EP4653565A1 - Austenitic stainless steel material - Google Patents

Austenitic stainless steel material

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Publication number
EP4653565A1
EP4653565A1 EP24744646.1A EP24744646A EP4653565A1 EP 4653565 A1 EP4653565 A1 EP 4653565A1 EP 24744646 A EP24744646 A EP 24744646A EP 4653565 A1 EP4653565 A1 EP 4653565A1
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EP
European Patent Office
Prior art keywords
less
content
stainless steel
austenitic stainless
steel material
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
EP24744646.1A
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German (de)
French (fr)
Other versions
EP4653565A4 (en
Inventor
Kana JOTOKU
Takahiro Osuki
Shinnosuke KURIHARA
Takahiro Izawa
Kiyoko Takeda
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Nippon Steel Corp
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Nippon Steel Corp
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Publication of EP4653565A1 publication Critical patent/EP4653565A1/en
Publication of EP4653565A4 publication Critical patent/EP4653565A4/en
Pending legal-status Critical Current

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    • CCHEMISTRY; METALLURGY
    • 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
    • C21D9/46Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
    • CCHEMISTRY; METALLURGY
    • 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
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/004Heat treatment of ferrous alloys containing Cr and Ni
    • CCHEMISTRY; METALLURGY
    • 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
    • C21D8/00Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C30/00Alloys containing less than 50% by weight of each constituent
    • C22C30/04Alloys containing less than 50% by weight of each constituent containing tin or lead
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/001Ferrous alloys, e.g. steel alloys containing N
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/004Very low carbon steels, i.e. having a carbon content of less than 0,01%
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/008Ferrous alloys, e.g. steel alloys containing tin
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/02Ferrous alloys, e.g. steel alloys containing silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/04Ferrous alloys, e.g. steel alloys containing manganese
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/34Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • 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
    • C22C38/42Ferrous alloys, e.g. steel alloys containing chromium with nickel with copper
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • 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
    • C22C38/44Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • 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
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • 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
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • 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
    • C22C38/50Ferrous alloys, e.g. steel alloys containing chromium with nickel with titanium or zirconium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • 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
    • C22C38/52Ferrous alloys, e.g. steel alloys containing chromium with nickel with cobalt
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • 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
    • C22C38/54Ferrous alloys, e.g. steel alloys containing chromium with nickel with boron
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • 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
    • C22C38/58Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C8/00Solid 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
    • C23C8/06Solid 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
    • C23C8/08Solid 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
    • C23C8/24Nitriding
    • C23C8/26Nitriding of ferrous surfaces
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C8/00Solid 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
    • C23C8/80After-treatment
    • CCHEMISTRY; METALLURGY
    • 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

Definitions

  • Austenitic stainless steel materials are excellent in strength and corrosion resistance, and are used for various applications. For this reason, for example, as disclosed in Patent Document 1, austenitic stainless steel materials with enhanced wear resistance have been developed.
  • Patent Document 1 JP5-222512A
  • Patent Document 1 discloses an austenitic stainless steel material which is subjected to a heat treatment in a nitrogen atmosphere (hereinafter, also referred to as "nitridation treatment") to harden the surface and thereby improve its properties.
  • nitridation treatment is sometimes performed, for example, after a certain amount of processing has been performed, in order to make it difficult for scratches to occur during transportation and the like.
  • microcracks small cracks occur from the hardened surface (hereinafter, referred to simply as "microcracks") in the austenitic stainless steel material. Such microcracks are undesirable in terms of the appearance and performance of the product.
  • an austenitic stainless steel material is required to have weldability.
  • the weldability may decrease. In other words, it is generally difficult to both suppress microcracks and also improve weldability.
  • an austenitic stainless steel material in which microcracks are suppressed and which has good weldability even when subjected to processing before and after nitridation treatment is obtained.
  • the present inventors have conducted various studies directed at improving weldability while suppressing the microcracks described above, and obtained the findings described in (a) to (c) below.
  • C carbon
  • C has an effect of improving strength.
  • C has an effect of suppressing formation of a nitridation layer. Therefore, the content of C is 0.010% or more.
  • the content of C is preferably 0.020% or more, and more preferably is 0.030% or more.
  • the content of C is 0.15% or less.
  • the content of C is preferably 0.12% or less, and more preferably is 0.10% or less.
  • Si silicon is an element that has a deoxidizing effect. In addition, Si has an effect of suppressing formation of a nitridation layer. Therefore, the content of Si is 0.10% or more.
  • the content of Si is preferably 0.12% or more, more preferably is 0.15% or more, and further preferably is 0.20% or more. However, if Si is excessively contained, weldability will decrease. Therefore, the content of Si is 2.00% or less.
  • the content of Si is preferably 1.70% or less, more preferably is 1.40% or less, and further preferably is 1.00% or less.
  • P phosphorus
  • P is an impurity element contained in the steel. P reduces mechanical properties such as strength and toughness. Therefore, the content of P is 0.060% or less.
  • the content of P is preferably 0.050% or less. Although it is preferable to reduce the content of P as much as possible, excessive reduction of P will increase the refining cost. Therefore, the content of P is preferably 0.005% or more.
  • S sulfur is an impurity element contained in the steel. S reduces mechanical properties such as strength and toughness. Therefore, the content of S is 0.010% or less. The content of S is preferably 0.0050% or less. Although it is preferable to reduce the content of S as much as possible, excessive reduction of S will increase the refining cost. Therefore, the content of S is preferably 0.0001% or more.
  • N nickel is an element that stabilizes austenite. Further, N has an effect of improving strength. In addition, N has an effect of suppressing formation of a nitridation layer. Therefore, the content of Ni is 16.0% or more. The content of Ni is preferably 16.5% or more, more preferably is 17.0% or more, and further preferably is 18.0% or more. However, if Ni is excessively contained, weldability and hot workability will decrease. Therefore, the content of Ni is 25.0% or less. The content of Ni is preferably 24.8% or less, more preferably is 24.5% or less, and further preferably is 24.0% or less.
  • Cr Cr (chromium) has an effect of increasing corrosion resistance. Therefore, the content of Cr is 20.0% or more.
  • the content of Cr is preferably 21.0% or more, more preferably is 21.5% or more, and further preferably is 22.0% or more. However, if Cr is excessively contained, weldability will decrease. Therefore, the content of Cr is 29.0% or less.
  • the content of Cr is preferably 28.0% or less, more preferably is 27.5% or less, and further preferably is 27.0% or less.
  • Mo mobdenum
  • the content of Mo is 0.08% or more.
  • the content of Mo is preferably 0.10% or more, more preferably is 0.12% or more, and further preferably is 0.15% or more.
  • the content of Mo is 1.0% or less.
  • the content of Mo is preferably 0.95% or less, more preferably is 0.90% or less, and further preferably is 0.85% or less.
  • Sn (tin) has an effect of increasing corrosion resistance. Further, Sn also has an effect of increasing weldability. Therefore, the content of Sn is 0.001% or more.
  • the content of Sn is preferably 0.0015% or more, more preferably is 0.002% or more, and further preferably is 0.003% or more. However, if Sn is excessively contained, hot workability will decrease. Therefore, the content of Sn is 0.080% or less.
  • the content of Sn is preferably 0.075% or less, more preferably is 0.070% or less, and further preferably is 0.060% or less.
  • N nitrogen
  • the content of N is preferably 0.015% or more, more preferably is 0.020% or more, and further preferably is 0.030% or more.
  • the content of N is 0.15% or less.
  • the content of N is preferably 0.14% or less, more preferably is 0.13% or less, and further preferably is 0.12% or less.
  • Co is an important element in a steel plate of the present embodiment, and has an effect of suppressing formation of a nitridation layer. Therefore, the content of Co is 0.001% or more.
  • the content of Co is preferably 0.005% or more, more preferably is 0.01% or more, and further preferably is 0.02% or more. However, if Co is excessively contained, the production cost will increase. Therefore, the content of Co is 1.50% or less.
  • the content of Co is preferably 1.30% or less, more preferably is 1.00% or less, and further preferably is 0.80% or less.
  • the chemical composition may also contain Nb within the range described below in lieu of a part of Fe. The reason for limiting the element is described below.
  • Nb (niobium) forms carbo-nitrides and has an effect of increasing corrosion resistance. Therefore, Nb may be contained as necessary. However, if Nb is excessively contained, mechanical properties such as toughness will decrease. Therefore, the content of Nb is 0.20% or less.
  • the content of Nb is preferably 0.15% or less, and more preferably is 0.10% or less.
  • the content of Nb is preferably 0.001% or more, more preferably is 0.005% or more, further preferably is 0.010% or more, and further preferably is 0.015% or more.
  • the chemical composition may also contain one or more kinds of element selected from Cu, V, Ti, Al, and B within the ranges described below in lieu of a part of Fe. The reasons for limiting each element are described below.
  • Cu copper stabilizes austenite and has an effect of improving strength. Therefore, Cu may be contained as necessary. However, if the content of Cu is excessive, hot workability will decrease. Therefore, the content of Cu is 1.0% or less.
  • the content of Cu is preferably 0.80% or less, and more preferably is 0.60% or less. On the other hand, in order to obtain the aforementioned advantageous effect, the content of Cu is preferably 0.001% or more.
  • V 0.30% or less
  • V vanadium
  • V vanadium
  • the content of V is preferably 0.25% or less, and more preferably is 0.20% or less.
  • the content of V is preferably 0.001% or more.
  • Ti titanium
  • Ti has an effect of improving the strength of the steel by forming carbo-nitrides. Therefore, Ti may be contained as necessary. However, if the content of Ti is excessive, toughness will decrease. Therefore, the content of Ti is 0.020% or less.
  • the content of Ti is preferably 0.015% or less, and more preferably is 0.010% or less. On the other hand, in order to obtain the aforementioned advantageous effect, the content of Ti is preferably 0.001% or more.
  • W tungsten
  • W dissolves in the parent phase and has an effect of improving the strength of the steel. Therefore, W may be contained as necessary. However, if the content of W is excessive, hot workability will decrease. Therefore, the content of W is 0.10% or less.
  • the content of W is preferably 0.08% or less, and more preferably is 0.05% or less. On the other hand, in order to obtain the aforementioned advantageous effect, the content of W is preferably 0.001% or more.
  • Al is an element that has a deoxidizing effect. Therefore, Al may be contained as necessary. However, if the content of Al is excessive, inclusions will excessively form and productivity will decrease. Therefore, the content of Al is 0.050% or less.
  • the content of Al is preferably 0.040% or less, and more preferably is 0.030% or less. On the other hand, in order to obtain the aforementioned advantageous effect, the content of Al is preferably 0.001% or more.
  • B (boron) forms intermetallic compounds at grain boundaries, and has an effect of increasing grain boundary strength. Therefore, B may be contained as necessary. However, if the content of B is excessive, hot workability will decrease. Therefore, the content of B is to be 0.050% or less.
  • the content of B is preferably 0.040% or less, and more preferably is 0.030% or less. On the other hand, in order to obtain the aforementioned advantageous effect, the content of B is preferably 0.0001% or more.
  • the balance is Fe and impurities.
  • impurities refers to components which, during industrial production of the steel, are mixed in from raw material such as ore or scrap or due to various causes during the production process, and which are allowed within a range that does not adversely affect the present embodiment.
  • Fl calculated by Formula (i) below is 7.5 to 20.0.
  • F 1 16.0 + 8.0 C + 2.4 Si ⁇ 0.5 Mn + 0.3 Ni ⁇ 0.9 Cr ⁇ 3.1 Mo + 119 N + 2.0 Co
  • each symbol of an element in the above formula represents the content (mass%) of a corresponding element contained in the austenitic stainless steel material, and is assigned a value of 0 if the corresponding element is not contained.
  • nitridation layer in which nitrogen is concentrated at the surface of the steel material grows too thick due to nitridation treatment, microcracks will form. Therefore, it is effective to cause nitrides, for example, CrN and the like, to form in order to reduce the thickness of the nitridation layer.
  • nitrides for example, CrN and the like
  • the above Formula (i) is an experimentally obtained relational expression with respect to C, Si, Mn, Ni, Cr, Mo, N, and Co, which are elements which affect the formation of nitrides
  • F1 is an index of the likelihood of microcracks occurring in a case where processing is performed before and after nitridation treatment.
  • F1 is 7.5 or more.
  • Fl is preferably 7.6 or more, more preferably is 7.7 or more, and further preferably is 7.8 or more.
  • F1 is 20.0 or less.
  • F1 is preferably 19.0 or less, more preferably is 18.0 or less, and further preferably is 17.0 or less.
  • Formula (ii) is an experimentally obtained formula. That is, Formula (ii) is a relational expression with respect to C, Si, Mn, Cr, Mo, Sn, and Nb which mutually affect weldability. If F2 is more than 320.0, weldability will decrease and cracks will easily occur after welding. Therefore, F2 is 320.0 or less. F2 is preferably 319.0 or less, more preferably is 318.0 or less, and further preferably is 317.0 or less. Note that, although a lower limit of F2 is not particularly limited, F2 will be 213.0 or more based on the ranges of the contents of the elements constituting Formula (ii).
  • the thickness of the aforementioned Cr depleted zone is to be measured by the following method.
  • a field emission electron probe microanalyzer FE-EPMA
  • FE-EPMA field emission electron probe microanalyzer
  • the measurement is to be performed under conditions of an acceleration voltage of 15 kV and an analysis diameter of 0.1 ⁇ m.
  • a region where the Cr concentration is 0.9 times or less for the content of Cr in the aforementioned austenitic stainless steel material is defined as a Cr depleted zone.
  • the shape of the austenitic stainless steel material of the present embodiment is not particularly limited.
  • the austenitic stainless steel material may be a steel plate, or may be a steel bar or wire rod.
  • the austenitic stainless steel material of the present embodiment is suitable for use in applications in which processing such as drawing is performed after nitridation treatment.
  • the austenitic stainless steel material of the present embodiment can be stably produced, for example, by the following production method.
  • the hot working is, for example, hot forging, hot extrusion, hot rolling or the like.
  • the shape may be, for example, a steel plate, a steel bar, a wire rod or the like. Note that, the conditions of the hot working are not particularly limited and may be adjusted as necessary. After the hot working, cold working may be performed as necessary.
  • the cold working is, for example, cold drawing or cold rolling.
  • a heat treatment is performed.
  • Well-known conditions can be used as the heat treatment conditions.
  • the steel material may be heated to a temperature range of 1060 to 1350°C, and thereafter rapidly cooled.
  • An atmosphere furnace is generally used when performing the heat treatment.
  • Steel types A to S having the chemical compositions shown in Table 1 were melted in a laboratory and subjected to hot forging to produce steel materials with a thickness of 20 mm. Thereafter, hot rolling was performed to a predetermined thickness to produce steel plates (austenitic stainless steel materials) of 1.25 mm and 7 mm in thickness.
  • the obtained steel plates were then subjected to a heat treatment in which the steel plates were heated to a temperature of 1060°C or more in an atmosphere furnace described in Table 2, followed by rapid cooling. For some of the steel plates, the thickness of a Cr depleted zone was measured in the as heat treatment condition. Thereafter, for steel type N which had been subjected to heat treatment using an atmosphere furnace, a descaling treatment was performed by pickling. Further, for all of the steel materials, evaluation of the occurrence of microcracks and evaluation of weldability were carried out by the methods described below.
  • microcracks The occurrence of microcracks was evaluated by a tensile test, and a subsequent structural observation and the like. Specifically, based on JIS Z 2241: 2022, a No. 5 test coupon specified in JIS was taken from each 1.25-mm thick steel plate. Strain was introduced into the test coupon by performing cold working so that the cold reduction ratio was 30% using a tensile testing machine. Thereafter, nitridation treatment was performed in which the test coupon was held at a heat treatment temperature of 1040°C for a heat treatment time of 30 minutes in a 100% nitrogen atmosphere, and then cooled with gas.
  • a tensile test was performed once more, and strain was introduced into the tensile test coupon by cold working so that the cold reduction ratio was 25%. At such time, strain was introduced in a manner so that the tensile test coupon did not rupture, and thereafter the surface of the test coupon was observed with a scanning microscope to check for the presence or absence of microcracks. At that time, the observation magnification was set to 500 ⁇ , and the number of visual fields was set to five visual fields. The number of visual fields in which cracks were observed is shown in Table 2. In the present Example, if the number of visual fields in which cracks were observed among the five visual fields was one or less, it was determined that the test coupon was acceptable.
  • Trans-Varestraint test refers to a test to examine cracking (solidification cracking) that occurs in a weld metal during welding.
  • GTAW Gas Tungsten Arc Welding
  • the maximum length of the occurred cracks was measured. The results are shown in Table 2. In the present Example, if the maximum length of the cracks was 1.00 mm or less, it was determined that the resistance to weld crack susceptibility was good. On the other hand, if the maximum length of the cracks was more than 1.00 mm, it was determined that the resistance to weld crack susceptibility was failed.
  • the content of N was low and, furthermore, the value of F1 was less than the specified value, and consequently the thickness of the nitridation layer was excessive and microcracks occurred.
  • the content of Cr was excessive, the value of F1 was less than the specified value and, in addition, the value of F2 was more than the specified value. As a result, microcracks occurred, and the weld crack resistance was inferior.

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Abstract

An austenitic stainless steel material having a chemical composition including, in mass%, C: 0.010 to 0.15%, Si: 0.10 to 2.00%, Mn: 0.10 to 3.00%, P: 0.060% or less, S: 0.010% or less, Ni: 16.0 to 25.0%, Cr: 20.0 to 29.0%, Mo: 0.08 to 1.0%, Sn: 0.001 to 0.080%, N: 0.010 to 0.15%, Co: 0.001 to 1.50%, Nb: 0 to 0.20%, and the balance: Fe and impurities, and in which F1 (= 16.0 + 8.0C + 2.4Si - 0.5Mn + 0.3Ni - 0.9Cr - 3.1Mo + 119N + 2.0Co) is 7.5 to 20.0, and F2 (= 286.2 + 337.9C + 23.9Si - 2.7Mn + 0.1Cr - 15.5Mo + 339.4Sn - 286.9Nb) is 320.0 or less.

Description

    TECHNICAL FIELD
  • The present invention relates to an austenitic stainless steel material.
  • BACKGROUND ART
  • Austenitic stainless steel materials are excellent in strength and corrosion resistance, and are used for various applications. For this reason, for example, as disclosed in Patent Document 1, austenitic stainless steel materials with enhanced wear resistance have been developed.
  • LIST OF PRIOR ART DOCUMENT PATENT DOCUMENT
  • Patent Document 1: JP5-222512A
  • SUMMARY OF INVENTION TECHNICAL PROBLEM
  • Patent Document 1 discloses an austenitic stainless steel material which is subjected to a heat treatment in a nitrogen atmosphere (hereinafter, also referred to as "nitridation treatment") to harden the surface and thereby improve its properties. Such nitridation treatment is sometimes performed, for example, after a certain amount of processing has been performed, in order to make it difficult for scratches to occur during transportation and the like.
  • However, when it is necessary to perform further processing such as drawing thereafter, in some cases small cracks occur from the hardened surface (hereinafter, referred to simply as "microcracks") in the austenitic stainless steel material. Such microcracks are undesirable in terms of the appearance and performance of the product.
  • Furthermore, depending on the application, in some cases an austenitic stainless steel material is required to have weldability. However, when it is attempted to suppress the microcracks, in some cases the weldability may decrease. In other words, it is generally difficult to both suppress microcracks and also improve weldability.
  • In view of the above situation, an objective of the present invention is to provide an austenitic stainless steel material in which microcracks are suppressed and which has good weldability even when subjected to processing before and after nitridation treatment.
  • SOLUTION TO PROBLEM
  • The present invention has been made to solve the problem described above, and the gist of the present invention is an austenitic stainless steel material described hereunder.
    1. (1) An austenitic stainless steel material having a chemical composition including, in mass%,
      • C: 0.010 to 0.15%,
      • Si: 0.10 to 2.00%,
      • Mn: 0.10 to 3.00%,
      • P: 0.060% or less,
      • S: 0.010% or less,
      • Ni: 16.0 to 25.0%,
      • Cr: 20.0 to 29.0%,
      • Mo: 0.08 to 1.0%,
      • Sn: 0.001 to 0.080%,
      • N: 0.010 to 0.15%,
      • Co: 0.001 to 1.50%,
      • Nb: 0 to 0.20%, and
      • the balance: Fe and impurities,
      • wherein:
        • F1 calculated by Formula (i) below is 7.5 to 20.0; and
        • F2 calculated by Formula (ii) below is 320.0 or less; F 1 = 16.0 + 8.0 C + 2.4 Si 0.5 Mn + 0.3 Ni 0.9 Cr 3.1 Mo + 119 N + 2.0 Co F 2 = 286.2 + 337.9 C + 23.9 Si 2.7 Mn + 0.1 Cr 15.5 Mo + 339.4 Sn 286.9 Nb
        • where, each symbol of an element in the above formulas represents a content (mass%) of a corresponding element contained in the austenitic stainless steel material, and is assigned a value of 0 if the corresponding element is not contained.
    2. (2) The austenitic stainless steel material according to (1) above, wherein the chemical composition contains, in lieu of a part of the Fe, one or more kinds of element selected from, in mass%:
      • Cu: 1.0% or less,
      • V: 0.30% or less,
      • Ti: 0.020% or less,
      • W: 0.10% or less,
      • Al: 0.050% or less, and
      • B: 0.050% or less.
    3. (3) An austenitic stainless steel material having a chemical composition including, in mass%,
      • C: 0.010 to 0.15%,
      • Si: 0.10 to 2.0%,
      • Mn: 0.10 to 3.0%,
      • P: 0.06% or less,
      • S: 0.010% or less,
      • Ni: 16.0 to 25.0%,
      • Cr: 20.0 to 29.0%,
      • Mo: 0.08 to 1.0%,
      • Sn: 0.001 to 0.080%,
      • N: 0.010 to 0.15%,
      • Co: 0.001 to 1.5%,
      • Nb: 0 to 0.20%, and
      • the balance: Fe and impurities,
      • wherein:
        • F1 calculated by Formula (i) below is 7.5 to 20.0; and
        • F2 calculated by Formula (ii) below is 320.0 or less; F 1 = 16.0 + 8.0 C + 2.4 Si 0.5 Mn + 0.3 Ni 0.9 Cr 3.1 Mo + 119 N + 2.0 Co F 2 = 286.2 + 337.9 C + 23.9 Si 2.7 Mn + 0.1 Cr 15.5 Mo + 339.4 Sn 286.9 Nb
        • where, each symbol of an element in the above formulas represents a content (mass%) of a corresponding element contained in the austenitic stainless steel material, and is assigned a value of 0 if the corresponding element is not contained.
    4. (4) The austenitic stainless steel material according to (3) above, wherein the chemical composition contains, in lieu of a part of the Fe, one or more kinds of element selected from a group consisting of, in mass%:
      • Cu: 1.0% or less,
      • V: 0.30% or less,
      • Ti: 0.020% or less,
      • W: 0.10% or less,
      • Al: 0.050% or less, and
      • B: 0.050% or less.
    ADVANTAGEOUS EFFECT OF INVENTION
  • According to the present invention, an austenitic stainless steel material in which microcracks are suppressed and which has good weldability even when subjected to processing before and after nitridation treatment is obtained.
  • DESCRIPTION OF EMBODIMENTS
  • The present inventors have conducted various studies directed at improving weldability while suppressing the microcracks described above, and obtained the findings described in (a) to (c) below.
    1. (a) Microcracks form when a nitridation layer in which nitrogen is concentrated grows too thick due to nitridation treatment. Therefore, the present inventors have investigated the possibility of reducing the thickness of a nitridation layer in order to suppress the occurrence of microcracks. In order to reduce the thickness of a nitridation layer, it is desirable to cause nitrides, such as CrN, to form within the nitridation layer, to thereby consume N that constitutes the nitridation layer.
    2. (b) On the other hand, if nitrides are excessively formed, the formed nitrides may become starting points for microcracks. Therefore, it is important to adjust the balance between the amount of the nitridation layer and the amount of nitrides that are formed. Specifically, it is effective to set the balance with respect to the contents of elements such as C, Si, Mn, Ni, Cr, Mo, N, and Co which affect the formation of the nitridation layer, within an appropriate range.
    3. (c) It is necessary to ensure weldability while adjusting the balance between the amount of the nitridation layer and the amount of nitrides that are formed. Therefore, it is necessary to control the range of the contents of elements such as C, Si, Mn, Cr, Mo, Sn, and Nb.
  • An embodiment of the present invention has been made based on the above findings. The respective requirements of the austenitic stainless steel material of the present embodiment are described in detail hereunder.
  • 1. Chemical composition
  • The reasons for limiting each element are as follows. Note that, the symbol "%" in relation to content in the following description means "mass percent".
  • C: 0.010 to 0.15%
  • C (carbon) has an effect of improving strength. In addition, C has an effect of suppressing formation of a nitridation layer. Therefore, the content of C is 0.010% or more. The content of C is preferably 0.020% or more, and more preferably is 0.030% or more. However, if C is excessively contained, weldability will decrease. Further, mechanical properties such as toughness will decrease. Therefore, the content of C is 0.15% or less. The content of C is preferably 0.12% or less, and more preferably is 0.10% or less.
  • Si: 0.10 to 2.00%
  • Si (silicon) is an element that has a deoxidizing effect. In addition, Si has an effect of suppressing formation of a nitridation layer. Therefore, the content of Si is 0.10% or more. The content of Si is preferably 0.12% or more, more preferably is 0.15% or more, and further preferably is 0.20% or more. However, if Si is excessively contained, weldability will decrease. Therefore, the content of Si is 2.00% or less. The content of Si is preferably 1.70% or less, more preferably is 1.40% or less, and further preferably is 1.00% or less.
  • Mn: 0.10 to 3.00%
  • Mn (manganese) has an effect of improving strength. Therefore, the content of Mn is 0.10% or more. The content of Mn is preferably 0.15% or more, more preferably is 0.20% or more, and further preferably is 0.25% or more. However, if Mn is excessively contained, microcracks will easily occur. Further, weldability will also decrease. Therefore, the content of Mn is 3.00% or less. The content of Mn is preferably 2.50% or less, more preferably is 2.30% or less, and further preferably is 2.00% or less.
  • P: 0.060% or less
  • P (phosphorus) is an impurity element contained in the steel. P reduces mechanical properties such as strength and toughness. Therefore, the content of P is 0.060% or less. The content of P is preferably 0.050% or less. Although it is preferable to reduce the content of P as much as possible, excessive reduction of P will increase the refining cost. Therefore, the content of P is preferably 0.005% or more.
  • S: 0.010% or less
  • S (sulfur) is an impurity element contained in the steel. S reduces mechanical properties such as strength and toughness. Therefore, the content of S is 0.010% or less. The content of S is preferably 0.0050% or less. Although it is preferable to reduce the content of S as much as possible, excessive reduction of S will increase the refining cost. Therefore, the content of S is preferably 0.0001% or more.
  • Ni: 16.0 to 25.0%
  • N (nickel) is an element that stabilizes austenite. Further, N has an effect of improving strength. In addition, N has an effect of suppressing formation of a nitridation layer. Therefore, the content of Ni is 16.0% or more. The content of Ni is preferably 16.5% or more, more preferably is 17.0% or more, and further preferably is 18.0% or more. However, if Ni is excessively contained, weldability and hot workability will decrease. Therefore, the content of Ni is 25.0% or less. The content of Ni is preferably 24.8% or less, more preferably is 24.5% or less, and further preferably is 24.0% or less.
  • Cr: 20.0 to 29.0%
  • Cr (chromium) has an effect of increasing corrosion resistance. Therefore, the content of Cr is 20.0% or more. The content of Cr is preferably 21.0% or more, more preferably is 21.5% or more, and further preferably is 22.0% or more. However, if Cr is excessively contained, weldability will decrease. Therefore, the content of Cr is 29.0% or less. The content of Cr is preferably 28.0% or less, more preferably is 27.5% or less, and further preferably is 27.0% or less.
  • Mo: 0.08 to 1.0%
  • Mo (molybdenum) has an effect of increasing strength and corrosion resistance. Therefore, the content of Mo is 0.08% or more. The content of Mo is preferably 0.10% or more, more preferably is 0.12% or more, and further preferably is 0.15% or more. However, if Mo is excessively contained, mechanical properties such as ductility and toughness will tend to decrease. Therefore, the content of Mo is 1.0% or less. The content of Mo is preferably 0.95% or less, more preferably is 0.90% or less, and further preferably is 0.85% or less.
  • Sn: 0.001 to 0.080%
  • Sn (tin) has an effect of increasing corrosion resistance. Further, Sn also has an effect of increasing weldability. Therefore, the content of Sn is 0.001% or more. The content of Sn is preferably 0.0015% or more, more preferably is 0.002% or more, and further preferably is 0.003% or more. However, if Sn is excessively contained, hot workability will decrease. Therefore, the content of Sn is 0.080% or less. The content of Sn is preferably 0.075% or less, more preferably is 0.070% or less, and further preferably is 0.060% or less.
  • N: 0.010 to 0.15%
  • N (nitrogen) dissolves in the matrix and has an effect of stabilizing austenite. In addition, N has an effect of suppressing formation of a nitridation layer. Therefore, the content of N is 0.010% or more. The content of N is preferably 0.015% or more, more preferably is 0.020% or more, and further preferably is 0.030% or more. However, if N is excessively contained, sensitization will occur in a heat affected zone during welding, and the corrosion resistance will decrease. Therefore, the content of N is 0.15% or less. The content of N is preferably 0.14% or less, more preferably is 0.13% or less, and further preferably is 0.12% or less.
  • Co: 0.001 to 1.50%
  • Co (cobalt) is an important element in a steel plate of the present embodiment, and has an effect of suppressing formation of a nitridation layer. Therefore, the content of Co is 0.001% or more. The content of Co is preferably 0.005% or more, more preferably is 0.01% or more, and further preferably is 0.02% or more. However, if Co is excessively contained, the production cost will increase. Therefore, the content of Co is 1.50% or less. The content of Co is preferably 1.30% or less, more preferably is 1.00% or less, and further preferably is 0.80% or less.
  • In addition to the elements described above, the chemical composition may also contain Nb within the range described below in lieu of a part of Fe. The reason for limiting the element is described below.
  • Nb: 0 to 0.20%
  • Nb (niobium) forms carbo-nitrides and has an effect of increasing corrosion resistance. Therefore, Nb may be contained as necessary. However, if Nb is excessively contained, mechanical properties such as toughness will decrease. Therefore, the content of Nb is 0.20% or less. The content of Nb is preferably 0.15% or less, and more preferably is 0.10% or less. On the other hand, in order to obtain the aforementioned advantageous effect, the content of Nb is preferably 0.001% or more, more preferably is 0.005% or more, further preferably is 0.010% or more, and further preferably is 0.015% or more.
  • In addition to the elements described above, the chemical composition may also contain one or more kinds of element selected from Cu, V, Ti, Al, and B within the ranges described below in lieu of a part of Fe. The reasons for limiting each element are described below.
  • Cu: 1.0% or less
  • Cu (copper) stabilizes austenite and has an effect of improving strength. Therefore, Cu may be contained as necessary. However, if the content of Cu is excessive, hot workability will decrease. Therefore, the content of Cu is 1.0% or less. The content of Cu is preferably 0.80% or less, and more preferably is 0.60% or less. On the other hand, in order to obtain the aforementioned advantageous effect, the content of Cu is preferably 0.001% or more.
  • V: 0.30% or less
  • V (vanadium) has an effect of improving the strength of the steel by forming carbides. Therefore, V may be contained as necessary. However, if the content of V is excessive, toughness will decrease. Therefore, the content of V is 0.30% or less. The content of V is preferably 0.25% or less, and more preferably is 0.20% or less. On the other hand, in order to obtain the aforementioned advantageous effect, the content of V is preferably 0.001% or more.
  • Ti: 0.020% or less
  • Ti (titanium) has an effect of improving the strength of the steel by forming carbo-nitrides. Therefore, Ti may be contained as necessary. However, if the content of Ti is excessive, toughness will decrease. Therefore, the content of Ti is 0.020% or less. The content of Ti is preferably 0.015% or less, and more preferably is 0.010% or less. On the other hand, in order to obtain the aforementioned advantageous effect, the content of Ti is preferably 0.001% or more.
  • W: 0.10% or less
  • W (tungsten) dissolves in the parent phase and has an effect of improving the strength of the steel. Therefore, W may be contained as necessary. However, if the content of W is excessive, hot workability will decrease. Therefore, the content of W is 0.10% or less. The content of W is preferably 0.08% or less, and more preferably is 0.05% or less. On the other hand, in order to obtain the aforementioned advantageous effect, the content of W is preferably 0.001% or more.
  • Al: 0.050% or less
  • Al (aluminum) is an element that has a deoxidizing effect. Therefore, Al may be contained as necessary. However, if the content of Al is excessive, inclusions will excessively form and productivity will decrease. Therefore, the content of Al is 0.050% or less. The content of Al is preferably 0.040% or less, and more preferably is 0.030% or less. On the other hand, in order to obtain the aforementioned advantageous effect, the content of Al is preferably 0.001% or more.
  • B: 0.050% or less
  • B (boron) forms intermetallic compounds at grain boundaries, and has an effect of increasing grain boundary strength. Therefore, B may be contained as necessary. However, if the content of B is excessive, hot workability will decrease. Therefore, the content of B is to be 0.050% or less. The content of B is preferably 0.040% or less, and more preferably is 0.030% or less. On the other hand, in order to obtain the aforementioned advantageous effect, the content of B is preferably 0.0001% or more.
  • In the chemical composition of the austenitic stainless steel of the present embodiment, the balance is Fe and impurities. Here, the term "impurities" refers to components which, during industrial production of the steel, are mixed in from raw material such as ore or scrap or due to various causes during the production process, and which are allowed within a range that does not adversely affect the present embodiment.
  • Formula (i)
  • In the chemical composition of the austenitic stainless steel of the present embodiment, Fl calculated by Formula (i) below is 7.5 to 20.0. F 1 = 16.0 + 8.0 C + 2.4 Si 0.5 Mn + 0.3 Ni 0.9 Cr 3.1 Mo + 119 N + 2.0 Co
  • In the formula, each symbol of an element in the above formula represents the content (mass%) of a corresponding element contained in the austenitic stainless steel material, and is assigned a value of 0 if the corresponding element is not contained.
  • If the nitridation layer in which nitrogen is concentrated at the surface of the steel material grows too thick due to nitridation treatment, microcracks will form. Therefore, it is effective to cause nitrides, for example, CrN and the like, to form in order to reduce the thickness of the nitridation layer. Here, the above Formula (i) is an experimentally obtained relational expression with respect to C, Si, Mn, Ni, Cr, Mo, N, and Co, which are elements which affect the formation of nitrides, and F1 is an index of the likelihood of microcracks occurring in a case where processing is performed before and after nitridation treatment. If F1 is less than 7.5, nitrides cannot be formed sufficiently and the thickness of the nitridation layer cannot be reduced, and consequently microcracks will easily occur. Therefore, F1 is 7.5 or more. Fl is preferably 7.6 or more, more preferably is 7.7 or more, and further preferably is 7.8 or more.
  • On the other hand, if F1 is more than 20.0, nitrides will excessively form and, on the contrary, microcracks will easily occur. Therefore, F1 is 20.0 or less. F1 is preferably 19.0 or less, more preferably is 18.0 or less, and further preferably is 17.0 or less.
  • Formula (ii)
  • In the chemical composition of the austenitic stainless steel of the present embodiment, F2 calculated by Formula (ii) below is 320.0 or less: F 2 = 286.2 + 337.9 C + 23.9 Si 2.7 Mn + 0.1 Cr 15.5 Mo + 339.4 Sn 286.9 Nb where, each symbol of an element in the above formula represents the content (mass%) of a corresponding element contained in the austenitic stainless steel material, and is assigned a value of 0 if the corresponding element is not contained.
  • Here, the aforementioned F2 is an index indicating weldability, and Formula (ii) is an experimentally obtained formula. That is, Formula (ii) is a relational expression with respect to C, Si, Mn, Cr, Mo, Sn, and Nb which mutually affect weldability. If F2 is more than 320.0, weldability will decrease and cracks will easily occur after welding. Therefore, F2 is 320.0 or less. F2 is preferably 319.0 or less, more preferably is 318.0 or less, and further preferably is 317.0 or less. Note that, although a lower limit of F2 is not particularly limited, F2 will be 213.0 or more based on the ranges of the contents of the elements constituting Formula (ii).
  • 2. Cr depleted zone
  • In the austenitic stainless steel material of the present embodiment, as mentioned above, the occurrence of microcracks is suppressed by controlling the chemical composition to adjust the balance between the amount of a nitridation layer and the amount of nitrides that are formed. However, in a case where a Cr depleted zone is thickly formed at the surface of the austenitic stainless steel material, when nitridation treatment is performed, microcracks are slightly more likely to occur because the amount of precipitated nitrides increases due to an increase in N activity in the Cr depleted zone. From such a viewpoint, it is preferable that the thickness of the Cr depleted zone formed at the surface of the austenitic stainless steel material is thin, and specifically, the thickness is preferably 10 µm or less, and more preferably 5 µm or less. Note that it is possible to control the thickness of the Cr depleted zone to be thin by performing a heat treatment during production, to be described later, using a hydrogen furnace.
  • Note that, in the present invention the thickness of the aforementioned Cr depleted zone is to be measured by the following method. After cutting out a cross section perpendicular to the surface of the austenitic stainless steel material, a field emission electron probe microanalyzer (FE-EPMA) is used to perform a line analysis to a depth of 50 µm from the surface toward the central portion of the wall thickness at a pitch of 0.16 µm, and measurement of the Cr concentration in the depth direction is performed. At such time, the measurement is to be performed under conditions of an acceleration voltage of 15 kV and an analysis diameter of 0.1 µm. A region where the Cr concentration is 0.9 times or less for the content of Cr in the aforementioned austenitic stainless steel material is defined as a Cr depleted zone.
  • 3. Shape and applications
  • The shape of the austenitic stainless steel material of the present embodiment is not particularly limited. For example, the austenitic stainless steel material may be a steel plate, or may be a steel bar or wire rod. Further, the austenitic stainless steel material of the present embodiment is suitable for use in applications in which processing such as drawing is performed after nitridation treatment.
  • 4. Production method
  • The austenitic stainless steel material of the present embodiment can be stably produced, for example, by the following production method.
  • Steel having the aforementioned chemical composition is melted, and a raw steel such as a slab or a billet is produced by continuous casting or the like. The obtained raw steel is subjected to hot working to produce an austenitic stainless steel material having a desired shape. The hot working is, for example, hot forging, hot extrusion, hot rolling or the like. The shape may be, for example, a steel plate, a steel bar, a wire rod or the like. Note that, the conditions of the hot working are not particularly limited and may be adjusted as necessary. After the hot working, cold working may be performed as necessary. The cold working is, for example, cold drawing or cold rolling.
  • After hot working, or after cold working, usually a heat treatment is performed. Well-known conditions can be used as the heat treatment conditions. For example, the steel material may be heated to a temperature range of 1060 to 1350°C, and thereafter rapidly cooled. An atmosphere furnace is generally used when performing the heat treatment. However, as described above, when it is desired to suppress formation of a Cr depleted zone to reduce the thickness of the Cr depleted zone, it is preferable to use a hydrogen furnace.
  • Further, when performing the heat treatment using an atmosphere furnace, pickling or the like may be performed as necessary. These production conditions are also not particularly limited and may be adjusted as appropriate. The production conditions are controlled so that the final structure is an austenitic stainless steel structure.
  • In the obtained austenitic stainless steel material, it will be difficult for microcracks to occur even if, thereafter, cold working such as drawing is performed after performing nitridation treatment.
  • Hereunder, the austenitic stainless steel material according to the present invention is described more specifically by way of examples, although the present embodiment is not limited to these examples.
  • EXAMPLE
  • Steel types A to S having the chemical compositions shown in Table 1 were melted in a laboratory and subjected to hot forging to produce steel materials with a thickness of 20 mm. Thereafter, hot rolling was performed to a predetermined thickness to produce steel plates (austenitic stainless steel materials) of 1.25 mm and 7 mm in thickness. The obtained steel plates were then subjected to a heat treatment in which the steel plates were heated to a temperature of 1060°C or more in an atmosphere furnace described in Table 2, followed by rapid cooling. For some of the steel plates, the thickness of a Cr depleted zone was measured in the as heat treatment condition. Thereafter, for steel type N which had been subjected to heat treatment using an atmosphere furnace, a descaling treatment was performed by pickling. Further, for all of the steel materials, evaluation of the occurrence of microcracks and evaluation of weldability were carried out by the methods described below.
  • [Table 2]
  • Table 2
    Steel Atmosphere furnace Evaluation of microcrack occurrence Evaluation of resistance to weld crack
    Number of cracks observed/Number of observations Maximum length of crack (mm)
    A Hydrogen furnace 0/5 0.32
    B Hydrogen furnace 0/5 0.31
    C Hydrogen furnace 0/5 0.32
    D Hydrogen furnace 0/5 0.38
    E Hydrogen furnace 0/5 0.41
    F Hydrogen furnace 0/5 0.36
    G Hydrogen furnace 0/5 0.37
    H Hydrogen furnace 0/5 0.31
    I Hydrogen furnace 0/5 0.25
    J Hydrogen furnace 0/5 0.29
    K Hydrogen furnace 0/5 0.39
    L Hydrogen furnace 0/5 0.37
    M Hydrogen furnace 0/5 0.38
    N Atmosphere furnace 1/5 0.37
    O Hydrogen furnace 5/5 0.33
    P Hydrogen furnace 5/5 1.08
    Q Hydrogen furnace 3/5 0.40
    R Hydrogen furnace 3/5 1.22
    S Hydrogen furnace 0/5 1.20
    T Hydrogen furnace 2/5 0.43
  • (Measurement of thickness of Cr depleted zone)
  • For the as-heat-treated steel plates of 1.25 mm in thickness obtained from steel types C and N, a cross section perpendicular to the surface was cut out, and thereafter an FE-EPMA was used to perform a line analysis to a depth of 50 µm from the base metal surface toward the central portion of the wall thickness at a pitch of 0.16 µm to measure the Cr concentration in the depth direction. At such time, the measurement was performed under conditions of an acceleration voltage of 15 kV and an analysis diameter of 0.1 µm. A region where the Cr concentration was 0.9 times or less for the content of Cr in the austenitic stainless steel material was defined as a Cr depleted zone, and the thickness of the Cr depleted zone was measured.
  • As a result, it was found that although in steel type C which was heat-treated using a hydrogen furnace, the thickness of the Cr depleted zone was approximately 3 µm, in steel type N which was heat-treated using an atmosphere furnace, the thickness of the Cr depleted zone was approximately 15 µm.
  • (Evaluation of occurrence of microcracks)
  • The occurrence of microcracks was evaluated by a tensile test, and a subsequent structural observation and the like. Specifically, based on JIS Z 2241: 2022, a No. 5 test coupon specified in JIS was taken from each 1.25-mm thick steel plate. Strain was introduced into the test coupon by performing cold working so that the cold reduction ratio was 30% using a tensile testing machine. Thereafter, nitridation treatment was performed in which the test coupon was held at a heat treatment temperature of 1040°C for a heat treatment time of 30 minutes in a 100% nitrogen atmosphere, and then cooled with gas.
  • After nitridation treatment, a tensile test was performed once more, and strain was introduced into the tensile test coupon by cold working so that the cold reduction ratio was 25%. At such time, strain was introduced in a manner so that the tensile test coupon did not rupture, and thereafter the surface of the test coupon was observed with a scanning microscope to check for the presence or absence of microcracks. At that time, the observation magnification was set to 500×, and the number of visual fields was set to five visual fields. The number of visual fields in which cracks were observed is shown in Table 2. In the present Example, if the number of visual fields in which cracks were observed among the five visual fields was one or less, it was determined that the test coupon was acceptable.
  • (Evaluation of weldability)
  • Weldability was evaluated by examining the resistance to weld crack (solidification cracking) susceptibility in a Trans-Varestraint test. Specifically, a test specimen with dimensions of 4 mm in thickness × 100 mm in width × 100 mm in length was taken from each 7-mm thick steel plate, and the Trans-Varestraint test was performed. Here, the term "Trans-Varestraint test" refers to a test to examine cracking (solidification cracking) that occurs in a weld metal during welding. At a central part in the width direction of the surface of the aforementioned test specimen, welding was performed using GTAW (Gas Tungsten Arc Welding) to form a weld metal extending in the longitudinal direction. Further, at the moment of arc extinction during the welding, a bending strain (2%) was forcibly applied to cause cracks to occur in the weld metal. Note that, the welding condition was set to 6 kJ/cm.
  • The maximum length of the occurred cracks was measured. The results are shown in Table 2. In the present Example, if the maximum length of the cracks was 1.00 mm or less, it was determined that the resistance to weld crack susceptibility was good. On the other hand, if the maximum length of the cracks was more than 1.00 mm, it was determined that the resistance to weld crack susceptibility was failed.
  • In steel types A to M which satisfied the requirements of the austenitic stainless steel material of the present embodiment, microcracks did not occur, and weldability was good. Further, in steel type N which was heat-treated using an atmosphere furnace, microcracks were observed in only one visual field, which was within the allowable range, and weldability was also good. On the other hand, in steel types O to T which did not satisfy the requirements of the austenitic stainless steel material of the present embodiment, at least one of microcrack occurrence and a decrease in weldability occurred.
  • Specifically, in steel type O, the content of N was low and, furthermore, the value of F1 was less than the specified value, and consequently the thickness of the nitridation layer was excessive and microcracks occurred. In steel type P, the content of Cr was excessive, the value of F1 was less than the specified value and, in addition, the value of F2 was more than the specified value. As a result, microcracks occurred, and the weld crack resistance was inferior.
  • In steel type Q, the value of F1 was less than the specified value, and consequently the thickness of the nitridation layer was excessive and microcracks occurred. In steel type R, the value of F1 was excessive, and consequently nitrides excessively formed and microcracks occurred. In addition, the value of F2 was excessive, and consequently the weld crack resistance was inferior. In steel type S, the value of F2 was excessive, and consequently the weld crack resistance was inferior. In steel type T, Co was not contained, and consequently the thickness of the nitridation layer was excessive and microcracks occurred.

Claims (2)

  1. An austenitic stainless steel material having a chemical composition comprising, in mass%,
    C: 0.010 to 0.15%,
    Si: 0.10 to 2.00%,
    Mn: 0.10 to 3.00%,
    P: 0.060% or less,
    S: 0.010% or less,
    Ni: 16.0 to 25.0%,
    Cr: 20.0 to 29.0%,
    Mo: 0.08 to 1.0%,
    Sn: 0.001 to 0.080%,
    N: 0.010 to 0.15%,
    Co: 0.001 to 1.50%,
    Nb: 0 to 0.20%, and
    the balance: Fe and impurities,
    wherein:
    F1 calculated by Formula (i) below is 7.5 to 20.0; and
    F2 calculated by Formula (ii) below is 320.0 or less; F 1 = 16.0 + 8.0 C + 2.4 Si - 0.5 Mn + 0.3 Ni - 0.9 Cr - 3.1 Mo + 119 N + 2.0 Co F 2 = 286.2 + 337.9 C + 23.9 Si - 2.7 Mn + 0.1 Cr - 15.5 Mo + 339.4 Sn - 286.9 Nb
    where, each symbol of an element in the above formulas represents a content (mass%) of a corresponding element contained in the austenitic stainless steel material, and is assigned a value of 0 if the corresponding element is not contained.
  2. The austenitic stainless steel material according to claim 1, wherein the chemical composition contains, in lieu of a part of the Fe, one or more kinds selected from, in mass%:
    Cu: 1.0% or less,
    V: 0.30% or less,
    Ti: 0.020% or less,
    W: 0.10% or less,
    Al: 0.050% or less, and
    B: 0.050% or less.
EP24744646.1A 2023-01-16 2024-01-16 AUSTENITIC STAINLESS STEEL MATERIAL Pending EP4653565A4 (en)

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Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH05222512A (en) 1991-09-05 1993-08-31 Aimetsukusu Kk Method for high temperature nitriding treatment by which wear resistance in austenitic stainless steel improves and its application

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JP4325522B2 (en) * 2004-09-28 2009-09-02 住友金属工業株式会社 Stainless steel plate with excellent workability and properties of processed part and method for producing the same
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JP5780598B2 (en) * 2012-02-15 2015-09-16 新日鐵住金ステンレス株式会社 Austenitic stainless steel for high temperature equipment of welded pipe structure
JP5984213B2 (en) * 2012-10-23 2016-09-06 日本冶金工業株式会社 Austenitic Fe-Ni-Cr alloy for cladding tubes with excellent weldability
JP6684629B2 (en) * 2016-03-31 2020-04-22 日鉄ステンレス株式会社 Austenitic stainless steel with excellent high-temperature slidability, and turbocharger parts manufactured using it
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Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH05222512A (en) 1991-09-05 1993-08-31 Aimetsukusu Kk Method for high temperature nitriding treatment by which wear resistance in austenitic stainless steel improves and its application

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