EP3115476A1 - Wärmebeständige austenitische legierung - Google Patents
Wärmebeständige austenitische legierung Download PDFInfo
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- EP3115476A1 EP3115476A1 EP15758391.5A EP15758391A EP3115476A1 EP 3115476 A1 EP3115476 A1 EP 3115476A1 EP 15758391 A EP15758391 A EP 15758391A EP 3115476 A1 EP3115476 A1 EP 3115476A1
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/54—Ferrous alloys, e.g. steel alloys containing chromium with nickel with boron
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- 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
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- 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
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/0068—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for particular articles not mentioned below
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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- C22C38/00—Ferrous alloys, e.g. steel alloys
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/002—Ferrous 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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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/005—Ferrous alloys, e.g. steel alloys containing rare earths, i.e. Sc, Y, Lanthanides
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/42—Ferrous alloys, e.g. steel alloys containing chromium with nickel with copper
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—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
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/48—Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/50—Ferrous alloys, e.g. steel alloys containing chromium with nickel with titanium or zirconium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/58—Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/001—Austenite
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/004—Dispersions; Precipitations
Definitions
- the present invention relates to an austenitic heat-resistant steel.
- the method of growing crystal grains to be coarse interferes with formation of a Cr 2 O 3 protective film and therefore may have a risk of worsening steam oxidation resistance.
- the amount of the element to be added must be increased.
- the amount of the element to be added it may have some negative influences on other various basal characteristics than creep strength.
- the method of employing the solute strengthening method for a heat-resistant material could not be said to be desirable as a method of realizing an intended strength.
- Patent Document 1 discloses a method for producing an austenitic stainless steel having a high creep strength, having a fine-grained texture and excellent corrosion resistance, which includes a cold-processing step for an austenitic stainless steel containing one or more of Ti: 0.15 to 0.5% by mass and Nb: 0.3 to 1.5% by mass, wherein the steel is heated at a final softening temperature set to be higher than 1200°C and up to 1350°C, then cooled at a cooling rate of 500°C/hr or more, thereafter cold-worked by 20 to 90%, further thereafter heated at 1070 to 1300°C and at a temperature lower by 30°C or more than the final softening temperature, and processed for final heat treatment for cooling at a cooling rate not lower than air cooling.
- a cold-processing step for an austenitic stainless steel containing one or more of Ti: 0.15 to 0.5% by mass and Nb: 0.3 to 1.5% by mass wherein the steel is heated at a final softening temperature set to be higher than 1
- the method disclosed in Patent Document 1 is for precipitating only small amounts of a part of the elements to be precipitated in the practical environment or during the creep test in the stage of the above-mentioned final heat treatment to thereby prevent the crystal grains from growing to be coarse by the boundary pinning effect of the precipitates.
- the softening heat treatment temperature before the cold processing is increased by a certain level or more relative to the final heat treatment, so that the difference in the solid solute amount corresponding to the temperature difference is thereby precipitated.
- both improvement of the creep strength by high-temperature heat treatment and formation of a texture containing large quantities of fine crystal grains (fine crystal grain texture) have been realized.
- Patent Document 1 JP-B H05-69885
- a production plant for use in practical production has an upper limit temperature.
- the softening heat treatment temperature is increased up to the plant upper limit temperature, and when a difference is provided between the two heat treatment temperatures like in the method disclosed in Patent Document 1, the final heat treatment temperature must be set lower than the plant upper limit.
- lowering the final heat treatment temperature may result in reduction in the amount of the precipitate to be formed in a practical environment or during a creep test, and therefore, as a result, there is a possibility that the creep strength could not be fully increased.
- the invention disclosed in Patent Document 1 is to realize excellent steam oxidation resistance by providing a fine crystal grain texture and to realize an excellent creep strength by precipitating a small amount of precipitates to provide the boundary pinning effect.
- it is considered that realizing the pinning effect by lowering the final heat treatment temperature would use forwardly but scarify the precipitates that are to be formed in a practical environment or during a creep test.
- the presence or absence of fine precipitates of Ti carbides may have a great influence on the high-temperature strength of the steel.
- the temperature range in which Ti dissolves in solid covers high temperatures, and therefore the softening heat treatment temperature may often reach the upper limit owing to limitations on plants in many cases.
- the final heat treatment temperature must be inevitably lowered, and as the case may be, therefore, the amount of the Ti solute to precipitate in a practical environment or during a creep test could not be secured.
- the precipitation strengthening that may be obtained from steel material components could not be sufficiently utilized.
- the creep strength serves as a constraining factor to determine the thickness of the member, and therefore it is considered that, with the increase in the creep strength thereof, the member can be thinned and the cost thereof can be reduced.
- an austenitic heat-resistant steel could have a sufficient creep strength, and it may be said that the situation of the steel is such that the thickness reduction could bring about cost reduction thereof.
- the present invention has been made in consideration of the situation as above, and its object is to provide austenitic heat-resistant steel having an excellent creep strength while maintaining a fine crystal grain texture.
- a creep strength problem has been solved by specifically noting the solute amount of a precipitating element that depends on the temperature in heat treatment. Therefore, in general, it has been considered that, when the final heat treatment temperature is lowered, the solute amount of a precipitating element may reduce and therefore the amount of fine precipitates that would newly precipitate in a practical environment or during a creep test may reduce to thereby lower the creep strength.
- the temperature difference between the softening heat treatment and the final heat treatment is defined to be 30°C or more and a part of elements to be precipitated are made to be precipitated in the final heat treatment to thereby prevent the crystal grains from growing to be coarse.
- the precipitates to be precipitated according to this operation are the precipitates that should naturally precipitate in a practical environment or during a creep test to contribute toward increasing the creep strength of the steel. Specifically, there is a probability that, of the austenitic stainless steel produced according to the method disclosed in Patent Document 1, the creep strength could not be sufficiently increased by the proportion corresponding to the precipitate formed through precipitation of the precipitating element for preventing the crystal grains from growing to be coarse.
- the present inventors have assiduously studied the possibility whether the precipitates formed in the final heat treatment could directly act on the improvement of the creep strength of steel.
- the inventors have found that the precipitates that are formed by controlling the addition amount and the solute amount of the precipitating element to fall within a specific range and by carrying out the final heat treatment under a specific heat treatment condition where the precipitated grain size and the precipitation amount contained in the steel are defined to fall within a specific range (concretely, by carrying out the final heat treatment at a lower temperature than before) can improve creep strength.
- the present inventors have found that the precipitates formed through final heat treatment under a specific heat treatment condition can contribute toward improvement of creep strength directly as fine grain precipitates. This finding indicates that the precipitates provide a more excellent creep strength than conventional precipitates that are formed in high-temperature heat treatment, and is beyond the concept of the conventional technology.
- the inventors have found that, since the final heat treatment is carried out under the above-mentioned specific heat treatment condition (at a lower temperature than before), the fine crystal grain texture can be kept as such and the steam oxidation resistance can be maintained.
- the present inventors have found that, in an austenitic heat-resistant steel, the precipitates formed through final heat treatment can more effectively prevent creep deformation than the precipitates formed during a creep test.
- the precipitates formed during a creep test of an austenitic heat-resistant steel are formed along dislocation that is introduced along with deformation. Dislocation concentrates in the vicinity of grain boundaries, and therefore the distribution of the precipitates would be uneven.
- the precipitates formed in final heat treatment in production of an austenitic heat-resistant steel are formed uniformly in the grains. Accordingly, it is considered that the precipitates formed in the final heat treatment could more efficiently prevent the dislocation movement accompanied by creep deformation throughout the grains from the initial stage of deformation. For these reasons, it is presumed that, when the final heat treatment is carried out under the specific heat treatment condition as mentioned above, a good creep strength can be realized. This finding is beyond the conventional conception of the solute amount of a precipitating element that depends on the temperature of heat treatment.
- the austenitic heat-resistant steel which is achieved based on the above findings and solves the above problems includes: C: 0.05 to 0.16% by mass; Si: 0.1 to 1% by mass; Mn: 0.1 to 2.5% by mass; P: 0.01 to 0.05% by mass; S: 0.005% by mass or less (not including 0% by mass); Ni: 7 to 12% by mass; Cr: 16 to 20% by mass; Cu: 2 to 4% by mass; Mo: 0.1 to 0.8% by mass; Nb: 0.1 to 0.6% by mass; Ti: 0.1 to 0.6% by mass; B: 0.0005 to 0.005% by mass; N: 0.001 to 0.15% by mass; and at least one of Mg: 0.005% by mass or less (not including 0% by mass) and Ca: 0.005% by mass or less (not including 0% by mass), with the remainder being Fe and unavoidable impurities, and a total of a content of Nb and a content of Ti is 0.3% by mass or more, and in the austenitic
- the austenitic heat-resistant steel in the present invention contains steel material components each falling within the above-mentioned range and can be provide with a precipitate that may be formed through final heat treatment under a specific heat treatment condition.
- the precipitate is so controlled that the diameter of the precipitated particles contained in the steel and the precipitation amount thereof each could fall within a specific range, and the precipitate directly contributes toward improving the creep strength of the steel directly as a fine precipitate after the precipitation.
- the fine precipitate is, as described above, able to improve more the creep strength than a precipitate formed through precipitation by final heat treatment at a higher temperature as in before.
- the steel can have a fine grain texture and can have excellent steam oxidation resistance.
- the austenitic heat-resistant steel in the present invention further includes at least one of Zr: 0.3% by mass or less (not including 0% by mass), a rare earth element: 0.15% by mass or less (not including 0% by mass) and W: 3% by mass or less (not including 0% by mass).
- the austenitic heat-resistant steel in the present invention contains Zr within the above-mentioned range, the high-temperature strength thereof can be improved by precipitation strengthening.
- the austenitic heat-resistant steel in the present invention contains the rare earth element within the above-mentioned range, the oxidation resistance of the stainless steel can be improved. Further, when the austenitic heat-resistant steel in the present invention contains W within the above-mentioned range, the high-temperature strength thereof can be improved by solute strengthening.
- the austenitic heat-resistant steel in the present invention contains steel material components each falling within the above-mentioned range, in which the precipitate is so controlled that the precipitated particle diameter and the precipitation amount each could fall within a specific range, and therefore the steel can have an excellent creep strength while maintaining a fine crystal grain texture.
- FIG. 1 This is a graph for explaining the obtainment of a precipitated particle diameter corresponding to a half of a cumulative number density in the distribution of the cumulative number density and the precipitate particle diameter.
- the horizontal axis indicates the precipitated particle diameter (nm), and the vertical axis indicates the cumulative number density (Number/ ⁇ m 2 ).
- the austenitic heat-resistant steel of this embodiment contains, as steel material components: C: 0.05 to 0.16% by mass; Si: 0.1 to 1% by mass; Mn: 0.1 to 2.5% by mass; P: 0.01 to 0.05% by mass; S: 0.005% by mass or less (not including 0% by mass); Ni: 7 to 12% by mass; Cr: 16 to 20% by mass; Cu: 2 to 4% by mass; Mo: 0.1 to 0.8% by mass; Nb: 0.1 to 0.6% by mass; Ti: 0.1 to 0.6% by mass; B: 0.0005 to 0.005% by mass; N: 0.001 to 0.15% by mass; and at least one of Mg: 0.005% by mass or less (not including 0% by mass) and Ca: 0.005% by mass or less (not including 0% by mass), with the remainder being Fe and unavoidable impurities, and a total of a content of Nb and a content of Ti is 0.3% by mass or more.
- the austenitic heat-resistant steel of this embodiment further contains at least one of Zr: 0.3% by mass or less (not including 0% by mass), a rare earth element: 0.15% by mass or less (not including 0% by mass) and W: 3% by mass or less (not including 0% by mass).
- the austenitic heat-resistant steel of this embodiment is similar to KA-SUS321J2HTB steel using Ti as a precipitating element (18 mass% Cr - 10 mass% Ni - 3 mass% Cu -Ni,Ti steel).
- the cumulative number density of the precipitate whose particle diameter falls within a range of more than 0 nm up to 100 nm is 0.1 to 2.0 Number/ ⁇ m 2
- the precipitate particle diameter corresponding to a half of the cumulative number density in the distribution of the cumulative number density and the precipitate particle diameter is 70 nm or less
- the average hardness is 160 Hv or less
- the grain size number is 7.5 or more.
- the precipitated particle diameter is one calculated as a circle-corresponding diameter of the precipitated particle (precipitate).
- the reason why the precipitate as so controlled that the precipitated particle size and the precipitation in the steel each fall within a specific range can be formed through final heat treatment under a specific heat treatment condition is as already described hereinabove in the section of Solution to Problem.
- the above-mentioned average hardness and the grain size number can be controlled by controlling the heat treatment temperature.
- the specific heat treatment condition and heat treatment temperature will be described hereinunder.
- the precipitate formed under a specific heat treatment condition contributes toward improving creep strength, as being a fine precipitate.
- the crystal grains can keep a fine crystal grain texture. Accordingly, the austenitic heat-resistant steel of this embodiment can be excellent in steam oxidation resistance.
- the steel material components of the austenitic heat-resistant steel of this embodiment and the reason why the precipitated particle diameter and the precipitation amount to be contained in the steel are defined each to fall within a specific range are described below.
- the austenitic heat-resistant steel of this embodiment is similar to KA-SUS321J2HTB that uses Ti as a precipitating element.
- the steel material components described below each exhibit the effect as described below, and when their content falls outside a predetermined content range, there may occur some inconveniences.
- C has an effect of forming a carbide to improve high-temperature strength.
- C is contained in an amount of 0.05% by mass or more.
- the C content is excessive to be more than 0.16% by mass, coarse carbides are formed to fail in improving high-temperature strength.
- the lower limit of the C content is preferably 0.08% by mass, more preferably 0.09% by mass.
- the upper limit of the C content is preferably 0.15% by mass, more preferably 0.13% by mass.
- Si has a deoxidizing effect in a molten steel and effectively acts for improving oxidation resistance.
- Si is contained in an amount of 0.1% by mass or more.
- the case where the Si content is excessive and is more than 1% by mass is unfavorable as often causing embrittlement of the steel material.
- the lower limit of the Si content is preferably 0.2% by mass, more preferably 0.3% by mass.
- the upper limit of the Si content is 0.7% by mass, more preferably 0.5% by mass.
- Mn has a deoxidizing effect in a molten steel.
- Mn is contained in an amount of 0.1 % by mass or more.
- the case where the Mn content is more than 2.5% by mass is unfavorable as promoting growth of carbide precipitates to be coarse.
- the lower limit of the Mn content is preferably 0.2% by mass, more preferably 0.3% by mass.
- the upper limit of the Mn content is 2.0% by mass, more preferably 1.8% by mass.
- P has an effect of improving high-temperature strength.
- P for improving high-temperature strength, P is contained in an amount of 0.01% by mass or more.
- the P content is excessive to be more than 0.05% by mass, it may detract from weldability.
- the lower limit of the P content is preferably 0.015% by mass, more preferably 0.02% by mass.
- the upper content of the P content is 0.04% by mass, more preferably 0.03% by mass.
- S is an unavoidable impurity.
- the S content is excessive to be more than 0.005% by mass, it degrades hot processability.
- the S content is limited to be 0.005% by mass or less. The S content is preferably smaller.
- the upper limit of the S content is preferably 0.002% by mass, more preferably 0.001 % by mass.
- Ni has an effect of stabilizing an austenitic phase.
- Ni for stabilizing the austenitic phase, Ni is contained in an amount of 7% by mass or more. However, when the Ni content is more than 12% by mass, it causes cost increase of the steel material.
- the lower limit of the Ni content is preferably 9% by mass, more preferably 9.5% by mass.
- the upper limit of the Ni content is preferably 11.5% by mass, more preferably 11% by mass.
- Cr has an effect of improving oxidation resistance and corrosion resistance of a steel material.
- Cr is contained in an amount of 16% by mass or more.
- the steel material may be thereby embrittled.
- the lower limit of the Cr content is preferably 17.5% by mass, more preferably 18% by mass.
- the upper limit of the Cr content is preferably 19.5% by mass, more preferably 19% by mass.
- Cu has an effect of forming a precipitate in a steel to improve high-temperature strength.
- Cu is contained in an amount of 2% by mass or more.
- the effect may be saturated.
- the lower limit of the Cu content is preferably 2.5% by mass, more preferably 2.8% by mass.
- the upper limit of the Cu content is preferably 3.5% by mass, more preferably 3.2% by mass.
- Mo has an effect of improving corrosion resistance.
- Mo is contained in an amount of 0.1% by mass or more.
- the Mo content is excessive to be more than 0.8% by mass, the steel material may be thereby embrittled.
- the lower limit of the Mo content is preferably 0.2% by mass, more preferably 0.3% by mass.
- the upper limit of the Mo content is preferably 0.6% by mass, more preferably 0.5% by mass.
- the total of the Nb content and the Ni content is 0.3% by mass or more.
- Nb and Ti are, when precipitated as a carbonitride (carbide, nitride or carbonitride), able to improve high-temperature strength.
- the precipitate prevents crystal grains from growing to be coarse and promotes Cr diffusion. Owing to Cr diffusion, the elements exhibits an effect of subsidiarily improving corrosion resistance (steam oxidation resistance), and therefore, these can be said to be a part of most important elements in the present invention.
- Nb is contained in an amount of 0.1% by mass or more and Ti is contained in an amount of 0.1% by mass or more.
- the lower limit of the Nb content is preferably 0.2% by mass.
- the lower limit of the Ti content is preferably 0.15% by mass.
- the lower limit of the total of the Nb content and the Ti content is preferably 0.35% by mass.
- the precipitate may grow to be coarse in any case, thereby lowering toughness.
- the upper limit of the Nb content and the Ti content is each preferably 0.4% by mass, more preferably 0.3% by mass.
- B has an effect of promoting formation of an M 23 C 6 -type carbide (where M is a carbide-forming element) to improve high-temperature strength.
- M is a carbide-forming element
- B is contained in an amount of 0.0005% by mass or more.
- the B content is excessive to be more than 0.005% by mass, it lowers weldability.
- the lower limit of the B content is preferably 0.001% by mass, more preferably 0.0015% by mass.
- the upper limit of the B content is preferably 0.004% by mass, more preferably 0.003% by mass.
- N has an effect of improving high-temperature strength by solute strengthening.
- N for improving high-temperature strength, N is contained in an amount of 0.001% by mass or more.
- the N content is excessive to be more than 0.15% by mass, it causes formation of coarse Ti nitride and Nb nitride to worsen toughness.
- the lower limit of the N content is preferably 0.002% by mass, more preferably 0.003% by mass.
- the upper limit of the N content is preferably 0.08% by mass, more preferably 0.04% by mass.
- Mg and Ca each act as a desulfurizing/deoxidizing element and have an effect of improving hot processability of a steel material.
- Ca and Mg are preferably contained each in a range of 0.005% by mass or less.
- the upper limit of Ca and Mg is 0.002% by mass each.
- Zr is an optional component and has an effect of improving high-temperature strength by precipitation strengthening.
- the Zr content is excessive to be more than 0.3% by mass, a coarse intermetallic compound may be thereby formed to lower high-temperature ductility.
- the upper limit of the Zr content is preferably 0.25% by mass.
- the component when Zr is contained, it increases the cost of a steel material, and therefore, the component may be optionally contained.
- Rare earth elements are optional components and have an effect of improving oxidation resistance of stainless steel.
- the upper limit of the rare earth element content is preferably 0.1% by mass, more preferably 0.05% by mass.
- rare earth elements are one or more elements selected from Sc and Y, and 15 kinds of lanthanoid elements typified by La, Ce and Ne, that is, 17 kinds of elements in total.
- the rare earth element content is the total content of one or more elements selected from those 17 kinds of elements.
- W is an optional component, and has an effect of improving high-temperature strength by solute strengthening.
- W content is excessive to be more than 3% by weight, coarse intermetallic compounds are formed to lower high-temperature ductility.
- the upper limit of the W content is preferably 2.5% by mass, more preferably 2.0% by mass.
- the remainder is Fe and other unavoidable impurities.
- the other unavoidable impurities include, for example, Al, Sn, Zn, Pb, As, Bi, Sb, Te, Se, In, etc.
- the amounts of the unavoidable impurities are as small as possible, and as rough indication thereof, it is recommended that the amount of Al is 0.01% by mass or less, Sn is 0.005% by mass or less, Zn is 0.01% by mass or less, Pb is 0.002% by mass or less, As is 0.01% by mass or less, Bi is 0.002% by mass or less, Sb is 0.002% by mass or less, Te is 0.01% by mass or less, Se is 0.002% by mass or less, and In is 0.002% by mass or less.
- the average hardness is defined to be 160 Hv or less.
- the average hardness is more than 160 Hv, the solute amount of the element to precipitate in a practical environment or during a creep test could not be secured, and if so, therefore, the creep strength lowers.
- the steel is heat-treated at a temperature of 1150°C or higher and then cooled in water to easily attain the numeral range, though depending on the above-mentioned compositional formulation thereof.
- the upper limit of the average hardness is 140 Hv.
- the lower limit of the average hardness is 100 Hv, more preferably 110 Hv.
- the Vickers hardness may be measured, for example, according to JIS Z 2244:2009.
- the cumulative number density of the precipitate whose particle diameter falls within a range of more than 0 nm up to 100 nm is 0.1 to 2.0 Number/ ⁇ m 2 .
- the precipitate particle diameter corresponding to a half of the cumulative number density in the distribution of the cumulative number density and the precipitate particle diameter is 70 nm or less.
- the cumulative number density of the precipitate whose particle diameter falls within a range of more than 0 nm up to 100 nm is defined to be 0.1 to 2.0 Number/ ⁇ m 2
- the precipitate particle diameter corresponding to a half of the cumulative number density in the distribution of the cumulative number density and the precipitate particle diameter is defined to be 70 nm or less, whereby the creep strength can be enhanced.
- the precipitate to form in the final heat treatment while the amount of the precipitate having a size of 100 nm or less is controlled to be not more than a specific level, the precipitate particle diameter corresponding to a half of the cumulative number density is controlled to be 70 nm or less, that is, the precipitates are kept fine, and accordingly, the creep strength can be thereby enhanced.
- the lower limit of the cumulative number density is preferably 0.3 Number/ ⁇ m 2 , more preferably 0.4 Number/ ⁇ m 2 .
- the upper limit of the precipitate particle diameter corresponding to a half of the cumulative number density is preferably 60 nm, more preferably 50 nm.
- the lower limit of the precipitate particle diameter corresponding to a half of the cumulative number density is more than 0 nm.
- the grain size number is 7.5 or more.
- the metal texture is in a sufficiently fine state, and can be said to be a fine crystal grain texture. Accordingly, the steel of the type can maintain steam oxidation resistance.
- the steel may be processed for final heat treatment under a specific heat treatment condition to be mentioned below.
- the steel may be subjected to final heat treatment under a condition under which the coarsening factor for the precipitate could be 2000°C ⁇ min or less, on the premise of the above-mentioned steel material composition and the hardness range.
- This "condition under which the coarsening factor for the precipitate could be 2000°C ⁇ min or less" is the above-mentioned specific heat treatment condition.
- the coarsening factor for precipitate is an index of indicating the influence of heat on the growth of precipitate to be coarse grains, and is a value calculated by integrating a temperature of 900°C or higher at which the precipitate growth goes on relative to the temperature history during the heat treatment, with respect to time.
- the coarsening factor must include not only the retention time in heat treatment but also the heating time at 900°C or higher and the cooling time.
- the coarsening factor for a conventional austenitic heat-resistant steel which contains Ti as a precipitating element and whose high-temperature strength has been sufficiently increased, such as KA-SUS321J2HTB steel is about 3000 to 7000°C ⁇ min.
- the coarsening factor is 2000°C ⁇ min or less, as described above.
- the lower limit of the coarsening factor it is preferably larger than 473°C ⁇ min, more preferably 500°C ⁇ min or more, even more preferably 821°C ⁇ min. or more.
- the highest endpoint temperature and the retention time can be controlled in accordance with the limitations on equipment.
- the precipitating element must be dissolved in solid by carrying out the softening heat treatment at a temperature higher by 30°C or more than in the final heat treatment.
- a temperature lower by 30°C than in the softening heat treatment is the upper limit temperature for the above-mentioned final heat treatment.
- the coarsening factor could satisfy the above-mentioned condition, it is necessary to quantify the number density and the size distribution of the precipitate.
- This can be carried out by taking a microscopic image showing the dispersion of precipitate particles on the cross section of a steel material, and analyzing the image for quantification of the data.
- the microscopic image may be taken, for example, by photographing the surface of an electrolytically-polished steel material with a scanning electron microscope.
- a transmission electron microscope may be used in place of the scanning electron microscope. From the viewpoint of quantification accuracy, it is recommended that at least 200 precipitated particles are quantitatively analyzed, and the data of more than 0 nm to 100 nm are arranged through histogram at intervals of 10 nm.
- the cumulative number density (Number/ ⁇ m 2 ) at intervals of 10 nm is plotted on the vertical axis, and the precipitated particle diameter (nm) is on the horizontal axis, in which "the cumulative number density of the precipitate whose particle diameter falls within a range of more than 0 nm up to 100 nm” that is defined in the present invention can be understood from the numerical value falling between 90 nm and 100 nm on the horizontal axis.
- the precipitate particle diameter corresponding to a half of the cumulative number density of the precipitate whose particle diameter falls within a range of more than 0 nm to 100 nm the case shown in the drawing is referred to.
- the point between 50 nm and 60 nm and the point between 60 nm and 70 nm are connected to give a line
- the precipitate particle diameter can be understood as the numeral value on the horizontal axis on which the resultant line crosses the line extended from a half of the numeral value falling between 90 nm and 100 nm.
- the steel material components are defined to fall within the above-mentioned range, and the precipitated particle diameter and the precipitation amount in the steel are defined to fall within a specific range, and therefore the steel can have an excellent creep strength while maintaining a fine crystal grain texture.
- the precipitation that has been heretofore sacrificed can be made to contribute toward increasing the creep strength. Accordingly, even in the case where the temperature in heat treatment has an upper limit owing to limitations on equipment, etc., the precipitation strengthening effect can be maximized. Consequently, from an austenitic heat-resistant steel using Ti as a precipitating element therein, a heat-resistant stainless steel whose creep strength is further increased while the fine crystal grain texture thereof is kept as such can be produced.
- the austenitic heat-resistant steel of this embodiment can have an increased creep strength, and therefore the thickness of a heat-resistant member to be formed of the steel can be thinned more than before, and the present invention can realize cost reduction of heat-resistant members.
- Nos. A to F shown in Table 1 Nos. A to E are similar to so-called KA-SUS321J2HTB steel, and are steel materials satisfying the chemical component composition defined in the present invention. As opposed to these, No. F is a steel material overstepping the chemical component composition defined in the present invention.
- Each original steel material was heat-treated at a varying heating temperature of 1040 to 1215°C for a varying period of time of 0.5 to 10 minutes to vary the coarsening factor [°C ⁇ min] for the precipitate, thereby preparing steel materials of Nos. 1 to 31 shown in Table 2.
- These steel materials were analyzed for the Vickers hardness thereof, the cumulative number density of the precipitate therein whose particle diameter falls within a range of more than 0 nm up to 100 nm, the precipitate particle diameter corresponding to a half of the cumulative number density in the distribution of the cumulative number density and the precipitate particle diameter, the grain size number, and the creep rupture time, in the manner as mentioned below.
- the measured results are shown in Table 2 along and the coarsening factors therein.
- each steel material of Nos. 1 to 31 was tested in a Vickers hardness test according to JIS Z 2244:2009 to measure the hardness thereof.
- the load in the Vickers hardness test was 10 kg.
- Those having a Vickers hardness of 160 Hv or less were evaluated as excellent in average hardness, while those more than 160 Hv were evaluated as poor in average hardness.
- the texture of the steel material of Nos. 1 to 31 was microscopically observed according to JIS G 0551:2013 to measure the crystal grain number. Those having a crystal grain number of 7.5 or more were considered as having passed the test, while those with less than 7.5 were considered as having failed in the test.
- a test piece was prepared from each steel material of Nos. 1 to 31 according to JIS Z 2271:2010, and tested to measure the time. Those having taken a creep rupture time of 650 hours or more were evaluated as excellent in creep strength, while those with less than 650 hours were evaluated as poor in creep strength. [Table 2] No. Steel material component No.
- Nos. 4 and 7, Nos. 11 and 14, Nos. 16 and 18, Nos. 20 and 23, and Nos. 25 and 28 are Examples in which the heat treatment temperature for the former was lower than that for the latter.
- Nos. 4 and 7, Nos. 11 and 14, and Nos. 25 and 28 are Examples in which the temperature was lowered by 20°C;
- Nos. 16 and 18 are Examples in which the temperature was lowered by 10°C;
- Nos. 20 and 23 are Examples in which the temperature was lowered by 30°C.
- the steel materials of Nos. 1, 2, 19 and 24 are Comparative Examples in which the crystal grains grew coarsely since the heat treatment condition (the precipitate coarsening factor) was inappropriate. Specifically, these steel materials could not realize even a fine crystal grain texture that was attained according to a conventional technique (for example, in the invention described in Patent Document 1). Consequently, it is presumed that the steel materials of Nos. 1, 2, 19 and 24 could not obtain good moisture oxidation-resistant characteristics.
- the steel material of No. 9 is Comparative Example in which the precipitate coarsening factor of the material was too low, and therefore the precipitated component could not be sufficiently dissolved in solid.
- the steel material of No. 9 had a fine crystal grain texture, but it was confirmed that the Vickers hardness (average hardness) thereof was outside the definition in the present invention, and the creep rupture time was short.
- the steel materials of Nos. 29 to 31 are Comparative Examples in which the chemical component compositions are outside the definition in the present invention.
- the crystal grains were coarse and contained some favorable element in point of creep strength, but for the creep strength of both the steel materials, the time was shorter than 650 hours, that is, as compared with Examples, the steel materials could have only an insufficient strength.
- the steel material of No. 31 had a grain size number of 7.5 and had a good fine crystal grain texture, but for the creep strength thereof, the time was shorter than 650 hours, that is, as compared with Examples, the steel material could have only an insufficient strength.
- the steel materials of Nos. 3, 6, 10, 13, 15, 22 and 27 had a good fine crystal grain texture having a grain size number of 7.5 or more.
- these steel materials of Nos. 3, 6, 10, 13, 15, 22 and 27 could not satisfy at least one of the cumulative number density of the precipitate whose particle diameter falls within a range of more than 0 nm up to 100 nm, and the precipitate particle diameter corresponding to a half of the cumulative number density in the distribution of the cumulative number density and the precipitate particle diameter, and therefore, as compared with Examples, these were poor in point of the creep rupture time (all Comparative Examples).
- the steel materials satisfying the definition in the present invention were excellent in creep strength in point of having a fine crystal grain texture as compared with the steel materials not satisfying the definition in the present invention (the steel materials of Comparative Examples).
- the austenitic heat-resistant steel in the present invention exhibits an excellent creep strength even in a high-temperature environment, and is therefore useful for energy-related instruments such as boilers, reactors and the like.
- the steel has an excellent creep strength even in a high-temperature environment.
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JP2014042889A JP6289941B2 (ja) | 2014-03-05 | 2014-03-05 | オーステナイト系耐熱鋼 |
PCT/JP2015/056433 WO2015133551A1 (ja) | 2014-03-05 | 2015-03-04 | オーステナイト系耐熱鋼 |
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JP5143960B1 (ja) * | 2011-05-11 | 2013-02-13 | 株式会社神戸製鋼所 | 高温強度と耐繰返し酸化特性に優れた耐熱オーステナイト系ステンレス鋼 |
JP2017014575A (ja) * | 2015-07-01 | 2017-01-19 | 新日鐵住金株式会社 | オーステナイト系耐熱合金及び溶接構造物 |
JP6623719B2 (ja) * | 2015-11-25 | 2019-12-25 | 日本製鉄株式会社 | オーステナイト系ステンレス鋼 |
JP6638551B2 (ja) * | 2016-05-09 | 2020-01-29 | 日本製鉄株式会社 | オーステナイト系耐熱鋼溶接金属およびそれを有する溶接継手 |
CN105951002B (zh) * | 2016-05-25 | 2017-11-10 | 江苏金基特钢有限公司 | 一种耐腐蚀易成型不锈钢丝的制备方法 |
CN106544601A (zh) * | 2016-12-29 | 2017-03-29 | 董世祥 | 多性能耐高温系列铸钢 |
CN109554609B (zh) * | 2017-09-26 | 2022-03-15 | 宝钢德盛不锈钢有限公司 | 一种表面免起皮的奥氏体耐热钢及其制造方法 |
JP6870750B2 (ja) * | 2017-10-03 | 2021-05-12 | 日本製鉄株式会社 | オーステナイト系耐熱鋼用溶接材料、溶接金属および溶接構造物ならびに溶接金属および溶接構造物の製造方法 |
CN109576580B (zh) * | 2018-11-29 | 2020-09-29 | 武汉华培动力科技有限公司 | 柴油机可变截面增压器喷嘴组件用耐热钢及冶炼方法 |
WO2021220913A1 (ja) * | 2020-04-30 | 2021-11-04 | 日本製鉄株式会社 | オーステナイト系耐熱鋼の製造方法 |
JP7457262B2 (ja) * | 2020-04-30 | 2024-03-28 | 日本製鉄株式会社 | オーステナイト系耐熱鋼 |
US20220145174A1 (en) * | 2020-11-05 | 2022-05-12 | Seoul National University R&Db Foundation | Perovskite color converter and method of manufacturing the same |
FR3143631A1 (fr) * | 2022-12-15 | 2024-06-21 | Commissariat A L'energie Atomique Et Aux Energies Alternatives | Utilisation d’un acier à triple structuration dans un environnement acide |
CN116200668B (zh) * | 2023-04-17 | 2023-11-14 | 宁波晴力紧固件有限公司 | 一种耐热高强度紧固件材料及其制备方法 |
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JPS58167726A (ja) * | 1982-03-29 | 1983-10-04 | Sumitomo Metal Ind Ltd | オ−ステナイト系ステンレス鋼の製造方法 |
JPH01287249A (ja) * | 1988-12-27 | 1989-11-17 | Nkk Corp | オーステナイトステンレス鋼管およびその製造法 |
JPH0569885A (ja) | 1991-09-13 | 1993-03-23 | Nhk Spring Co Ltd | 駐艇装置用台車 |
JPH09165655A (ja) * | 1995-12-14 | 1997-06-24 | Nkk Corp | 高温機器用オーステナイトステンレス鋼およびその製造方法 |
JP3282481B2 (ja) * | 1996-01-31 | 2002-05-13 | 三菱マテリアル株式会社 | 耐熱鋼 |
JP3463617B2 (ja) * | 1999-08-06 | 2003-11-05 | 住友金属工業株式会社 | 熱間加工性に優れる継目無鋼管用オーステナイト系耐熱鋼 |
JP4173611B2 (ja) * | 1999-09-29 | 2008-10-29 | 日新製鋼株式会社 | 二重構造エキゾーストマニホールドの内管用オーステナイト系ステンレス鋼 |
JP2002146481A (ja) | 2000-11-07 | 2002-05-22 | Nippon Steel Corp | 電縫溶接性に優れた酸化物分散強化型フェライト系電縫ボイラ用鋼および鋼管 |
JP2003301242A (ja) * | 2002-04-11 | 2003-10-24 | Jfe Steel Kk | 高Cr−Ni系耐熱鋼および耐クリープ特性に優れた高温用部材の製造方法 |
JP2005281855A (ja) * | 2004-03-04 | 2005-10-13 | Daido Steel Co Ltd | 耐熱オーステナイト系ステンレス鋼及びその製造方法 |
JP4578280B2 (ja) * | 2005-03-08 | 2010-11-10 | 日新製鋼株式会社 | 自動車給油系部材用オーステナイト系ステンレス鋼 |
EP1867743B9 (de) * | 2005-04-04 | 2015-04-29 | Nippon Steel & Sumitomo Metal Corporation | Austenitischer nichtrostender stahl |
JP5296186B2 (ja) * | 2011-12-27 | 2013-09-25 | 株式会社神戸製鋼所 | 耐スケール剥離性に優れた耐熱オーステナイト系ステンレス鋼およびステンレス鋼管 |
JP5794945B2 (ja) * | 2012-03-30 | 2015-10-14 | 新日鐵住金ステンレス株式会社 | 耐熱オーステナイト系ステンレス鋼板 |
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- 2015-03-04 EP EP15758391.5A patent/EP3115476A4/de not_active Withdrawn
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CN106062230B (zh) | 2017-07-14 |
KR20160116344A (ko) | 2016-10-07 |
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US20170067139A1 (en) | 2017-03-09 |
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