Classifications

• • 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
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
  • C22C38/44—Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
• • 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
  • C21D6/004—Heat treatment of ferrous alloys containing Cr and Ni
• • 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
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
  • C22C38/46—Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
• • C—CHEMISTRY; METALLURGY
  • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
  • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
  • C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
  • C23C8/06—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases
  • C23C8/08—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases only one element being applied
  • C23C8/20—Carburising
  • C23C8/22—Carburising of ferrous surfaces
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
  • F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
  • F02M61/16—Details not provided for in, or of interest apart from, the apparatus of groups F02M61/02 - F02M61/14
  • F02M61/166—Selection of particular materials
• • 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
  • C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
  • C21D1/18—Hardening; Quenching with or without subsequent tempering
• • 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
  • C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
  • C21D1/26—Methods of annealing
  • C21D1/28—Normalising

Definitions

• the present invention relates to a composition of case-hardening steel, parts formed with this steel, as well as a method for manufacturing parts made from this steel.
• Case hardening is a surface thermochemical treatment generally intended to obtain parts combining good core ductility and a hard, hardened and wear resistant surface.
• the cementing steels usually used for these applications are, in particular, 17CrNiMo6, 16NiCr6, 14NiCr12, 10NiCrMo13, 16NiCrMo13 or 17NiCrMo17. These steels can be used up to operating temperatures in the region of 130 ° C, but have neither a softening resistance nor a hot hardness of the cemented layer sufficient for operating temperatures exceeding 190 ° C.
• the cemented layer allows a tempering temperature up to about 260 ° C.
• the maximum operating temperature is around 230 ° C.
• none of the cementation steel compositions of the prior art makes it possible to achieve a tempering temperature of the cemented layer of up to 350 ° C., as well as good hot hardness for operating temperatures of up to 'at 280 ° C, while retaining satisfactory core characteristics.
• the main object of the present invention is therefore to provide a cementation steel composition making it possible to achieve all of the above characteristics.
• a first object of the invention is thus a composition of case-hardening steel comprising, expressed by weight,
• Sulfur is preferably limited to 0.010% and phosphorus to 0.020% by weight for high-end applications, but higher contents are however acceptable for other applications, insofar as they do not cause reduction of the ductility, toughness and fatigue resistance properties of steel.
• Elements such as aluminum, cerium, titanium, zirconium, calcium, niobium, which serve either to deoxidize or to refine the grain size are preferably limited to 0.1% by weight each.
• the low contents of carbon, silicon, molybdenum, chromium and vanadium, as well as the high contents of manganese, nickel, cobalt and copper allow improve the ductility and toughness properties of steel.
• the high contents of carbon, silicon, molybdenum, chromium and vanadium as well as the low contents of manganese, nickel, cobalt and copper make it possible to improve the resistance to tempering of steel.
• the role of carbon is essentially to contribute to obtaining hardness, tensile strength and hardenability.
• the hardness and the tensile strength obtained at the core of the case-hardened and treated parts are insufficient.
• the minimum tensile strength sought is approximately 1000 MPa, or approximately 320 HV (Vickers hardness).
• Silicon contributes to a large extent to the resistance to tempering of this steel and its minimum content is 0.5% by weight. In order to avoid the formation of delta ferrite and to maintain sufficient toughness, the silicon content is limited to a maximum of 1.5% by weight. The optimal range is 0.7-1.3% by weight, but the range 1.3-3.5% is also interesting.
• Chromium contributes in part to the hardenability of the core and to the good resistance to tempering of the cemented layer, its minimum content is 0.2% by weight. To avoid embrittlement of the cemented layer by excess of networked carbides, the chromium content must be limited to a maximum value of 1.5% by weight. The optimal range is 0.5-1.2%, but the 0.2-0.8% and 0.8-1.5% ranges are also attractive. Molydbene plays a role identical to that of chromium, and it also makes it possible to maintain a high hot hardness, in particular by the formation of intragranular carbides in the cemented layer. Its minimum content is 1.1% by weight. However, its embrittling effect on this steel leads to limiting its maximum content to 3.5% by weight. The optimal range is 1.5-2.5%, but the ranges 1, 1-2.3% and 2.3-3.5% are also interesting.
• Vanadium helps limit grain magnification during the case hardening and processing cycles. Because of its embrittling effect and its influence on the formation of ferrite, its content must be limited to a maximum value of 0.4% by weight. The optimal range is 0.15-0.35% but the ranges 0.05-0.25% and 0.25-0.4% are also interesting.
• Manganese, nickel and copper are gamma elements necessary to balance the chemical composition, avoid the formation of ferrite and limit the temperature of the ⁇ ⁇ transformation points. They also greatly contribute to increasing the hardenability, resilience and toughness but, in too high a content, they deteriorate the income resistance, the hot hardness and the wear resistance and increase the amount of residual austenite in the layer. case-hardened.
• Manganese is therefore limited to a maximum of 1.6% by weight.
• the optimal range is 0.2-0.7% by weight, but the range 0.7-1.5% is also interesting.
• nickel is limited to the range 1-3.5% by weight, the optimal range is 2-3%, but the ranges 1-2% and 2-3.5% are also interesting.
• copper is limited to a maximum of 2% by weight, the optimal range is 0.3-1.1%, but the range 1.1-2% can also be interesting.
• Cobalt contributes to the income resistance of the steel and makes it possible to lower the transformation point on heating. Its effect is noticeable even at low contents. For high contents this element, by its gammagenic character, stabilizes the residual austenite in the cemented layer.
• the maximum limit is 4% by weight, contents of less than 1.5% by weight being recommended.
• a second object of the invention is a method of manufacturing cemented and treated parts comprising the following operations: a - constitution of a charge intended to obtain a composition in accordance with the present invention, as described above, b - fusion of said charge in an arc furnace, c - thermomechanical heating and transformation of the ingot, d - heat treatment for homogenizing the structure and refining of the grain, e - carburizing, and f - heat treatment for use.
• the steel according to the invention can be obtained by conventional production techniques but, to obtain better results in resilience, tenacity and fatigue, it is recommended to carry out a reflow by a consumable electrode, either under slag (ESR) or under reduced pressure (VAR), following melting in the arc furnace.
• ESR slag
• VAR reduced pressure
• VIM reduced pressure
• thermomechanical transformations aiming to confer on the product produced in this alloy a sufficient rate of wrinkling which one prefer greater than or equal to 3 (step c of the method according to the invention). Lower working rates may however be allowed for large parts.
• thermomechanical transformations are based on conventional procedures, such as rolling, forging, stamping or spinning.
• step d of the method according to the invention can simply be softened at a temperature below the critical point (AC-i), or annealed at a temperature above the critical point (AC-i), which then assumes a sufficiently slow start of cooling.
• the critical point temperature (AC-i) is generally in the range from 700 to 800 ° C, while the critical point temperature (AC 3 ) is generally in the range from 900 to 980 ° C.
• the case hardening, step e of the process according to the invention can be carried out using conventional means, the case hardening cycle being to be defined by the skilled person as a function of the depth hardening sought, in a completely conventional manner.
• stage f of the heat treatment of the use of the parts numerous alternative embodiments are possible. It is possible to go directly from the case temperature to the austenitization temperature, then to soak the parts, but it is preferable to allow the parts to cool to room temperature after case hardening, then to heat them up to the temperature austenitization, above the critical point (AC 3 ) before soaking.
• the austenitization temperature range is, for information, 900-1050 ° C.
• tempering In order to obtain the maximum values of hardness of the cemented layer, and of resilience and toughness of the sub-layer, it is preferable to carry out tempering at the lowest possible temperature, compatible with the temperature of use. A difference of 50 ° C. between tempering temperature and use temperature is more particularly preferred, the tempering temperature possibly reaching up to 350 ° C.
• the continuous casting technique can be used in order to reduce the production costs and we must then expect a lowering of the characteristics of ductility, resilience and toughness, especially.
• a third object of the invention is constituted by the case-hardened and treated parts produced with the case-hardening steel according to the invention and which exhibit, at ambient temperature, a hardness with a core close to 320 to 460 HV, an resilience ISO V d '' at least 50 Joules, and more particularly from 70 to 150 Joules, a toughness close to 100 MPaVm, a surface hardness of the cemented layer close to 750 HV, and which, at 250 ° C, has a surface hardness of the cemented layer close to 650 HV.
• These parts can advantageously be manufactured by means of the manufacturing method according to the invention, but also by any other method chosen according to the final application.
• FIG. 1 represents the variations in microhardness as a function of the depth for two samples, the preparation of which is described in example 1,
• FIG. 2 represents the variations in microhardness as a function of the depth for two samples, the preparation of which is described in example 2
• FIG. 3 represents the variations in microhardness as a function of the depth for two samples, the preparation of which is described in example 3,
• FIG. 4 represents the variations in microhardness as a function of the depth for two samples, the preparation of which is described in example 4,
• FIG. 7 represents the variations in microhardness as a function of the depth for three samples, the preparation of which is described in Example 8.
• a 35 kg ingot was produced in the chemical composition indicated in percentage by weight below, in accordance with the indications of the present invention:
• This ingot was produced by arc fusion, it was then homogenized at high temperature to give a uniform structure, then it was forged.
• the forged products were slowly cooled in the oven. They have been standardized in order to dissolve carbides, to homogenize the austenitic structure and to refine the grain.
• Bars resulting from this invention were austenitized at 940 ° C., soaked in oil, passed through the cold in a cryogenic enclosure regulated at -75 ° C., then returned to a temperature of 250 ° C.
• a 35 kg ingot was produced in the chemical composition indicated in percentage by weight below, in accordance with the indications of the present invention:
• This ingot was produced by arc fusion and was then homogenized at high temperature to obtain a uniform structure, then it was forged.
• the forged products were slowly cooled in the oven. They have been standardized in order to dissolve the carbides, to homogenize the austenitic structure and to refine the grain.
• Bars from these treatments were austenitized at 940 ° C, soaked in oil, cold passed in a cryogenic chamber regulated to -75 ° C, then returned to a temperature of 250 ° C.
• Figure 2 shows the results obtained for tempering temperatures of 150 ° C and 350 ° C.
• a 35 kg ingot was produced in the chemical composition indicated in percentage by weight below, in accordance with the indications of the present invention:
• This ingot was produced by arc fusion, it was then homogenized at high temperature to obtain a uniform structure, then it was forged.
• the forged products were slowly cooled in the oven. they have have been standardized to dissolve carbides, homogenize the austenitic structure and refine the grain.
• Bars resulting from this invention were austenitized at 940 ° C., soaked in oil, passed through the cold in a cryogenic enclosure regulated at -75 ° C., then returned to a temperature of 250 ° C.
• a 35 kg ingot was produced in the chemical composition indicated in percentage by weight below, in accordance with the indications of the present invention:
• This ingot was produced by arc fusion, it was then homogenized at high temperature to obtain a uniform structure, then it was forged.
• the forged products were slowly cooled in the oven. They have been standardized in order to dissolve the carbides, to homogenize the austenitic structure and to refine the grain.
• Bars from these treatments were austenitized at 940 ° C, soaked in oil, cold passed in a cryogenic chamber regulated to -75 ° C, then returned to a temperature of 250 ° C.
• Figure 4 shows the results obtained for tempering temperatures of 150 ° C and 350 ° C.
• a 35 kg ingot was produced in the chemical composition indicated in percentage by weight below, in accordance with the indications of the present invention:
• This ingot was produced by arc fusion, it was then homogenized at high temperature to obtain a uniform structure, then it was forged.
• the forged products were slowly cooled in the oven. they have have been standardized in order to dissolve the carbides, to homogenize the austenitic structure and to refine the grain.
• Bars from these treatments were austenitized at 960 ° C, soaked in oil, passed through the cold in a cryogenic chamber regulated at -75 ° C, then returned to a temperature of 250 ° C.
• a 35 kg ingot was produced in the chemical composition indicated in percentage by weight below, in accordance with the indications of the present invention:
• This ingot was produced by arc fusion, it was then homogenized at high temperature to obtain a uniform structure, then it was forged.
• the forged products were slowly cooled in the oven. They have been standardized in order to dissolve the carbides, to homogenize the austenitic structure and to refine the grain.
• Bars from these treatments were austenitized at 960 ° C, soaked in oil, passed through the cold in a cryogenic chamber regulated at -75 ° C, then returned to a temperature of 250 ° C.
• a 1000 kg ingot was prepared in accordance with the present invention, its chemical composition, expressed as a percentage by weight, being as follows:
• This ingot was obtained by partial pressure induction melting (VIM), then reflow by consumable electrode, it was then reheated to high temperature, in order to homogenize the structure, then it was laminated. to end up with 90 mm diameter cylindrical bars. These bars have undergone a standardization treatment, in order to dissolve the carbides, homogenize the austenitic structure and refine the grain size.
• VIP partial pressure induction melting
• Samples taken from these bars were cemented using a low pressure process at a temperature of around 900 ° C for 8 hours, the samples intended to characterize the core properties underwent an identical thermal cycle, but in a neutral atmosphere , so as not to modify their chemical composition.
• the following table indicates the evolution of the surface hardness of the cemented layer as a function of the test temperature, on a sample which has undergone tempering at 300 ° C.
• Figure 7 shows the results obtained for tempering temperatures of 150 ° C, 200 ° C and 300 ° C.
• the preceding eight examples show, on the one hand, that the steels according to the invention exhibit an excellent compromise between the characteristics of traction, resilience and toughness and, on the other hand, that the cemented layer has a high resistance to tempering. , as well as high values of hot hardness, significantly higher than those obtained with traditional case hardening steels.

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• Heat Treatment Of Articles (AREA)
• Heat Treatment Of Steel (AREA)
• Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)

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• 1998
  • 1998-06-29 FR FR9808247A patent/FR2780418B1/fr not_active Expired - Fee Related
• 1999
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