical resistance to rupture Rm as a function of the cooling rate Vr600 for the grades A and B.
  • FIG. 2 shows the variation of the elastic limit Re as a function of the cooling speed Vr600 for the shades A and B.
  • the grade according to the invention has a high stability of its mechanical properties when the cooling conditions vary.
  • the grade is therefore much more robust to variations in process conditions than grades according to the prior art.
  • FIG. 3 shows the delta of the mechanical strength at break Rm as a function of the criterion S1 for the grades A, B and C.
  • FIG. 4 shows the delta of the elastic limit Re as a function of the criterion S1. for grades A, B and C.
  • the invention will notably be used with advantage for the manufacture of hot formed parts and in particular, hot forged, for applications in land motor vehicles. It also finds applications in the manufacture of parts for boats or in the field of construction, in particular for the manufacture of screw bars for formwork.
  • the invention can be implemented for the manufacture of all types of parts requiring to achieve the properties referred to

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Abstract

The subject of the invention is a part, the composition of which comprises, the contents being expressed as percentages by weight, 0.10 < C < 0.30, 1.6 < Mn < 2.1, 0.5 < Cr ≤ 1.7, 0.5 < Si < 1.0, 0.065 < Nb < 0.15, 0.0010 < B < 0.0050, 0.0010 < N < 0.0130, 0 < Al < 0.060, 0 < Mo < 1.00, 0 < Ni < 1.0, 0.01 < Ti < 0.07, 0 < V < 0.3, 0 < P < 0.050, 0.01 < S < 0.1, 0 < Cu < 0.5, 0 < Sn < 0.1, the remainder of the composition consisting of iron and inevitable impurities resulting from the smelting, the microstructure consisting, in surface proportions, of 100% to 70% bainite, of less than 30% residual austenite and of less than 5% ferrite, and a process for the manufacture thereof.

Description

PIÈCES A STRUCTURE BAINITIQUE A HAUTES PROPRIETES DE RESISTANCE ET PROCEDE DE FABRICATION  PARTS WITH A BAINITIQUE STRUCTURE HAVING HIGH RESISTANCE PROPERTIES AND METHOD OF MANUFACTURE
L'a présente invention couvre la fabrication de pièces à hautes propriétés de résistance tout en étant usinables, obtenues à partir d'aciers présentant simultanément une bonne ductilité à chaud permettant de réaliser des opérations de formage à chaud et une trempabilité telle qu'il n'est pas utile de réaliser des opérations de trempe et revenu pour obtenir les propriétés annoncées. The present invention covers a parts manufacturing high strength properties while being machineable, obtained from steels simultaneously having good hot ductility for performing hot forming operations and such that n hardenability It is not useful to perform tempering and tempering operations to obtain the advertised properties.
L'invention concerne plus précisément des pièces présentant, quelle que soit la forme et la complexité de la pièce, une résistance mécanique supérieure ou égale à 1100 MPa, présentant une limite d'élasticité supérieure ou égale à 700 MPa, un allongement à rupture A supérieur ou égal à 12 et une striction à rupture Z supérieure à 30%,  The invention relates more precisely to parts having, whatever the shape and complexity of the part, a mechanical strength greater than or equal to 1100 MPa, having a yield strength greater than or equal to 700 MPa, an elongation at break A greater than or equal to 12 and a necking with Z-breaking greater than 30%,
Dans le cadre de la présente invention, on définit par pièce, barres toutes formes, fils ou pièces complexes obtenues par procédé de mise en forme à chaud comme, par exemple, le laminage, ou forgeage avec ou sans opérations ultérieures de réchauffage partiel ou total, de traitement thermique ou thermochimique et/ou de mise en forme avec ou sans enlèvement de matière, voire avec ajout de matière comme pour le soudage.  In the context of the present invention, each part, bar, any form, wire or complex piece obtained by hot forming process is defined as, for example, rolling, or forging with or without subsequent partial or total reheating operations. , thermal or thermochemical treatment and / or shaping with or without removal of material, or even with addition of material as for welding.
On entend par mise en forme à chaud d'un acier tout procédé qui modifie la forme première d'un produit par une opération qui se réalise à une température de la matière telle que la structure cristalline de l'acier est majoritairement austénitique.  By hot forming of a steel is meant any process that modifies the primary form of a product by an operation which is carried out at a temperature of the material such that the crystalline structure of the steel is predominantly austenitic.
La forte demande de réduction d'émissions de gaz à effet de serre, associée à la croissance des exigences de sécurité automobile et les prix du carburant ont poussé les constructeurs de véhicules terrestres à moteur à rechercher des matériaux présentant une résistance mécanique élevée. Cela permet de réduire le poids de ces pièces tout en maintenant ou en augmentant les performances de résistance mécanique. Pour obtenir de très hautes caractéristiques mécaniques, les solutions traditionnelles en acier existent depuis très longtemps. Elles contiennent des éléments d'alliage en plus ou moins grande quantité associés à des traitements thermiques de type austénitisation à une température supérieure à AC1 , suivie d'une trempe dans un fluide de type huile, polymère voire de l'eau et en général d'un revenu à une température inférieure à Ar3. Certains inconvénients associés à ces aciers et aux traitements nécessaires pour obtenir les propriétés demandées peuvent être d'ordre économique (coût des alliages, coût des traitements thermiques), environnemental (énergie dépensée pour la ré-austénitisation, dispersée par la trempe, traitement des bains de trempe), ou géométrique (déformation des pièces complexes). Dans cette perspective, les aciers permettant d'obtenir une résistance relativement élevée, juste après la mise en forme à chaud, prennent une importance grandissante. Il a ainsi été proposé, dans le temps, plusieurs familles d'aciers offrant divers niveaux de résistance mécanique, comme par exemple les aciers micro-alliés à structure ferrito perlitique à différentes teneurs en Carbone pour obtenir plusieurs niveaux de résistance. Ces aciers micro-alliés ferrito perlitiques se sont largement répandus dans les dernières décennies et sont très souvent utilisés pour toutes sortes de pièces mécaniques pour obtenir des pièces complexes sans traitement thermique directement après mise en forme à chaud. Bien que très performants, ces aciers voient maintenant leurs limites lorsque les concepteurs réclament des propriétés mécaniques dépassant les 700 MPa de limite élastique et les 1100 MPa de résistance mécanique, ce qui les oblige souvent à revenir à des solutions traditionnelles évoquées plus haut. The strong demand for reduced greenhouse gas emissions, coupled with growing automotive safety requirements and fuel prices, has prompted manufacturers of motorized land vehicles to look for materials with high mechanical strength. This reduces the weight of these parts while maintaining or increasing the mechanical strength performance. To obtain very high mechanical characteristics, traditional steel solutions have existed for a very long time. They contain alloying elements of greater or lesser quantity associated with thermal treatments of the austenitization type at a temperature greater than AC1, followed by quenching in an oil, polymer or even water-type fluid and generally an income at a temperature lower than Ar3. Some disadvantages associated with these steels and the treatments necessary to obtain the properties required can be of an economic nature (cost of alloys, cost of heat treatments), environmental (energy spent on re-austenitization, dispersed by quenching, treatment of baths tempering), or geometric (deformation of complex parts). In this perspective, steels to obtain a relatively high strength, just after hot forming, take on increasing importance. It has thus been proposed, over time, several families of steels offering various levels of mechanical strength, such as micro-alloyed steels ferritic pearlitic structure with different levels of carbon to obtain several levels of resistance. These micro-alloyed ferritic pearlitic steels have become widespread in recent decades and are very often used for all kinds of mechanical parts to obtain complex parts without heat treatment directly after hot forming. Although very efficient, these steels now have their limits when designers claim mechanical properties exceeding 700 MPa yield strength and 1100 MPa mechanical strength, which often requires them to return to traditional solutions mentioned above.
En outre, en fonction de l'épaisseur ét de la forme des pièces, il peut être difficile de garantir une homogénéité satisfaisante des propriétés, en raison notamment de l'hétérogénéité des vitesses de refroidissement qui impacte la microstructure.  In addition, depending on the thickness and shape of the parts, it can be difficult to ensure satisfactory homogeneity of the properties, particularly because of the heterogeneity of the cooling rates which impacts the microstructure.
Afin de répondre à cette demande de véhicules de plus en plus légers, tout en conservant les avantages économiques et environnementaux des aciers microalliés à matrice ferrito perlitique, il est donc nécessaire d'avoir des aciers de plus en plus résistants, obtenus directement après les opérations de mise en forme à chaud. Cependant, il est connu que dans le domaine des aciers au carbone, une augmentation de la résistance mécanique s'accompagne généralement d'une perte de ductilité et d'une perte d'usinabilité. En outre, les constructeurs de véhicules terrestres à moteur définissent des pièces de plus.en plus complexes qui nécessitent des aciers présentant des niveaux élevés de. résistance mécanique , de résistance à la fatigue, de ténacité, de formabilité, et d'usinabilité. In order to meet this demand for increasingly light vehicles, while retaining the economic and environmental benefits of microalloyed pearlite ferritic steels, it is therefore necessary to have increasingly resistant steels obtained directly after the operations. from fitness to hot. However, it is known that in the field of carbon steels, an increase in mechanical strength is generally accompanied by a loss of ductility and a loss of machinability. In addition, manufacturers of motorized land vehicles define more complex parts that require steels with high levels of. mechanical strength, fatigue resistance, toughness, formability, and machinability.
On a pu prendre connaissance du brevet EP0787812 décrivant un procédé pour la fabrication de pièces forgées dont la composition chimique comprend, en poids:0,1%≤C≤0,4% ;1%<Mn<1 ,8% ;1 ,2%<Si<1 ,7% ;0%<Ni<1 % ;0%<Cr<1 ,2% ;0 %<Mo<0,3% ;0%<V<0,3% ;Cu < 0,35% éventuellement de 0,005% à 0,06% d'aluminium, éventuellement du bore en des teneurs comprises entre 0,0005% et 0,01 %, éventuellement entre 0,005% et 0,03% de titane, éventuellement entre 0,005% et 0,06% de niobium, éventuellement de 0,005% à 0,1 % de soufre, éventuellement jusqu'à 0,006% de calcium, éventuellement jusqu'à 0,03% de tellure, éventuellement jusqu'à 0,05% de sélénium, éventuellement jusqu'à 0,05% de bismuth, éventuellement jusqu'à 0,1 % de plomb, le reste étant du fer et des impuretés résultant de l'élaboration. Ce procédé impliquant que l'on soumette la pièce à un traitement thermique comportant un refroidissement depuis une température à laquelle l'acier est entièrement austénitique jusqu'à une température Tm comprise entre Ms+100 D°C et Ms-20 °C à une vitesse de refroidissement Vr supérieure à 0,5 °C/s, suivi d'un maintien de la pièce entre Tm et Tf, avec Tf > Tm-100 °C, et de préférence Tf > Tm-60 °C, pendant au moins 2 minutes de façon à obtenir une structure comportant au moins 15%, et de préférence, au moins 30% de bainite formée entre Tm et Tf. Cette technique nécessite de nombreuses étapes de procédé nuisibles à la productivité.  EP0787812 describes a process for the manufacture of forged parts whose chemical composition comprises, by weight: 0.1% ≤C≤0.4%; 1% <Mn <1, 8%; 1, 2% <Si <1, 7%; 0% <Ni <1%; 0% <Cr <1, 2%; 0% <Mo <0.3%; 0% <V <0.3%; Cu < 0.35% optionally from 0.005% to 0.06% aluminum, optionally boron in contents of between 0.0005% and 0.01%, optionally between 0.005% and 0.03% titanium, optionally between 0.005 % and 0.06% of niobium, optionally from 0.005% to 0.1% of sulfur, optionally up to 0.006% of calcium, optionally up to 0.03% of tellurium, optionally up to 0.05% of selenium, optionally up to 0.05% bismuth, optionally up to 0.1% lead, the balance being iron and impurities resulting from the preparation. This method involves subjecting the workpiece to a heat treatment having a cooling from a temperature at which the steel is fully austenitic to a temperature Tm of between Ms + 100 D ° C and Ms-20 ° C at a temperature of cooling rate Vr greater than 0.5 ° C / s, followed by holding the workpiece between Tm and Tf, with Tf> Tm-100 ° C, and preferably Tf> Tm-60 ° C, for at least 2 minutes to obtain a structure comprising at least 15%, and preferably at least 30% of bainite formed between Tm and Tf. This technique requires many process steps that are detrimental to productivity.
D'autre part, on a connaissance de la demande EP1201774 dont l'objectif de l'invention est de fournir un procédé de forgeage réalisé de manière à améliorer l'usinabilité, en modifiant la structure métallographique des produits soumis à la charge d'impact en une structure ferrito-perlitique fine sans adopter la méthode de trempe et revenu, et ce afin d'obtenir une limite d'élasticité excédant celle obtenue par le procédé de trempe et revenu. La résistance à la traction (Rm) obtenue est inférieure à celle obtenu par le procédé de trempe et revenu. Cette méthode présente elle aussi l'inconvénient de nécessiter de nombreuses étapes de procédé complexifiant le procédé de fabrication. En outre l'absence d'éléments précis de composition chimique peut mener à l'utilisation" d'une composition chimique inadaptée pour des applications de pièces forgées car nuisibles à la soudabilité, l'usinabilité voire la ténacité. On the other hand, it is known from the application EP1201774 whose objective of the invention is to provide a forging process carried out so as to improve the machinability, by modifying the metallographic structure of the products subjected to the impact load in a fine ferrito-pearlitic structure without adopting the quenching and tempering method, in order to obtain a yield strength exceeding that obtained by the quenching and tempering process. The tensile strength (Rm) obtained is lower than that obtained by the tempering and tempering process. This method also has the disadvantage of requiring many process steps that complicate the manufacturing process. Furthermore the absence of specific elements of chemical composition may lead to the use of "inadequate chemical composition forgings applications as harmful to the weldability, machinability or toughness.
Le but de la présente invention est de résoudre les problèmes évoqués ci- dessus. Elle vise à mettre à disposition un acier pour pièces mises en forme à chaud à hautes propriétés de résistance, ' présentant simultanément une résistance mécanique et une capacité de déformation permettant de réaliser des opérations de mise en forme à chaud. L'invention concerne plus précisément des aciers présentant une résistance mécanique supérieure ou égale à 1100 MPa (soit une dureté supérieure ou égale à 300 Hv), présentant une limite d'élasticité supérieure ou égale à 700 MPa, et un allongement à rupture supérieur ou égal à 12%, avec une striction à rupture supérieure à 30%. L'invention vise également à mettre à disposition un acier avec une aptitude à être produit de manière robuste c'est-à-dire sans grandes variations de propriétés en fonction des paramètres de fabrication et usinable avec des outils disponibles dans le commerce sans perte de productivité pendant la mise en œuvre.  The object of the present invention is to solve the problems mentioned above. It aims to provide a steel for hot formed parts with high strength properties, simultaneously having a mechanical strength and a deformation capacity to perform hot forming operations. The invention more specifically relates to steels having a mechanical strength greater than or equal to 1100 MPa (ie a hardness greater than or equal to 300 Hv), having a yield strength greater than or equal to 700 MPa, and a higher breaking elongation or equal to 12%, with a failure greater than 30%. The invention also aims to provide a steel with an ability to be produced in a robust manner that is to say without large variations in properties depending on the manufacturing parameters and machinable with commercially available tools without loss of strength. productivity during implementation.
A cet effet, l'invention a pour objet une pièce selon les revendications 1 à 12 et un procédé de fabrication de pièce selon la revendication 13.  For this purpose, the subject of the invention is a part according to claims 1 to 12 and a part manufacturing method according to claim 13.
D'autres caractéristiques et avantages de l'invention apparaîtront au cours de la description ci-dessous, donné à titre d'exemple non limitatif.  Other features and advantages of the invention will become apparent from the description below, given by way of non-limiting example.
Dans le cadre de l'invention, la composition chimique, en pourcentage en poids, doit être la suivante :  In the context of the invention, the chemical composition, in percentage by weight, must be the following:
La teneur en carbone est comprise entre 0,10 et 0,30%. Si la teneur en carbone est en-dessous de 0,10 % en poids, il y a un risque de former de la ferrite pro-eutectoide et d'obtenir une résistance mécanique insuffisante. Au-delà de 0,30%, la soudabilité devient de plus en plus réduite car on peut former des microstructures de faible ténacité dans la Zone Affectée Thermiquement (ZAT) ou dans la zone fondue Au sein de cette plage, la soudabilité est satisfaisante, et les propriétés mécaniques sont stables et conformes aux cibles visées par l'invention. Selon un mode de réalisation préféré, la teneur en carbone est comprise entre 0,15 et 0,27% et de préférence entre 0,17 et 0,25%. The carbon content is between 0.10 and 0.30%. If the carbon content is below 0.10% by weight, there is a risk of forming pro-eutectoid ferrite and insufficient mechanical strength. Beyond 0.30%, the weldability becomes more and more reduced because it is possible to form low-tenacity microstructures in the heat-affected zone (ZAT) or in the melted zone. Within this range, the weldability is satisfactory, and the mechanical properties are stable and consistent with the targets of the invention. According to a preferred embodiment, the carbon content is between 0.15 and 0.27% and preferably between 0.17 and 0.25%.
Le manganèse est compris entre 1 ,6 et 2,1 % et de préférence compris entre 1 ,7% et 2,0%. C'est un élément durcissant par solution solide de substitution, il stabilise l'austénite et abaisse la température de transformation Ac3. Le manganèse contribue donc à une augmentation de la résistance mécanique. Une teneur minimale de 1 ,6% en poids est nécessaire pour obtenir les propriétés mécaniques désirées. Cependant, au-delà de 2,1%, son caractère gammagène conduit à un ralentissement significatif de la cinétique de transformation bainitique ayant lieu lors refroidissement final et la fraction de bainite serait insuffisante pour atteindre une résistance d'élasticité supérieure ou égale à 700 MPa. On combine ainsi une résistance mécanique satisfaisante sans accroître le risque de diminuer la fraction de bainite et donc de diminuer la limite d'élasticité, ni d'augmenter la trempabilité dans les alliages soudés, ce qui nuirait à la capacité au soudage de l'acier selon l'invention. The manganese is between 1, 6 and 2.1% and preferably between 1.7% and 2.0%. It is a hardening element with solid solution of substitution, it stabilizes the austenite and lowers the transformation temperature Ac3. Manganese therefore contributes to an increase in mechanical strength. A minimum content of 1.6% by weight is necessary to obtain the desired mechanical properties. However, beyond 2.1%, its gammagenic character leads to a significant slowing down of the bainitic transformation kinetics occurring during final cooling and the bainite fraction would be insufficient to achieve a yield strength greater than or equal to 700 MPa. . This combines a satisfactory mechanical strength without increasing the risk of decreasing the bainite fraction and thus reducing the yield strength, nor increasing the quenchability in welded alloys, which would adversely affect the weldability of steel according to the invention.
La teneur en chrome doit être comprise entre 0,5% et 1 ,7% et de préférence entre 1 ,0 et 1 ,5%. Cet élément permet de contrôler la formation de ferrite au refroidissement à partir d'une structure entièrement austénitique, car cette ferrite, en quantité élevée diminue la résistance mécanique nécessaire à l'acier selon l'invention. Cet élément permet en outre de durcir et d'affiner la microstructure bainitique, c'est pourquoi une teneur minimale de 0,5% est nécessaire. Cependant, cet élément ralentit considérablement la cinétique de la transformation bainitique, ainsi, pour des teneurs supérieures à 1 ,7 %, la fraction de bainite risque d'être insuffisante pour atteindre une limite d'élasticité supérieure ou égale à 700 MPa. A titre préférentiel on choisit un intervalle de teneur en chrome compris entre 1 ,0% et 1 ,5% pour affiner la microstructure bainitique.  The chromium content should be between 0.5% and 1.7% and preferably between 1.0 and 1.5%. This element makes it possible to control the formation of ferrite on cooling from a completely austenitic structure, because this ferrite, in a large quantity, reduces the mechanical strength required for the steel according to the invention. This element also makes it possible to harden and refine the bainitic microstructure, which is why a minimum content of 0.5% is necessary. However, this element considerably slows down the kinetics of the bainitic transformation, so, for contents greater than 1.7%, the bainite fraction may be insufficient to reach a yield strength greater than or equal to 700 MPa. Preferably, a range of chromium content of between 1.0% and 1.5% is chosen to refine the bainitic microstructure.
Le silicium doit être compris entre 0,5 et 1 ,0%. Dans cette fourchette, la stabilisation d'austénite résiduelle est rendue possible par l'addition de silicium qui ralentit considérablement la précipitation des carbures lors de la transformation bainitique. Ceci a été corroboré par les inventeurs qui ont noté que la bainite de l'invention est quasiment exempte de carbures. Ceci provient du fait que la solubilité du silicium dans la cémentite est très faible et que cet élément augmente l'activité du carbone dans l'austénite. Toute formation de cémentite sera donc précédée d'une étape de rejet de Si à l'interface. L'enrichissement de l'austénite en carbone, mène donc à sa stabilisation à la température ambiante sur l'acier selon ce premier mode de réalisation. Par la suite, l'application d'une contrainte extérieure à une température inférieure à 200°C par exemple, de mise en forme ou de sollicitation mécanique de type écrouissage ou de type fatigue, peut conduire à la transformation d'une partie de cette austénite en martensite. Cette transformation aura pour résultat d'augmenter la limite élastique. La teneur minimale en silicium doit être fixée à 0,5% en poids pour obtenir l'effet stabilisant sur l'austénite et retarder la formation des carbures. En outre, on observe que, si le . silicium est inférieur à 0,5%, la limite d'élasticité n'atteint pas le minimum requis de 700 MPa. Par ailleurs, une addition de silicium en quantité supérieure à 1 ,0% va induire un excès d'austénite résiduelle ce qui va diminuer la limite d'élasticité. De manière préférentielle, la teneur en silicium sera comprise entre 0,75 et 0,9% afin d'optimiser les effets susmentionnés. The silicon must be between 0.5 and 1.0%. In this range, the residual austenite stabilization is made possible by the addition of silicon which considerably slows the precipitation of carbides during bainitic transformation. This has been corroborated by the inventors who have noted that the bainite of the invention is virtually free of carbides. This is because the solubility of silicon in cementite is very low and this element increases carbon activity in austenite. Any formation of cementite will therefore be preceded by a step of rejection of Si at the interface. The enrichment of the austenite carbon, therefore leads to its stabilization at room temperature on the steel according to this first embodiment. Subsequently, the application of an external stress at a temperature below 200 ° C, for example, shaping or mechanical stressing type work hardening or fatigue type, may lead to the transformation of part of this austenite in martensite. This transformation will result in increasing the yield point. The minimum silicon content should be set at 0.5% by weight to achieve the stabilizing effect on the austenite and retard carbide formation. In addition, it is observed that, if the. silicon is less than 0.5%, the yield strength does not reach the required minimum of 700 MPa. Moreover, an addition of silicon in an amount greater than 1.0% will induce an excess of residual austenite which will reduce the yield strength. Preferably, the silicon content will be between 0.75 and 0.9% in order to optimize the aforementioned effects.
Le niobium doit être compris entre 0,065% et 0,15%. C'est un élément de micro-alliage qui a . la particularité de former des précipités durcissants avec le carbone et/ou l'azote. II. permet en outre de retarder la transformation bainitique, en synergie avec les éléments de micro-alliage comme le bore et le molybdène présents dans l'invention. La teneur en niobium doit néanmoins être limitée à 0,15% pour éviter la formation de précipités de grande taille qui peuvent être des sites d'amorçage de fissures et pour éviter les problèmes de perte de ductilité à chaud associés à une précipitation intergranulaire éventuelle de nitrures. En outre, la teneur en niobium doit être supérieure ou égale à 0,065% ce qui, combiné avec le Titane, permet d'avoir un effet stabilisant sur les propriétés mécaniques finales, c'est-à-dire une moindre sensibilité à la vitesse de refroidissement. En effet, il peut former des carbonitrures mixtes avec le Titane et rester stable à des températures relativement élevées, ce qui permet d'éviter le grossissement anormal des grains à haute température, voire ce qui permet un affinement suffisamment important du grain austénitique. Préférentiellement la teneur maximale en Nb est comprise dans la gamme 0,065 % et 0, 0% pour optimiser les effets susmentionnés.  The niobium should be between 0.065% and 0.15%. It is a micro-alloy element that has. the particularity of forming hardeners precipitating with carbon and / or nitrogen. II. also makes it possible to delay the bainitic transformation, in synergy with the micro-alloy elements such as boron and molybdenum present in the invention. The niobium content must nevertheless be limited to 0.15% to avoid the formation of large precipitates which may be crack initiation sites and to avoid the problems of loss of hot ductility associated with a possible intergranular precipitation of nitrides. In addition, the niobium content must be greater than or equal to 0.065% which, combined with titanium, makes it possible to have a stabilizing effect on the final mechanical properties, ie a lower sensitivity to the speed of cooling. Indeed, it can form mixed carbonitrides with titanium and remain stable at relatively high temperatures, which makes it possible to avoid the abnormal magnification of the grains at high temperature, or even allowing sufficiently high refinement of the austenitic grain. Preferably the maximum content of Nb is in the range 0.065% and 0, 0% to optimize the aforementioned effects.
La teneur en titane doit être telle que 0,010 < Ti < 0,1 %. Une teneur maximale de 0,1 % est tolérée, au dessus le titane aura pour effet d'augmenter le prix et de générer des précipités nocifs pour la tenue en fatigue et l'usinabilité. Une teneur minimale de 0,010% est nécessaire pour contrôler la taille de grain austénitique et pour protéger le bore de l'azote. A titre préférentiel, on choisit un intervalle de teneur en titane compris entre 0|020% et 0,03%. The titanium content should be such that 0.010 <Ti <0.1%. A content maximum of 0.1% is tolerated, above titanium will have the effect of increasing the price and generate harmful precipitates for fatigue resistance and machinability. A minimum of 0.010% is required to control the austenitic grain size and to protect the boron from nitrogen. As a preference, a titanium content range of between 0% and 0.20% and 0.03% is chosen.
La teneur en bore doit être comprise entre 10 ppm (0,0010%) et 50 ppm (0,0050%). Cet élément permet de contrôler la formation de ferrite au refroidissement à partir d'une structure entièrement austénitique, car cette ferrite, en quantité élevée diminuerait la résistance mécanique et la limite élastique visées par l'invention. Il s'agit d'un élément trempant. Une teneur minimale de 10 ppm est nécessaire pour éviter la formation de ferrite lors du refroidissement naturel donc en général inférieur à 2°C/s pour les types de pièces visées par l'invention. Cependant, au dessus de 50 ppm le bore aura pour effet de former des Borures de fer qui peuvent être néfastes pour la ductilité. A titre préférentiel on choisit un intervalle de teneur en bore compris entre 20 ppm et 30 ppm pour optimiser les effets susmentionnés. The boron content should be between 10 ppm (0.0010%) and 50 ppm (0.0050%). This element makes it possible to control the formation of ferrite on cooling from a completely austenitic structure, because this ferrite, in a large quantity, would reduce the mechanical strength and the elastic limit targeted by the invention. This is a soaking element. A minimum content of 10 ppm is necessary to avoid the formation of ferrite during natural cooling, so generally below 2 ° C / s for the types of parts covered by the invention. However, above 50 ppm boron will have the effect of forming iron borides that may be harmful to ductility. Preferably, a range of boron content of between 20 ppm and 30 ppm is chosen to optimize the above-mentioned effects.
La teneur en azote doit être comprise entre 10 ppm (0,0010%) et 130 ppm (0,0130%). Une teneur minimale de 10 ppm est nécessaire pour former les carbonitrures sus mentionnés. Cependant, au dessus de 130 ppm l'azote pourra avoir pour effet un durcissement trop élevé de la ferrite bainitique, avec diminution possible de la résilience de la pièce finie. A titre préférentiel, on choisit un intervalle de teneur en azote compris entre 50 ppm et 120 ppm pour optimiser les effets susmentionnés. The nitrogen content should be between 10 ppm (0.0010%) and 130 ppm (0.0130%). A minimum content of 10 ppm is required to form the abovementioned carbonitrides. However, above 130 ppm, the nitrogen may cause the bainitic ferrite to become too hard to harden, with possible reduction in the resilience of the finished part. Preferably, a range of nitrogen content between 50 ppm and 120 ppm is chosen to optimize the aforementioned effects.
La teneur en aluminium doit être inférieure ou égale à 0,050% et de préférence inférieure ou égale à 0,040%, voire inférieure ou égale à 0,020%. A titre préférentiel, la teneur en Al est telle que 0,003 % < Al≤ 0,015%. Il s'agit d'un élément résiduel dont on souhaite limiter la teneur. On considère que des teneurs élevées en aluminium accroissent l'érosion des réfractaires et le risque de bouchage des busettes lors de la coulée de l'acier. De plus l'aluminium ségrége négativement et, il peut mener à des macro-ségrégations. En quantité excessive, l'aluminium peut diminuer la ductilité à chaud et augmenter le risque d'apparition de défauts en coulée continue. Sans un contrôle poussé des conditions de coulée, les défauts de type micro et macro ségrégation donnent, in fine, une ségrégation sur la pièce forgée. Cette structure en bandes est constituée d'alternance de bandes bainitiques avec des duretés différentes ce qui peut nuire à la formabilité du matériau. La teneur en molybdène doit être inférieure ou égale à 1 ,0 %, de préférence inférieure ou égale à 0,5%. A titre préférentiel on choisit un intervalle de teneur en molybdène compris entre 0,03 et 0, 15%. Sa présence est favorable à la formation de la bainite par effet de synergie avec le bore et le niobium. Il permet ainsi de garantir l'absence de ferrite pro-eutectoide aux joints de grains. Au-delà d'une teneur de 1 ,0%, il favorise l'apparition de martensite qui n'est pas recherchée. The aluminum content must be less than or equal to 0.050% and preferably less than or equal to 0.040%, or even less than or equal to 0.020%. As a preference, the Al content is such that 0.003% <Al 0,0 0.015%. This is a residual element whose content we wish to limit. High levels of aluminum are considered to increase erosion of refractories and the risk of clogging of the nozzles during steel casting. In addition aluminum segregates negatively and, it can lead to macro-segregations. In excessive amounts, aluminum can reduce hot ductility and increase the risk of defects in continuous casting. Without a strong control of the casting conditions, the defects of the micro and macro segregation type ultimately give rise to segregation on the forged part. This band structure consists of alternating bainitic strips with different hardnesses which can adversely affect the formability of the material. The molybdenum content must be less than or equal to 1.0%, preferably less than or equal to 0.5%. Preferably, a range of molybdenum content of between 0.03 and 0.15% is chosen. Its presence is favorable for the formation of bainite by synergistic effect with boron and niobium. It thus makes it possible to guarantee the absence of pro-eutectoid ferrite at the grain boundaries. Beyond a content of 1.0%, it promotes the appearance of martensite which is not sought.
La teneur en nickel doit être inférieure ou égale à 1 ,0%. Une teneur maximale de 1 ,0% est tolérée, au dessus le nickel aura pour effet d'augmenter le prix de la solution proposée, ce qui risque de diminuer sa viabilité d'un point de vue économique. A titre préférentiel on choisit un intervalle de teneur en nickel compris entre 0 et 0,55%. The nickel content must be less than or equal to 1.0%. A maximum content of 1.0% is tolerated, above the nickel will have the effect of increasing the price of the proposed solution, which may reduce its viability from an economic point of view. Preferably, a range of nickel content between 0 and 0.55% is chosen.
La teneur en vanadium doit être inférieure ou égale à 0,3%. Une teneur maximale de 0,3% est tolérée, au dessus le vanadium aura pour effet d'augmenter le prix de la solution et d'affecter la résilience. A titre préférentiel, dans cette invention, on choisit un intervalle de teneur en vanadium compris entre 0 et 0,2%. Le soufre peut être à différents niveaux selon l'usinabilité recherchée. Il y en aura toujours en faible quantité car c'est un élément résiduel dont on ne peut réduire la valeur à un zéro absolu, mais il peut aussi être ajouté volontairement. On visera une teneur en S moindre si les propriétés de fatigue recherchées sont très élevées. D'une façon générale, on visera entre 0,015 et 0,04%, sachant qu'il est possible d'en ajouter jusqu'à 0,1 % pour améliorer l'usinabilité. En variante, il est également possible d'ajouter en combinaison avec le soufre un ou plusieurs éléments choisis parmi le tellure, le sélénium, le plomb et le bismuth dans des quantités inférieures ou égales à 0,1 % pour chaque élément. The vanadium content must be less than or equal to 0.3%. A maximum content of 0.3% is tolerated, above vanadium will have the effect of increasing the price of the solution and affect the resilience. Preferably, in this invention, a vanadium content range of between 0 and 0.2% is selected. Sulfur can be at different levels depending on the desired machinability. There will always be a small quantity because it is a residual element whose value can not be reduced to an absolute zero, but it can also be added voluntarily. A lower S content will be aimed if the desired fatigue properties are very high. In general, we will target between 0.015 and 0.04%, knowing that it is possible to add up to 0.1% to improve machinability. Alternatively, it is also possible to add in combination with sulfur one or more elements selected from tellurium, selenium, lead and bismuth in amounts of less than or equal to 0.1% for each element.
Le phosphore doit être inférieur ou égale à 0,050% et de préférence inférieur ou égal à 0,025%. C'est un élément qui durcit en solution solide mais qui diminue considérablement la soudabilité et la ductilité à chaud, particulièrement en raison de son aptitude à la ségrégation aux joints de grains ou à sa tendance à la co- ségrégation avec le manganèse. . Pour ces raisons, sa teneur doit être limitée à .0,025% afin d'obtenir une-bonne aptitude au soudage. The phosphorus must be less than or equal to 0.050% and preferably less than or equal to 0.025%. It is an element that hardens in solid solution but significantly reduces weldability and hot ductility, especially due to its ability to segregate at grain boundaries or its tendency to co-segregate with manganese. . For these reasons, its content should be limited to 0.025% in order to obtain good weldability.
"La teneur en cuivre doit être inférieure ou égale à 0,5%. Une teneur maximale de 0,5% est tolérée, car au dessus le cuivre aura pour effet de diminuer l'aptitude à la mise en forme du produit. "The copper content must be less than or equal to 0.5% A maximum content of 0.5% is tolerated because above the copper will have the effect of reducing the fitness of the product.
Le reste de la composition 'est constitué de fer et d'impuretés inévitables résultant de l'élaboration, telles que par exemple l'arsenic ou l'étain. The remainder of the composition consists of iron and unavoidable impurities resulting from processing, such as for example arsenic or tin.
Dans des modes de réalisation préférées, les compositions chimiques selon l'invention peuvent en outre remplir les conditions suivantes, prises seules ou en combinaison : In preferred embodiments, the chemical compositions according to the invention may furthermore fulfill the following conditions, taken alone or in combination:
0, 1 < S1 < 0,4 et 0, 1 <S1 <0.4 and
0,5 < S2 < 1 ,8 0,7 < S3 < 1 ,6 0.5 <S2 <1, 8 0.7 <S3 <1, 6
0,3 < S4 < 1 ,5 avec 0.3 <S4 <1.5 with
S1 = Nb + V + Mo + Ti + AI S1 = Nb + V + Mo + Ti + AI
S2= C + N +Cr/2+(S1 )/6 + (Si + Mn - 4 * S) /10 + Ni/20 S3= S2 + 1/3 x Vr600 S2 = C + N + Cr / 2 + (S1) / 6 + (Si + Mn - 4 * S) / 10 + Ni / 20 S3 = S2 + 1/3 x Vr600
S4 = S3 - Vr400 dans lesquelles les teneurs des éléments sont exprimées en pourcentage an poids et les vitesses de refroidissement Vr400 et Vr600 sont exprimées en °C/s. Vr400 représente la vitesse de refroidissement dans l'intervalle de température entre 420 et 380°C. Vr600 représente la vitesse de refroidissement dans l'intervalle de température entre 620 et 580°C. S4 = S3 - Vr400 in which the contents of the elements are expressed as a percentage by weight and the cooling rates Vr400 and Vr600 are expressed in ° C / s. Vr400 represents the cooling rate in the temperature range between 420 and 380 ° C. Vr600 represents the cooling rate in the temperature range between 620 and 580 ° C.
Comme on le verra dans les essais décrits ci-dessous, le critère S1 est corrélé avec la robustesse des propriétés mécaniques face aux variations de conditions de refroidissement en général et face aux variations de Vr600 en particulier. Le respect des fourchettes de valeur de ce critère permet donc de garantir une très faible sensibilité de la nuance aux conditions- de fabrication. Dans un mode de réalisation préféré, 0,200 < S1 < 0,4, ce qui permet d'améliorer encore la robustesse. As will be seen in the tests described below, the criterion S1 is correlated with the robustness of the mechanical properties compared to the variations of cooling conditions in general and in the face of Vr600 variations in particular. The respect of the value ranges of this criterion thus makes it possible to guarantee a very low sensitivity of the grade to the manufacturing conditions. In a preferred embodiment, 0.200 <S1 <0.4, which further improves the robustness.
D'autre part, les critères S2 à S4 sont corrélés avec l'obtention d'une structure majoritairement bainitique à plus de 70% pour les nuances selon l'invention, permettant ainsi de garantir l'atteinte des propriétés mécaniques visées.  On the other hand, the criteria S2 to S4 are correlated with obtaining a predominantly bainitic structure with more than 70% for the grades according to the invention, thus making it possible to guarantee the attainment of the intended mechanical properties.
Selon l'invention, la microstructure de l'acier peut contenir, en proportion surfaciques après le refroidissement final :  According to the invention, the microstructure of the steel may contain, in surface proportion after the final cooling:
- de la bainite en une teneur comprise entre 70 et 100%. Dans le cadre de la présente invention, on entend par bainite, une bainite comprenant moins de 5% en surface de carbures et dont la phase inter-lattes est de l'austénite.  - bainite in a content between 70 and 100%. In the context of the present invention, bainite means a bainite comprising less than 5% carbide surface and whose inter-slab phase is austenite.
- de l'austénite résiduelle en une teneur inférieure ou égale à 30%  - residual austenite in a content of not more than 30%
- de la ferrite en une teneur inférieure à 5%. En particulier, si la teneur en ferrite est supérieure à 5%, l'acier selon l'invention présentera une résistance mécanique inférieure aux 1100 MPa visés.  ferrite at a content of less than 5%. In particular, if the ferrite content is greater than 5%, the steel according to the invention will have a lower mechanical strength than the 1100 MPa referred to.
L'acier selon l'invention pourra être fabriqué par le procédé décrit ci-dessous :The steel according to the invention may be manufactured by the method described below:
- on approvisionne un acier de composition selon l'invention sous forme de bloom, de billette de section carrée rectangle ou ronde, ou sous forme de lingot, puis a steel of composition according to the invention is supplied in the form of a bloom, a billet of rectangular or round square section, or in the form of an ingot, then
- on lamine cet acier sous forme de demi-produit, sous forme de barre ou de fil puis  - This steel is rolled as a semi-finished product, in the form of a bar or wire and
- on porte le demi-produit à une température de réchauffage (Trech) comprise entre 00°C et 1300°C pour obtenir un demi-produit réchauffé, puis - on met en forme à chaud le demi-produit réchauffé, la température de fin de mise en forme à chaud étant supérieure ou égale à 850°C pour obtenir une pièce formée à chaud, puis, - one carries the semi-finished product to a reheating temperature (T rec h) of between 00 ° C and 1300 ° C to obtain a semi-finished product heated, then the heated half-product is shaped while hot, the hot-forming end temperature being greater than or equal to 850 ° C. in order to obtain a hot-formed part;
- on refroidit ladite pièce formée à chaud jusqu'à atteindre une température comprise entre 620 et 580°C à une vitesse de refroidissement Vr600 comprise entre 0, 10 °C/s et 10 °C/s puis said hot formed part is cooled to a temperature of between 620 and 580 ° C. at a cooling rate Vr600 of between 0.10 ° C./s and 10 ° C./s.
- on refroidit ladite pièce jusqu'à atteindre une température comprise entre 420 et 380°C à une vitesse de refroidissement Vr400 inférieure à 4°C/s, puis - on refroidit la pièce entre 380 °C et 300°C à une vitesse inférieure ou égale à 0,3 °C/s, puis said part is cooled down to a temperature between 420 and 380 ° C. at a cooling rate Vr 400 of less than 4 ° C./s, and then the part is cooled between 380 ° C. and 300 ° C. at a lower speed. or equal to 0.3 ° C / s, then
- on refroidit la pièce jusqu'à la température ambiante à une vitesse inférieure ou égale à 4°C/s, puis, the part is cooled to ambient temperature at a speed of less than or equal to 4 ° C./s, then
- on fait éventuellement subir un traitement thermique de revenu à ladite pièce formée à chaud et refroidie jusqu'à l'ambiante, à une température de revenu comprise entre 300 °C et 450°C pendant une durée comprise entre 30 minutes et 120 minutes, puis the heat-formed part which is cooled down to ambient temperature is optionally subjected to heat treatment at a temperature of between 300 ° C. and 450 ° C. for a period of between 30 minutes and 120 minutes; then
- on réalise l'usinage des pièces. - We perform the machining parts.
Dans un mode de réalisation préféré, on réalise le traitement thermique de revenu afin de garantir l'obtention de très bonnes propriétés des pièces après refroidissement. In a preferred embodiment, the heat treatment of income is carried out to ensure the obtaining of very good properties of the parts after cooling.
Pour mieux illustrer l'invention, des essais ont été réalisés sur trois nuances. Essais To better illustrate the invention, tests were performed on three shades. testing
Les compositions chimiques des aciers utilisés lors des tests ont été rassemblées dans le tableau 1. La température de réchauffage de ces nuances a été de 1250°C. La température de fin de mise en forme à chaud a été de 1220°C.The chemical compositions of the steels used in the tests were collated in Table 1. The reheating temperature of these grades was 1250 ° C. The end temperature of hot shaping was 1220 ° C.
Les vitesses de refroidissement Vr600 et Vr400 sont indiquées dans le tableau 2.Cooling rates Vr600 and Vr400 are shown in Table 2.
Les pièces ont été refroidies entre 380 et la température ambiante à 0, 15°C/s puis usinées. Les conditions de réalisation des essais et les résultats des mesures de caractérisation ont été rassemblés dans le tableau 2. Tableau 1 The parts were cooled between 380 and ambient temperature to 0, 15 ° C / s and then machined. The conditions for carrying out the tests and the results of the characterization measurements have been compiled in Table 2. Table 1
Tableau 2 Table 2
Les résultats de ces essais ont été représentés graphiquement sous forme de 4 figures. La figure 1 montre la variation de la résistance mécanique à la rupture Rm en fonction de la vitesse de refroidissement Vr600 pour les nuances A et B. La figure 2 montre la variation de la limite élastique Re en fonction de la vitesse de refroidissement Vr600 pour les nuances A et B. The results of these tests have been graphically represented as 4 figures. FIG. 1 shows the variation of the mechanical resistance to rupture Rm as a function of the cooling rate Vr600 for the grades A and B. FIG. 2 shows the variation of the elastic limit Re as a function of the cooling speed Vr600 for the shades A and B.
On constate que la nuance selon l'invention présente une grande stabilité de ses propriétés mécaniques lorsque les conditions de refroidissement varient. La nuance est donc beaucoup plus robuste face aux variations de conditions de procédé que les nuances selon l'art antérieur.  It is found that the grade according to the invention has a high stability of its mechanical properties when the cooling conditions vary. The grade is therefore much more robust to variations in process conditions than grades according to the prior art.
Par ailleurs, la figure 3 montre le delta de la résistance mécanique à la rupture Rm en fonction du critère S1 pour les nuances A, B et C. De même, la figure 4 montre le delta de la limite élastique Re en fonction du critère S1 pour les nuances A, B et C.  Furthermore, FIG. 3 shows the delta of the mechanical strength at break Rm as a function of the criterion S1 for the grades A, B and C. Similarly, FIG. 4 shows the delta of the elastic limit Re as a function of the criterion S1. for grades A, B and C.
On constate que la sensibilité aux conditions de refroidissement est d'autant plus faible que la valeur de S1 est élevée.  It is found that the sensitivity to the cooling conditions is even lower than the value of S1 is high.
L'invention sera notamment utilisée avec profit pour la fabrication de pièces formées à chaud et en particulier, forgées à chaud, pour applications dans les véhicules terrestres à moteur. Elle trouve également des applications dans la fabrication de pièces pour bateaux ou dans le domaine de la construction, notamment pour la fabrication de barres vissables pour coffrages. The invention will notably be used with advantage for the manufacture of hot formed parts and in particular, hot forged, for applications in land motor vehicles. It also finds applications in the manufacture of parts for boats or in the field of construction, in particular for the manufacture of screw bars for formwork.
D'une façon générale, l'invention pourra être mise en œuvre pour la fabrication de tous types de pièces nécessitant d'atteindre les propriétés visées  In general, the invention can be implemented for the manufacture of all types of parts requiring to achieve the properties referred to

Claims

REVENDICATIONS
1- Pièce dont la composition comprend, les teneurs étant exprimées en  1- Part whose composition includes, the contents being expressed in
pourcentage en poids,  percentage by weight,
0,10<C<0,30  0.10 <C <0.30
1,6 < Mn <2,1  1.6 <Mn <2.1
0,5<Cr< 1,7  0.5 <Cr <1.7
0,5 < Si < 1,0  0.5 <If <1.0
0,065 <Nb< 0,15  0.065 <Numbers <0.15
0,0010≤'B≤ 0,0050 0.0010≤ ' B≤ 0.0050
0,0010≤N≤ ,0,0.130  0.0010≤N≤, 0.0.130
0 < Al < 0,060  0 <Al <0.060
0 < Mo < 1,00  0 <Mo <1.00
0 < Ni < 1,0  0 <Ni <1.0
0,01 <Ti<0,07  0.01 <Ti <0.07
0<V<0,3  0 <V <0.3
0<P< 0,050  0 <P <0.050
0,01 <S< 0,1  0.01 <S <0.1
0<Cu<0,5  0 <Cu <0.5
0 < Sn < 0,1  0 <Sn <0.1
le reste de la composition étant constitué de fer et d'impuretés inévitables résultant de l'élaboration, la microstructure étant constituée, en proportions surfaciques, de 100 à 70 % de bainite, de moins de 30% d'austénite résiduelle et de moins de 5% de ferrite. the remainder of the composition consisting of iron and unavoidable impurities resulting from the preparation, the microstructure being constituted, in surface proportions, of 100 to 70% of bainite, of less than 30% of residual austenite and of less than 5% ferrite.
2- Pièce selon la revendication 1, dont les teneurs en niobium, vanadium, molybdène, titane et aluminium sont telles que :  2- part according to claim 1, the contents of niobium, vanadium, molybdenum, titanium and aluminum are such that:
0,1 <S1 <0,4  0.1 <S1 <0.4
avec S1 = Nb + V + Mo + Ti + Al  with S1 = Nb + V + Mo + Ti + Al
3- Pièce selon la revendication 2, dont les teneurs en carbone, azote, chrome, silicium, manganèse, soufre et nickel sont telles que : 0,5 <S2<1,8  3- part according to claim 2, the contents of carbon, nitrogen, chromium, silicon, manganese, sulfur and nickel are such that: 0.5 <S 2 <1.8
0,7 <S3<1,6 0,3 < S4 < 1 ,5 0.7 <S3 <1.6 0.3 <S4 <1, 5
avec S2= C + N +Cr/2+(S1)/6 + (Si + Mn - 4 * S) /10 + Ni/20 S3= S2 + 1/3 x Vr600 S4 = S3 - Vr400 with S2 = C + N + Cr / 2 + (S1) / 6 + (Si + Mn - 4 * S) / 10 + Ni / 20 S3 = S2 + 1/3 x Vr600 S4 = S3 - Vr400
Vr400 et Vr600 étant exprimées en °C/s, Vr400 représentant la vitesse de refroidissement de la pièce dans l'intervalle de température entre 420 et 380°C et Vr600 représentant la vitesse de refroidissement de la pièce dans l'intervalle de température entre 620 et 580°C. Vr400 and Vr600 being expressed in ° C / s, Vr400 representing the cooling rate of the part in the temperature range between 420 and 380 ° C and Vr600 representing the cooling rate of the part in the temperature range between 620 and 620. and 580 ° C.
4- Pièce selon l'une quelconque des revendications précédentes, dont la composition comprend, la teneur étant exprimée en pourcentage en poids 4. Part according to any one of the preceding claims, the composition of which comprises the content being expressed as a percentage by weight.
0, 15 < C < 0,27 0, 15 <C <0.27
5- Pièce selon l'une quelconque des revendications précédentes, dont la composition comprend, la teneur étant exprimée en pourcentage en poids 5. Part according to any one of the preceding claims, the composition of which comprises the content being expressed as a percentage by weight.
1 ,7 < Mn < 2,0 1, 7 <Mn <2.0
6- Pièce selon l'une quelconque des revendications précédentes dont la composition comprend, la teneur étant exprimée en pourcentage en poids 6. Part according to any one of the preceding claims, the composition of which comprises the content being expressed as a percentage by weight
1 ,0% < Cr < 1 ,5 7- Pièce selon l'une quelconque des revendications précédentes dont la composition comprend, la teneur étant exprimée en pourcentage en poids : 1.0% <Cr <1, 5. Part according to any one of the preceding claims, the composition of which comprises the content being expressed as a percentage by weight:
0,75< Si < 0,9 0.75 <Si <0.9
8- Pièce selon l'une quelconque des revendications précédentes dont la composition comprend, la teneur étant exprimée en pourcentage en poids : 0,065 < Nb < 0, 1 10 8- part according to any one of the preceding claims whose composition comprises, the content being expressed as a percentage by weight: 0.065 <Nb <0, 1 10
9- Pièce selon l'une quelconque des revendications précédentes dont la composition comprend, la teneur étant exprimée en pourcentage en poids : 9- part according to any one of the preceding claims whose composition comprises, the content being expressed as a percentage by weight:
0,0020 < B < 0,0030 10- Pièce selon l'une quelconque des revendications précédentes dont la composition comprend, la teneur étant exprimée en pourcentage en poids : 0.0020 <B <0.0030 10- part according to any one of the preceding claims whose composition comprises, the content being expressed as a percentage by weight:
1 1- Pièce selon l'une quelconque des revendications précédentes dont la composition comprend, la teneur étant exprimée en pourcentage en poids :  1-piece according to any one of the preceding claims whose composition comprises, the content being expressed as a percentage by weight:
0,003≤ Al≤ 0,015 0.003≤ Al≤ 0.015
12- Pièce selon l'une quelconque des revendications précédentes dont la composition comprend, la teneur étant exprimée en pourcentage en poids : 12- part according to any one of the preceding claims whose composition comprises, the content being expressed as a percentage by weight:
0 < Ni < 0,55 13- Pièce selon l'une quelconque des revendications précédentes dont la composition comprend, la teneur étant exprimée en pourcentage en poids : 0 <Ni <0.55 13- Part according to any one of the preceding claims, the composition of which comprises the content being expressed as a percentage by weight:
0 < V < 0,2 0 <V <0.2
14- Pièce selon l'une quelconque des revendications précédentes dont la composition comprend, la teneur étant exprimée en pourcentage en poids : 0,03 < Mo < 0,15 14- part according to any one of the preceding claims whose composition comprises, the content being expressed as a percentage by weight: 0.03 <Mo <0.15
15 - Pièce selon l'une quelconque des revendications précédentes dont la structure comporte 0% de ferrite. 15 - part according to any preceding claim whose structure comprises 0% ferrite.
16 - Procédé de fabrication d'une pièce en acier comprenant les étapes successives suivantes : - on approvisionne un acier de composition selon l'une quelconque des revendications 1 à 14 sous forme de bloom, de billette de section carrée rectangle ou ronde , ou sous forme de lingot, puis 16 - A method of manufacturing a steel part comprising the following successive steps: - supplying a steel composition according to any one of claims 1 to 14 in the form of a bloom, billet square section rectangle or round, or under ingot shape, then
- on lamine cet acier sous forme de demi-produit, sous forme de barre ou de fil puis - on porte ledit demi-produit à une température de réchauffage (TreCh) comprise entre 1 100°C et 1300°C pour obtenir un demi-produit réchauffé, puis - on met en forme à chaud ledit demi-produit réchauffé, la température de fin de mise en forme à chaud étant supérieure ou égale à 850°C pour obtenir une pièce formée à chaud, puis, this steel is rolled in the form of a semi- finished product, in the form of a bar or wire, and then said semi- finished product is heated to a reheating temperature (T reC h) of between 1100 ° C. and 1300 ° C. in order to obtain half-product warmed up, then said heated half-product is hot-shaped, the hot-forming end temperature being greater than or equal to 850 ° C. to obtain a hot-formed part, and then,
- on refroidit ladite pièce formée à chaud jusqu'à atteindre une température comprise entre 620 et 580°C à une vitesse de refroidissement Vr600 comprise entre 0,10 °C/s et 10 °C/s puis  said hot-formed part is cooled to a temperature of between 620 and 580 ° C. at a cooling rate Vr600 of between 0.10 ° C./s and 10 ° C./s.
- on refroidit ladite pièce jusqu'à atteindre une température comprise entre 420 et 380°C à une vitesse de refroidissement Vr400 inférieure à 4°C/s, puis  said part is cooled to a temperature of between 420 and 380 ° C. at a cooling rate Vr400 of less than 4 ° C./s, and then
- on refroidit la pièce entre 380 °C et 300°C à une vitesse inférieure ou égale à 0,3 °C/s, puis  the part is cooled between 380 ° C. and 300 ° C. at a speed less than or equal to 0.3 ° C./s, and then
- on refroidit la pièce jusqu'à la température ambiante à une vitesse inférieure ou égale à 4°C/s, puis,  the part is cooled to ambient temperature at a speed of less than or equal to 4 ° C./s, then
- on fait éventuellement subir un traitement thermique de revenu à ladite pièce formée à chaud et refroidie jusqu'à l'ambiante, à une température de revenu comprise entre 300 °C et 450°C pendant une durée comprise entre 30 minutes et 120 minutes, puis  the heat-formed part which is cooled down to ambient temperature is optionally subjected to heat treatment at a temperature of between 300 ° C. and 450 ° C. for a period of between 30 minutes and 120 minutes; then
- on réalise l'usinage des pièces.  - We perform the machining parts.
EP16718723.6A 2015-03-23 2016-03-23 Parts with a bainitic structure having high strength properties and manufacturing process Active EP3274483B1 (en)

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KR (1) KR101887844B1 (en)
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AU (1) AU2016238510B2 (en)
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FR3123659A1 (en) 2021-06-02 2022-12-09 Ascometal France Holding Sas Hot-formed steel part and method of manufacture
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CN107371369B (en) 2019-06-21
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CN107371369A (en) 2017-11-21
PL3274483T3 (en) 2020-01-31
AU2016238510A1 (en) 2017-10-12
US20180057909A1 (en) 2018-03-01
ES2748436T3 (en) 2020-03-16
BR112017020282B1 (en) 2021-08-17
MX2017012242A (en) 2017-12-15
CA2980878A1 (en) 2016-09-29
US12129527B2 (en) 2024-10-29
KR20170118916A (en) 2017-10-25
BR112017020282A2 (en) 2018-06-05
WO2016151345A1 (en) 2016-09-29
JP6625657B2 (en) 2019-12-25
EP3274483B1 (en) 2019-07-24
EA201792077A1 (en) 2018-01-31
CA2980878C (en) 2020-01-14
UA118920C2 (en) 2019-03-25
WO2016151390A1 (en) 2016-09-29
HUE045789T2 (en) 2020-01-28

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