EP3926057A1 - High-mn steel and method for manufacturing same - Google Patents
High-mn steel and method for manufacturing same Download PDFInfo
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- EP3926057A1 EP3926057A1 EP20756282.8A EP20756282A EP3926057A1 EP 3926057 A1 EP3926057 A1 EP 3926057A1 EP 20756282 A EP20756282 A EP 20756282A EP 3926057 A1 EP3926057 A1 EP 3926057A1
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- 229910000831 Steel Inorganic materials 0.000 title claims abstract description 128
- 239000010959 steel Substances 0.000 title claims abstract description 128
- 238000004519 manufacturing process Methods 0.000 title claims description 15
- 238000000034 method Methods 0.000 title description 7
- 229910001566 austenite Inorganic materials 0.000 claims abstract description 21
- 239000000203 mixture Substances 0.000 claims abstract description 17
- 239000000126 substance Substances 0.000 claims abstract description 17
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 14
- 239000011159 matrix material Substances 0.000 claims abstract description 8
- 239000012535 impurity Substances 0.000 claims abstract description 7
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 7
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 4
- 229910052791 calcium Inorganic materials 0.000 claims abstract description 4
- 229910052760 oxygen Inorganic materials 0.000 claims abstract description 4
- 229910052698 phosphorus Inorganic materials 0.000 claims abstract description 4
- 229910052717 sulfur Inorganic materials 0.000 claims abstract description 4
- 229910052799 carbon Inorganic materials 0.000 claims abstract 3
- 229910052804 chromium Inorganic materials 0.000 claims abstract 3
- 229910052748 manganese Inorganic materials 0.000 claims abstract 3
- 229910052757 nitrogen Inorganic materials 0.000 claims abstract 3
- 238000001816 cooling Methods 0.000 claims description 34
- 239000000463 material Substances 0.000 claims description 33
- 238000005096 rolling process Methods 0.000 claims description 22
- 238000005098 hot rolling Methods 0.000 claims description 16
- 238000010438 heat treatment Methods 0.000 claims description 12
- 229910052802 copper Inorganic materials 0.000 claims description 7
- 229910052720 vanadium Inorganic materials 0.000 claims description 5
- 229910052750 molybdenum Inorganic materials 0.000 claims description 4
- 229910052749 magnesium Inorganic materials 0.000 claims description 3
- 229910052721 tungsten Inorganic materials 0.000 claims description 3
- 230000000052 comparative effect Effects 0.000 description 35
- VEXZGXHMUGYJMC-UHFFFAOYSA-M Chloride anion Chemical compound [Cl-] VEXZGXHMUGYJMC-UHFFFAOYSA-M 0.000 description 27
- 238000005336 cracking Methods 0.000 description 26
- 238000005260 corrosion Methods 0.000 description 25
- 230000007797 corrosion Effects 0.000 description 25
- 230000000694 effects Effects 0.000 description 16
- 229910052761 rare earth metal Inorganic materials 0.000 description 13
- 150000002910 rare earth metals Chemical class 0.000 description 13
- 239000013078 crystal Substances 0.000 description 12
- 239000011777 magnesium Substances 0.000 description 12
- 229910052758 niobium Inorganic materials 0.000 description 11
- 230000002542 deteriorative effect Effects 0.000 description 9
- 239000010953 base metal Substances 0.000 description 8
- TWRXJAOTZQYOKJ-UHFFFAOYSA-L Magnesium chloride Chemical compound [Mg+2].[Cl-].[Cl-] TWRXJAOTZQYOKJ-UHFFFAOYSA-L 0.000 description 6
- 229910045601 alloy Inorganic materials 0.000 description 6
- 239000000956 alloy Substances 0.000 description 6
- 238000009864 tensile test Methods 0.000 description 6
- 230000015572 biosynthetic process Effects 0.000 description 5
- 230000000877 morphologic effect Effects 0.000 description 5
- 238000007670 refining Methods 0.000 description 5
- 238000003860 storage Methods 0.000 description 5
- 238000009835 boiling Methods 0.000 description 4
- 238000005266 casting Methods 0.000 description 4
- 230000001965 increasing effect Effects 0.000 description 4
- 239000002244 precipitate Substances 0.000 description 4
- 238000001556 precipitation Methods 0.000 description 4
- 239000000243 solution Substances 0.000 description 4
- UCKMPCXJQFINFW-UHFFFAOYSA-N Sulphide Chemical compound [S-2] UCKMPCXJQFINFW-UHFFFAOYSA-N 0.000 description 3
- 238000009749 continuous casting Methods 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 238000009863 impact test Methods 0.000 description 3
- 229910001629 magnesium chloride Inorganic materials 0.000 description 3
- 150000001247 metal acetylides Chemical class 0.000 description 3
- 238000009628 steelmaking Methods 0.000 description 3
- 239000002131 composite material Substances 0.000 description 2
- 230000001814 effect on stress Effects 0.000 description 2
- 239000003949 liquefied natural gas Substances 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 239000002994 raw material Substances 0.000 description 2
- 239000002893 slag Substances 0.000 description 2
- 239000006104 solid solution Substances 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910001257 Nb alloy Inorganic materials 0.000 description 1
- 229910000746 Structural steel Inorganic materials 0.000 description 1
- 229910001069 Ti alloy Inorganic materials 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 229910000963 austenitic stainless steel Inorganic materials 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 238000005485 electric heating Methods 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 238000009776 industrial production Methods 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 229910000734 martensite Inorganic materials 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 238000010992 reflux Methods 0.000 description 1
- 238000004088 simulation Methods 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000001574 stearyl tartrate Substances 0.000 description 1
- 238000009849 vacuum degassing Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
- 229910000859 α-Fe Inorganic materials 0.000 description 1
Classifications
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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
- C21D6/005—Heat treatment of ferrous alloys containing Mn
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/02—Hardening articles or materials formed by forging or rolling, with no further heating beyond that required for the formation
-
- 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
- C21D6/002—Heat treatment of ferrous alloys containing Cr
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/004—Heat treatment of ferrous alloys containing Cr and Ni
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0205—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips of ferrous alloys
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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
- C21D8/021—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips involving a particular fabrication or treatment of ingot or slab
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0226—Hot rolling
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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
- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
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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
- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
- C21D8/0263—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment following hot rolling
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
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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
- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
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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
- C22C38/002—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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- 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
- C22C38/005—Ferrous alloys, e.g. steel alloys containing rare earths, i.e. Sc, Y, Lanthanides
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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
- C22C38/02—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
- C22C38/06—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
- C22C38/46—Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
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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
Definitions
- This disclosure relates to high-Mn steel that is suitable for a structure used in a cryogenic environment such as a storage tank of liquefied gas and a manufacturing method therefor.
- a structure for a storage tank of liquefied gas is used in a cryogenic environment. Therefore, a steel plate used for this type of structure needs to have high strength and excellent toughness at extremely low temperature. For example, when a hot-rolled steel plate is used for a storage tank of liquefied natural gas, excellent toughness needs to be guaranteed at an extremely low temperature equal to or below the boiling point of the liquefied natural gas, that is, -164 °C or lower. When a steel material has poor low-temperature toughness, the safety as a structure for a cryogenic storage tank may not be maintained. Thus, there is a growing demand for steel materials with improved low-temperature toughness that are applied to such a structure.
- austenitic stainless steel which has austenite as a primary microstructure of a steel plate, the austenite showing no brittleness at extremely low temperature, 9 % Ni steel, or 5000-series aluminum alloy have been conventionally used.
- the alloy cost and manufacturing cost of these steels and alloy are high, and thus there is a demand for steel materials which are inexpensive and excellent in low-temperature toughness.
- JP 2016-084529 A (PTL 1) and JP 2016-196703 A (PTL 2) propose using, as structural steel used in a cryogenic environment, high-Mn steel added with a large amount of Mn which is relatively inexpensive and an austenite-stabilizing element.
- PTL 1 proposes controlling carbide coverage on austenite crystal grain boundaries. Further, PTL 2 proposes controlling austenite crystal grain size by using carbide coated materials and adding Mg, Ca, and REM.
- the deformation performance in the later stage of deformation after the stress measured in a tensile test reaches the maximum (tensile strength) is also an important characteristic for a structural member. This is because the deformation performance in the later stage of deformation is the performance in the final stage leading to the eventual fracture. From this perspective, ductility in the later stage of deformation, particularly, a sufficient reduction of area should be ensured. From the viewpoint of ensuring ductility of high-strength steel, a desirable reduction of area is 50 % or more.
- high-Mn steel which has both high strength and excellent low-temperature toughness and exhibits excellent ductility, and a manufacturing method therefor.
- high strength refers to having a yield strength of 400 MPa or more and a tensile strength of 800 MPa or more at room temperature.
- excellent low-temperature toughness means that when a Charpy impact test in conformity with JIS Z2242 (1998) is performed at ⁇ 196 °C on a full-sized (10 mm ⁇ 10 mm ⁇ 55 mm) test piece which is a steel plate having a plate thickness of 10 mm or more, the base metal has a Charpy impact absorbed energy of 100 J or more on average (when using a half-sized test piece of 10 mm ⁇ 5 mm ⁇ 55 mm which is a steel plate having a plate thickness of less than 10 mm, 20 J or more on a Charpy V notch half size test).
- excellent ductility refers to having a reduction of area of 50 % or more.
- chloride stress corrosion cracking refers to a phenomenon in which, in a corrosive environment specific to high-Mn steel, in particular, in an environment with chloride ions, high-Mn steel leads to cracking or breaking even when tensile stress applied to the high-Mn steel is not greater than the tensile strength of the high-Mn steel.
- chloride stress corrosion cracking resistance refer to resistance properties to the chloride stress corrosion cracking.
- the C content is an inexpensive austenite-stabilizing element, and an important element to obtain austenite. To obtain this effect, the C content needs to be 0.10 % or more. On the other hand, a C content beyond 0.70 % generates excessive Cr carbides, deteriorating low-temperature toughness. Therefore, the C content is set to 0.10 % or more and 0.70 % or less.
- the C content is preferably 0.20 % or more.
- the C content is preferably 0.60 % or less.
- the C content is more preferably 0.20 % or more and 0.60 % or less.
- Si 0.10 % or more and 0.90 % or less
- Si acts as a deoxidizer, is necessary for steelmaking, and is effective at increasing hardness of a steel plate by solid solution strengthening when dissolved in steel. To obtain such effects, the Si content needs to be 0.10 % or more. On the other hand, a Si content beyond 0.9 % deteriorates weldability and also reduces low-temperature toughness, in particular toughness at extremely low temperature. Therefore, the Si content is set to 0.10 % or more and 0.90 % or less.
- the Si content is preferably 0.12 % or more.
- the Si content is preferably 0.70 % or less.
- the Si content is more preferably 0.12 % or more and 0.70 % or less.
- Mn 20 % or more and 30 % or less
- Mn is a relatively inexpensive austenite-stabilizing element.
- Mn is an important element for achieving both strength and cryogenic toughness.
- the Mn content needs to be 20 % or more.
- a Mn content beyond 30 % does not increase the effect of improving low-temperature toughness but increases alloy cost. Further, such a high Mn content deteriorates weldability and cuttability. Therefore, the Mn content is set to 20 % or more and 30 % or less.
- the Mn content is preferably 23 % or more.
- the Mn content is preferably 28 % or less.
- the Mn content is more preferably 23 % or more and 28 % or less.
- the P content is desirably set to 0.002 % or more.
- the P content is preferably 0.005 % or more.
- the P content is preferably 0.028 % or less, and more preferably 0.024 % or less. Further, the P content is more preferably 0.005 % or more and 0.028 % or less.
- the upper limit of the S content is 0.0070 %, and desirably, the S content is kept as small as possible. Accordingly, the S content is set to 0.0070 % or less. Excessively reducing S, however, involves high refining cost and is economically disadvantageous. Therefore, the S content is preferably set to 0.001 % or more.
- the S content is preferably 0.0020 % or more.
- the S content is preferably 0.0060 % or less.
- the S content is more preferably 0.0020 % or more and 0.0060 % or less.
- Al 0.01 % or more and 0.07 % or less
- Al acts as a deoxidizer and is most commonly used in molten steel deoxidizing processes to obtain a steel plate. To obtain such an effect, the Al content needs to be 0.01 % or more. On the other hand, when the Al content is beyond 0.07 %, Al is mixed into a weld metal portion during welding, deteriorating toughness of the weld metal. Therefore, the Al content is set to 0.07 % or less. Therefore, the Al content is set to 0.01 % or more and 0.07 % or less.
- the Al content is preferably 0.02 % or more.
- the Al content is preferably 0.06 % or less.
- the Al content is more preferably 0.02 % or more and 0.06 % or less.
- the Cr content is an element which stabilizes austenite with an appropriate amount of addition and is effective at improving low-temperature toughness and base metal strength. To obtain such effects, the Cr content needs to be 1.8 % or more. On the other hand, a Cr content beyond 7.0 % generates Cr carbides, deteriorating low-temperature toughness and stress corrosion cracking resistance. Therefore, the Cr content is set to 1.8 % or more and 7.0 % or less.
- the Cr content is preferably 2.0 % or more.
- the Cr content is preferably 6.7 % or less.
- the Cr content is more preferably 2.0 % or more and 6.7 % or less.
- the Cr content is further preferably 2.0 % or more.
- the content is further preferably 6.0 % or less.
- Ni 0.01 % or more and less than 1.0 %
- Ni is effective at increasing hardness of a steel plate by solid solution strengthening when dissolved in steel and at improving low-temperature toughness, especially toughness at extremely low temperature.
- Ni is contained in an amount of 0.01 % or more.
- the Ni content is desirably minimized, and thus the addition amount of Ni is set to less than 1.0 %.
- the Ni content is preferably 0.03 % or more.
- the Ni content is preferably 0.8 % or less.
- the Ni content is more preferably 0.03 % or more and 0.8 % or less.
- stainless steels such as SUS304 and SUS316 as austenite steel which are excellent in low-temperature toughness have optimized Ni equivalent and Cr equivalent as an alloy design for obtaining an austenite microstructure, and thus are added with a large amount of Ni.
- the steel of this disclosure is an austenitic material which is produced at lower cost by minimizing the need for Ni. The need for Ni is minimized by optimizing the addition amount of Mn.
- Ni 0.1 % or more and less than 1.0 %
- the addition of Ni with an appropriate balance between the amount of Cu and the amount of Ni can exhibit excellent chloride stress corrosion cracking resistance regardless of the chloride concentration.
- the Ni content is set to 0.1 % or more and less than 1.0 %.
- a Ni content of less than 0.1 % does not produce the effect on stress corrosion cracking.
- a Ni content of 1.0 % or more incurs cost increase.
- the Ca content improves toughness through morphological control of inclusions described below and effectively acts to ensure ductility (reduction of area) during tensile deformation. To obtain such effects, the Ca content needs to be 0.0005 % or more. On the other hand, addition of Ca in excess of 0.010 % may reduce ductility and toughness instead. Therefore, the Ca content is set to 0.0005 % or more and 0.010 % or less.
- the Ca content is preferably 0.0010 % or more.
- the Ca content is preferably 0.0090 % or less.
- the Ca content is more preferably 0.0010 % or more and 0.0090 % or less.
- Ca/S it is important to control the morphology of Ca-based inclusions by further keeping Ca/S within an appropriate range. That is, setting Ca/S to ⁇ 1.0 to promote composite precipitation of MnS using Ca-based inclusions as nuclei in crystal grains is effective at suppressing the precipitation and coarsening of MnS on crystal grain boundaries, thereby improving toughness and ensuring ductility during tensile deformation, specifically, achieving a reduction of area of 50 % or more. To obtain such effects, Ca/S needs to be 1.0 or more. Ca/S is preferably 1.7 or more.
- N 0.0050 % or more and 0.0500 % or less
- N is an austenite-stabilizing element and an element which is effective at improving low-temperature toughness. To obtain such an effect, the N content needs to be 0.0050 % or more. On the other hand, the N content beyond 0.0500 % coarsens nitrides or carbonitrides, deteriorating toughness. Therefore, the N content is set to 0.0050 % or more and 0.0500 % or less.
- the N content is preferably 0.0060 % or more.
- the N content is preferably 0.0400 % or less.
- the N content is more preferably 0.0060 % or more and 0.0400 % or less.
- the O content is set to 0.0050 % or less.
- the O content is preferably 0.0045 % or less. Excessive reducing the O content involves high refining cost and is economically disadvantageous. Therefore, the O content is desirably 0.0003 % or more.
- Ti and Nb form carbonitrides with a high melting point in steel to prevent coarsening of crystal grains, then becoming an origin of fracture and a propagation path of cracks.
- Ti and Nb hinder microstructural control for enhancing low-temperature toughness and improving ductility, and thus, need to be intentionally limited.
- Ti and Nb are components which are inevitably introduced with raw materials and other sources, and Ti of more than 0.005 % and 0.010 % or less and Nb of more than 0.005 % and 0.010 % or less are typically introduced into steel.
- each of Ti and Nb By limiting the content of each of Ti and Nb to 0.0050 % or less, the adverse effect of carbonitrides can be eliminated, and excellent low-temperature toughness and ductility can be guaranteed.
- the content of each of Ti and Nb is preferably set to less than 0.0050 %, and more preferably 0.003 % or less.
- Cu has an effect of improving chloride stress corrosion cracking resistance under an environment with low chloride concentration. From this point of view, a Cu content of 0.2 % or more is effective. On the other hand, Cu conversely deteriorates chloride stress corrosion cracking resistance under an environment with high chloride concentration. Therefore, when Cu is contained, the Cu content is set to less than 2.0 %. A Cu content of less than 0.2 % does not produce an effect on stress corrosion cracking properties, and a Cu content of 2.0 % or more causes the above problem and incurs cost increase.
- the Cu content is preferably 0.3 % or more.
- the Cu content is preferably 0.8 % or less.
- the Cu content is more preferably 0.3 % or more and 0.8 % or less.
- the balance other than the aforementioned essential components is Fe and inevitable impurities.
- the inevitable impurities include H, and a total content of 0.01 % or less may be allowed.
- the following elements can be contained as necessary in addition to the above essential components: at least one selected from the group consisting of Mo: 2.0 % or less, V: 2.0 % or less, W: 2.0 % or less, Mg: 0.0005 % or more and 0.0050 % or less, REM: 0.0010 % or more and 0.0200 % or less.
- Mo, V, and W stabilize austenite and improve base metal strength. To obtain such effects, Mo, V, and/or W is preferably contained in an amount of 0.001 % or more.
- the content of each added element is preferably 2.0 % or less.
- the content of each added element is more preferably 0.003 % or more.
- the content of each added element is preferably 1.7 % or less, and more preferably 1.5 % or less. Further, the content of each added element is preferably 0.003 % or more and 1.7 % or less, and more preferably 0.003 % or more and 1.5 % or less.
- Mg 0.0005 % or more and 0.0050 % or less
- REM 0.0010 % or more and 0.0200 % or less
- Mg and REM are elements useful for morphological control of inclusions and can be contained as necessary.
- the morphological control of inclusions means granulating elongated sulfide inclusions.
- the morphological control of inclusions improves ductility, toughness, and sulfide stress corrosion cracking resistance.
- Mg is preferably contained in an amount of 0.0005 % or more and REM is preferably contained in an amount of 0.0010 % or more.
- these elements are contained in a large amount, not only the amount of nonmetallic inclusions may be increased, ending up deteriorating ductility, toughness, and sulfide stress corrosion cracking resistance, but also an economic disadvantage may be entailed.
- the Mg content is preferably 0.0005 % or more.
- the Mg content is preferably 0.0050 % or less.
- the REM content is preferably 0.0010 % or more.
- the REM content is preferably 0.0200 % or less.
- the Mg content is more preferably 0.0010 % or more.
- the Mg content is more preferably 0.0040 % or less.
- the Mg content is further preferably 0.0010 % or more and 0.0040 % or less.
- the REM content is more preferably 0.0020 % or more.
- the REM content is more preferably 0.0150 % or less.
- the REM content is further preferably 0.0020 % or more and 0.0150 % or less.
- the steel material When a steel material has a body centered cubic (bcc) crystal structure, the steel material may cause brittle fracture in a low-temperature environment, and thus, is not suitable for use in a low-temperature environment.
- the steel material When the steel material is assumed to be used in a low-temperature environment, the steel material is required to have, as a matrix, an austenite microstructure, which has a face centered cubic (fcc) crystal structure.
- fcc face centered cubic
- the terms of "containing austenite as a matrix” means that the area ratio of austenite phase is 90 % or more. The remainder besides the austenite phase is ferrite or martensite phase. Of course, the area ratio of the austenite phase may be 100 %.
- the manufacturing method of high-Mn steel of this disclosure comprises: heating a steel material having the aforementioned chemical composition; hot rolling the heated steel material to obtain a hot-rolled plate; and subjecting the hot-rolled plate to cooling treatment.
- the temperature range in the heating of the steel material is 1100 °C to 1300 °C
- the rolling finish temperature in the hot rolling is 750 °C or higher and lower than 950 °C
- the average cooling rate from a temperature at or above (the rolling finish temperature - 100 °C) to a temperature range of 300 °C to 650 °C in the cooling treatment is 0.5 °C/s or more.
- the steel material can be obtained from molten steel having the aforementioned chemical composition which is prepared by steelmaking using a publicly-known method such as using a converter or an electric heating furnace.
- the high-Mn steel may also be subjected to secondary refinement in a vacuum degassing furnace. During the secondary refinement, to limit the contents of Ti and Nb which hinder suitable microstructural control within the aforementioned range, it is necessary to prevent Ti and Nb from being inevitably introduced with raw materials and other sources so as to reduce the contents of Ti and Nb.
- the molten steel can be oxidized by blowing in oxygen, and the Ti and Nb alloys can be suspended and separated during reflux. Subsequently, it is preferable to make the steel into a steel material such as a slab having a determined size by a publicly-known steelmaking method such as continuous casting or ingot casting. The slab after continuous casting may be subjected to blooming to obtain a steel material.
- manufacturing conditions are specifically defined below to make the aforementioned steel material into a steel material exhibiting high strength, excellent low-temperature toughness and ductility.
- Heating temperature of a steel material 1100 °C or higher and 1300 °C or lower
- the heating temperature before hot rolling is set to 1100 °C or higher. However, the heating temperature beyond 1300 °C may trigger local melting. Thus, the upper limit of the heating temperature is set to 1300 °C.
- the temperature is controlled based on a surface temperature of the steel material.
- Rolling finish temperature 750 °C or higher and lower than 950 °C
- the steel material (steel ingot or a billet) is heated and subsequently subjected to hot rolling.
- hot rolling at low temperature refines the microstructure and excessively introduces working strain, thus deteriorating low-temperature toughness. Therefore, the lower limit of the rolling finishing temperature in the hot rolling is set to 750 °C in terms of a surface temperature of the steel plate.
- finishing of rolling in a temperature range of 950 °C or higher will result in excessively coarse grain size, and thus desired yield stress cannot be obtained. Therefore, final finish rolling needs to be performed in one pass or more at lower than 950 °C.
- the rolling finish temperature - 100 °C Average cooling rate from a temperature at or above (the rolling finish temperature - 100 °C) to a temperature range of 300 °C to 650 °C: 0.5 °C/s or more
- cooling is immediately performed. Slowly cooling the steel plate after the hot rolling promotes formation of precipitates, thus deteriorating low-temperature toughness. Cooling the steel plate at a cooling rate of 0.5 °C/s or more in a predetermined temperature range can prevent formation of these precipitates. Further, excessive cooling distorts the steel plate, deteriorating productivity. Therefore, the upper limit of the cooling start temperature can be set at 900 °C. Further, the lower limit of the cooling start temperature is set at (the rolling finish temperature - 100 °C).
- the cooling end temperature is within a temperature range of 300 °C to 650 °C. This is because cooling to the above temperature range can suppress the precipitation of carbides which lower toughness.
- the average cooling rate at a surface of the steel plate from a temperature at or above (the rolling finish temperature - 100 °C) in terms of a surface temperature of the steel plate to a temperature range of 300 °C to 650 °C is set to 0.5 °C/s or more.
- the average cooling rate is preferably 200 °C/s or less.
- the cooling rate is calculated as an average cooling rate of the steel plate by simulation calculation based on the temperature change of its surface.
- the cooling time in the temperature range of 1400 °C to 1300 °C in terms of a surface temperature of the steel is preferably controlled to 100 s or less. Controlling the cooling time in the casting process as described above promotes composite precipitation of MnS containing Ca-based inclusions such as Ca(O,S) as nucleus and the number of (Ca,Mn)S is increased. As a result, MnS does not grow at crystal grain boundaries or within crystal grains and thus the ratio of elongated MnS is lowered. Through such morphological control of Ca-based inclusions, high-Mn steel having a good reduction of area as high as 51 % or more can be obtained.
- Steel slabs having the chemical compositions listed in Table 1 were made as steel materials by a process for refining with converter and ladle and continuous casting. Next, the obtained steel slabs were subjected to blooming and hot rolling to obtain steel plates having a thickness up to 32 mm under the conditions listed in Table 2. Tensile properties, toughness, and microstructures of the steel plates were evaluated as described below.
- JIS NO. 4 tensile test pieces were collected from the obtained steel plates having a plate thickness of more than 15 mm.
- Round bar tensile test pieces having a parallel portion diameter of 6 mm and a gauge length of 25 mm were collected from the obtained steel plates having a plate thickness of less than 15 mm. Then, the test pieces were subjected to a tensile test to investigate tensile test properties.
- a test piece had a yield stress of 400 MPa or more and a tensile strength of 800 MPa or more
- the corresponding steel plate was determined to have excellent tensile properties and high strength.
- the corresponding steel plate was determined to have excellent ductility.
- Charpy V-notch full-sized test pieces were taken from the direction parallel to the rolling direction at a position from the steel plate surface to a depth of 1/4 of the plate thickness (hereinafter, referred to as 1/4 position of the plate thickness) of each steel plate over 20 mm in thickness, or at a position from the steel plate surface to a depth of 1/2 of the plate thickness (hereinafter, referred to as 1/2 position of the plate thickness) of each steel plate not over 20 mm in thickness, in conformity with JIS Z 2202 (1998). Then, the test pieces were subjected to the Charpy impact test in conformity with JIS Z 2242 (1998), where three test pieces were used for each steel plate, to determine absorbed energy at -196 °C and evaluate base metal toughness.
- the corresponding steel plate when the three test pieces had an average absorbed energy (vE -196 ) of 100 J or more, the corresponding steel plate was determined to have excellent base metal low-temperature toughness.
- Charpy V-notch half-sized test pieces were collected from the steel plates and similarly subjected to the Charpy impact test.
- the test pieces when the test pieces had an average absorbed energy of 20 J or more, the corresponding steel plate was determined to have excellent base metal low-temperature toughness.
- test time was 400 hours. After the test, test pieces with no cracks observed on the surface thereof was judged to have excellent chloride stress corrosion cracking resistance. In Table 3, cases where no cracks were visually observed on the surface are indicated as "good", and cases where cracks were visually observed on the surface as "poor".
- High-Mn steel of this disclosure was confirmed to satisfy the aforementioned desired performance (a base metal yield stress of 400 MPa or more, a reduction of area of 50 % or more, an average absorbed energy (vE -196 ) of 100 J or more (20 J or more for a half-sized test piece) for low-temperature toughness).
- the comparative examples out of the scope of this disclosure did not satisfy the aforementioned desired performance in terms of one or more of yield stress, reduction of area, and low-temperature toughness.
- sample 32 in which Cu and Ni were contained so that Cu/Ni was within the predetermined range. exhibited excellent chloride stress corrosion cracking resistance. On the other hand, in sample 33 where Cu/Ni was outside the predetermined range, sufficient chloride stress corrosion cracking resistance could not be confirmed.
- Cooling time from 1400 °C to 1300 °C during casting Plate thickness Hot rolling method Remarks Heating temperature of steel material Rolling finish temperature Cooling start temperature Average cooling rate to temperature range of 300 °C to 650 °C (s) (mm) (°C) (°C) (°C) (°C/s) 1 A 20 32 1160 863 836 8 Example 2 B 50 23 1180 825 795 11 Example 3 C 60 12 1150 781 726 13 Example 4 D 80 21 1120 792 760 10 Example 5 E 20 24 1130 860 830 9 Example 6 F 30 14 1130 842 787 11 Example 7 G 30 8 1260 885 821 15 Example 8 H 40 9 1200 832 773 12 Example 9 I 50 14 1140 828 772 4 Example 10 J 70 29 1160 858 831 0.9 Example 11 K 30 11 1110 755 705 11 Example 12 J 20 12 1150 775 723 11 Example 13 L 30 19 1230 765 733 8 Comparative Example 14 M 50 30 1180 885 858 7 Comparative Example 15 N
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Abstract
Description
- This disclosure relates to high-Mn steel that is suitable for a structure used in a cryogenic environment such as a storage tank of liquefied gas and a manufacturing method therefor.
- A structure for a storage tank of liquefied gas is used in a cryogenic environment. Therefore, a steel plate used for this type of structure needs to have high strength and excellent toughness at extremely low temperature. For example, when a hot-rolled steel plate is used for a storage tank of liquefied natural gas, excellent toughness needs to be guaranteed at an extremely low temperature equal to or below the boiling point of the liquefied natural gas, that is, -164 °C or lower. When a steel material has poor low-temperature toughness, the safety as a structure for a cryogenic storage tank may not be maintained. Thus, there is a growing demand for steel materials with improved low-temperature toughness that are applied to such a structure.
- In view of the demand, austenitic stainless steel which has austenite as a primary microstructure of a steel plate, the austenite showing no brittleness at extremely low temperature, 9 % Ni steel, or 5000-series aluminum alloy have been conventionally used. However, the alloy cost and manufacturing cost of these steels and alloy are high, and thus there is a demand for steel materials which are inexpensive and excellent in low-temperature toughness.
- As new steel materials replacing conventional steel for extremely low temperature,
(PTL 1) andJP 2016-084529 A (PTL 2) propose using, as structural steel used in a cryogenic environment, high-Mn steel added with a large amount of Mn which is relatively inexpensive and an austenite-stabilizing element.JP 2016-196703 A - That is, PTL 1 proposes controlling carbide coverage on austenite crystal grain boundaries. Further, PTL 2 proposes controlling austenite crystal grain size by using carbide coated materials and adding Mg, Ca, and REM.
-
- PTL 1:
JP 2016-84529 A - PTL 2:
JP 2016-196703 A - Austenite steel used as steel for extremely low temperature described in PTLs 1 and 2, which is highly strain-hardened from the early stage of deformation until maximum stress (tensile strength) is applied upon tensile deformation, has excellent plastic deformability, and thus exhibits excellent ductility until the middle stage of deformation. On the other hand, the deformation performance in the later stage of deformation after the stress measured in a tensile test reaches the maximum (tensile strength) is also an important characteristic for a structural member. This is because the deformation performance in the later stage of deformation is the performance in the final stage leading to the eventual fracture. From this perspective, ductility in the later stage of deformation, particularly, a sufficient reduction of area should be ensured. From the viewpoint of ensuring ductility of high-strength steel, a desirable reduction of area is 50 % or more.
- It could thus be helpful to provide high-Mn steel which has both high strength and excellent low-temperature toughness and exhibits excellent ductility, and a manufacturing method therefor. As used herein, the terms of "high strength" refers to having a yield strength of 400 MPa or more and a tensile strength of 800 MPa or more at room temperature. Further, the terms of "excellent low-temperature toughness" means that when a Charpy impact test in conformity with JIS Z2242 (1998) is performed at ―196 °C on a full-sized (10 mm × 10 mm × 55 mm) test piece which is a steel plate having a plate thickness of 10 mm or more, the base metal has a Charpy impact absorbed energy of 100 J or more on average (when using a half-sized test piece of 10 mm × 5 mm × 55 mm which is a steel plate having a plate thickness of less than 10 mm, 20 J or more on a Charpy V notch half size test). Moreover, the terms of "excellent ductility" refers to having a reduction of area of 50 % or more.
- We made extensive studies on measures to solve the above-mentioned problems on high-Mn steel, and discovered the following.
- That is, we discovered that in high-Mn steel, toughness can be improved and ductility (reduction of area) upon tensile deformation can be guaranteed by controlling the morphology of Ca-based inclusions and for that purpose, it is effective to control the balance between the Ca content and the S content within an appropriate range.
- Further, we found that in manufacturing the high-Mn steel, it is possible to control the crystal grain size and suppress the formation of precipitates, thereby improving low-temperature toughness by limiting steel material heating temperature, rolling finish temperature and average cooling rate from a temperature at or above (the rolling finish temperature - 100 °C) to a temperature range of 300 °C to 650 °C.
- When high-Mn steel contains Cu, Cu has an effect of improving the chloride stress corrosion cracking resistance under an environment with low chloride concentration. However, Cu conversely deteriorates the chloride stress corrosion cracking resistance under an environment with high chloride concentration. To address this issue, we found that high-Mn steel containing Cu, when optimized in the balance between the Cu content and the Ni content and added with Ni, exhibits excellent chloride stress corrosion cracking resistance even in an environment with high chloride concentration. Thus, it is possible to impart excellent chloride stress corrosion cracking resistance to high-Mn steel containing Cu regardless of the chloride concentration.
- In this disclosure, the term of chloride stress corrosion cracking refers to a phenomenon in which, in a corrosive environment specific to high-Mn steel, in particular, in an environment with chloride ions, high-Mn steel leads to cracking or breaking even when tensile stress applied to the high-Mn steel is not greater than the tensile strength of the high-Mn steel. Further, the terms of chloride stress corrosion cracking resistance refer to resistance properties to the chloride stress corrosion cracking.
- Based on these discoveries, we conducted further investigation which eventually led to the present disclosure. The primary features of the present disclosure are as follows.
- 1. High-Mn steel comprising:
- a chemical composition containing (consisting of), in mass%,
- C: 0.10 % or more and 0.70 % or less,
- Si: 0.10 % or more and 0.90 % or less,
- Mn: 20 % or more and 30 % or less,
- P: 0.030 % or less,
- S: 0.0070 % or less,
- Al: 0.01 % or more and 0.07 % or less,
- Cr: 1.8 % or more and 7.0 % or less,
- Ni: 0.01 % or more and less than 1.0 %,
- Ca: 0.0005 % or more and 0.010 % or less,
- N: 0.0050 % or more and 0.0500 % or less,
- O: 0.0050 % or less,
- Ti: 0.0050 % or less, and
- Nb: 0.0050 % or less, within a range satisfying the following formula (1), with the balance being Fe and inevitable impurities,
- a microstructure containing austenite as a matrix;
- a yield stress of 400 MPa or more; and
- an average Charpy impact absorbed energy at ―196 °C of 100 J or more for a full-sized test piece and 20 J or more for a half-sized test piece.
- 2. The High-Mn steel according to 1., wherein the chemical composition further contains, in mass%, at least one selected from the group consisting of
- Cu: less than 2.0 %,
- Mo: 2.0 % or less,
- V: 2.0 % or less,
- W: 2.0 % or less,
- Mg: 0.0005 % or more and 0.0050 % or less, and
- REM (rare earth metal): 0.0010 % or more and 0.0200 % or less.
- 3. A manufacturing method of high-Mn steel, comprising: heating a steel material having the chemical composition according to 1. or 2. to a temperature range of 1100 °C to 1300 °C; then hot rolling the steel material with a rolling finish temperature of 750 °C or higher and lower than 950 °C to obtain a hot-rolled plate; and then subjecting the hot-rolled plate to cooling treatment at an average cooling rate of 0.5 °C/s or more from a temperature at or above (the rolling finish temperature - 100 °C) to a temperature range of 300 °C to 650 °C.
- 4. High-Mn steel comprising:
a chemical composition containing (consisting of), in mass%,- C: 0.10 % or more and 0.70 % or less,
- Si: 0.10 % or more and 0.90 % or less,
- Mn: 20 % or more and 30 % or less,
- P: 0.030 % or less,
- S: 0.0070 % or less,
- Al: 0.01 % or more and 0.07 % or less,
- Cr: 1.8 % or more and 7.0 % or less,
- Cu: 0.2 % or more and less than 2.0 %
- Ni: 0.1 % or more and less than 1.0 %,
- Ca: 0.0005 % or more and 0.010 % or less,
- N: 0.0050 % or more and 0.0500 % or less,
- O: 0.0050 % or less,
- Ti: 0.0050 % or less and
- Nb: 0.0050 % or less, within a range satisfying the following formulas (1) and (2), with the balance being Fe and inevitable impurities,
and and
a microstructure containing austenite as a matrix.
- 5. A manufacturing method of high-Mn steel, comprising: heating a steel material having the chemical composition according to 4. to a temperature range of 1100 °C to 1300 °C; then hot rolling the steel material with a rolling finish temperature of 750 °C or higher and lower than 950 °C to obtain a hot-rolled plate; and then subjecting the hot-rolled plate to cooling treatment at an average cooling rate of 0.5 °C/s or more from a temperature at or above (the rolling finish temperature - 100 °C) to a temperature range of 300 °C to 650 °C.
- According to an embodiment of this disclosure, it is possible to provide high-Mn steel which has high strength, excellent low-temperature toughness especially in a cryogenic range and excellent ductility. Therefore, the safety and the service life of a steel structure used in a cryogenic environment such as a storage tank of liquefied gas can be improved by using our high-Mn steel, which provides significant industrial effects.
- Further, according to another embodiment of this disclosure, it is possible to provide high-Mn steel which exhibits excellent chloride stress corrosion cracking resistance regardless of the chloride concentration.
- Our high-Mn steel will be described in detail below.
- The chemical composition of our high-Mn steel and the reasons for the limitations thereof are described first. In the description of the chemical composition, "%" denotes "mass%" unless otherwise noted.
- C is an inexpensive austenite-stabilizing element, and an important element to obtain austenite. To obtain this effect, the C content needs to be 0.10 % or more. On the other hand, a C content beyond 0.70 % generates excessive Cr carbides, deteriorating low-temperature toughness. Therefore, the C content is set to 0.10 % or more and 0.70 % or less. The C content is preferably 0.20 % or more. The C content is preferably 0.60 % or less. The C content is more preferably 0.20 % or more and 0.60 % or less.
- Si acts as a deoxidizer, is necessary for steelmaking, and is effective at increasing hardness of a steel plate by solid solution strengthening when dissolved in steel. To obtain such effects, the Si content needs to be 0.10 % or more. On the other hand, a Si content beyond 0.9 % deteriorates weldability and also reduces low-temperature toughness, in particular toughness at extremely low temperature. Therefore, the Si content is set to 0.10 % or more and 0.90 % or less. The Si content is preferably 0.12 % or more. The Si content is preferably 0.70 % or less. The Si content is more preferably 0.12 % or more and 0.70 % or less.
- Mn is a relatively inexpensive austenite-stabilizing element. In this disclosure, Mn is an important element for achieving both strength and cryogenic toughness. To obtain such effects, the Mn content needs to be 20 % or more. On the other hand, a Mn content beyond 30 % does not increase the effect of improving low-temperature toughness but increases alloy cost. Further, such a high Mn content deteriorates weldability and cuttability. Therefore, the Mn content is set to 20 % or more and 30 % or less. The Mn content is preferably 23 % or more. The Mn content is preferably 28 % or less. The Mn content is more preferably 23 % or more and 28 % or less.
- When a P content is beyond 0.030 %, P segregates to grain boundaries and becomes an origin of stress corrosion cracking. Therefore, the upper limit of the P content is 0.030 %, and desirably, the P content is kept as small as possible. Therefore, the P content is set to 0.030 % or less. Excessively reducing P, however, involves high refining cost and is economically disadvantageous. Therefore, the P content is desirably set to 0.002 % or more. The P content is preferably 0.005 % or more. The P content is preferably 0.028 % or less, and more preferably 0.024 % or less. Further, the P content is more preferably 0.005 % or more and 0.028 % or less.
- S deteriorates base metal low-temperature toughness and ductility. Therefore, the upper limit of the S content is 0.0070 %, and desirably, the S content is kept as small as possible. Accordingly, the S content is set to 0.0070 % or less. Excessively reducing S, however, involves high refining cost and is economically disadvantageous. Therefore, the S content is preferably set to 0.001 % or more. The S content is preferably 0.0020 % or more. The S content is preferably 0.0060 % or less. The S content is more preferably 0.0020 % or more and 0.0060 % or less.
- Al acts as a deoxidizer and is most commonly used in molten steel deoxidizing processes to obtain a steel plate. To obtain such an effect, the Al content needs to be 0.01 % or more. On the other hand, when the Al content is beyond 0.07 %, Al is mixed into a weld metal portion during welding, deteriorating toughness of the weld metal. Therefore, the Al content is set to 0.07 % or less. Therefore, the Al content is set to 0.01 % or more and 0.07 % or less. The Al content is preferably 0.02 % or more. The Al content is preferably 0.06 % or less. The Al content is more preferably 0.02 % or more and 0.06 % or less.
- Cr is an element which stabilizes austenite with an appropriate amount of addition and is effective at improving low-temperature toughness and base metal strength. To obtain such effects, the Cr content needs to be 1.8 % or more. On the other hand, a Cr content beyond 7.0 % generates Cr carbides, deteriorating low-temperature toughness and stress corrosion cracking resistance. Therefore, the Cr content is set to 1.8 % or more and 7.0 % or less. The Cr content is preferably 2.0 % or more. The Cr content is preferably 6.7 % or less. The Cr content is more preferably 2.0 % or more and 6.7 % or less. Further, to improve stress corrosion cracking resistance, the Cr content is further preferably 2.0 % or more. The content is further preferably 6.0 % or less.
- Ni is effective at increasing hardness of a steel plate by solid solution strengthening when dissolved in steel and at improving low-temperature toughness, especially toughness at extremely low temperature. Thus, Ni is contained in an amount of 0.01 % or more. On the other hand, from the perspective of alloy cost, the Ni content is desirably minimized, and thus the addition amount of Ni is set to less than 1.0 %. The Ni content is preferably 0.03 % or more. The Ni content is preferably 0.8 % or less. The Ni content is more preferably 0.03 % or more and 0.8 % or less. Here, stainless steels such as SUS304 and SUS316 as austenite steel which are excellent in low-temperature toughness have optimized Ni equivalent and Cr equivalent as an alloy design for obtaining an austenite microstructure, and thus are added with a large amount of Ni. In contrast with these steels, the steel of this disclosure is an austenitic material which is produced at lower cost by minimizing the need for Ni. The need for Ni is minimized by optimizing the addition amount of Mn.
- Further, when the high-Mn steel contains a predetermined amount of Cu, the addition of Ni with an appropriate balance between the amount of Cu and the amount of Ni can exhibit excellent chloride stress corrosion cracking resistance regardless of the chloride concentration. From this point of view, in high-Mn steel containing Cu in an amount of 0.2 % or more and less than 2.0 % as described later, the Ni content is set to 0.1 % or more and less than 1.0 %. A Ni content of less than 0.1 % does not produce the effect on stress corrosion cracking. A Ni content of 1.0 % or more incurs cost increase.
- Ca improves toughness through morphological control of inclusions described below and effectively acts to ensure ductility (reduction of area) during tensile deformation. To obtain such effects, the Ca content needs to be 0.0005 % or more. On the other hand, addition of Ca in excess of 0.010 % may reduce ductility and toughness instead. Therefore, the Ca content is set to 0.0005 % or more and 0.010 % or less. The Ca content is preferably 0.0010 % or more. The Ca content is preferably 0.0090 % or less. The Ca content is more preferably 0.0010 % or more and 0.0090 % or less.
- With the Ca content and S content described above, it is important to control the morphology of Ca-based inclusions by further keeping Ca/S within an appropriate range. That is, setting Ca/S to ≥ 1.0 to promote composite precipitation of MnS using Ca-based inclusions as nuclei in crystal grains is effective at suppressing the precipitation and coarsening of MnS on crystal grain boundaries, thereby improving toughness and ensuring ductility during tensile deformation, specifically, achieving a reduction of area of 50 % or more. To obtain such effects, Ca/S needs to be 1.0 or more. Ca/S is preferably 1.7 or more.
- N is an austenite-stabilizing element and an element which is effective at improving low-temperature toughness. To obtain such an effect, the N content needs to be 0.0050 % or more. On the other hand, the N content beyond 0.0500 % coarsens nitrides or carbonitrides, deteriorating toughness. Therefore, the N content is set to 0.0050 % or more and 0.0500 % or less. The N content is preferably 0.0060 % or more. The N content is preferably 0.0400 % or less. The N content is more preferably 0.0060 % or more and 0.0400 % or less.
- O deteriorates low-temperature toughness through the formation of oxides. Therefore, the O content is set to 0.0050 % or less. The O content is preferably 0.0045 % or less. Excessive reducing the O content involves high refining cost and is economically disadvantageous. Therefore, the O content is desirably 0.0003 % or more.
- Ti and Nb form carbonitrides with a high melting point in steel to prevent coarsening of crystal grains, then becoming an origin of fracture and a propagation path of cracks. In particular, in high-Mn steel, Ti and Nb hinder microstructural control for enhancing low-temperature toughness and improving ductility, and thus, need to be intentionally limited. Specifically, Ti and Nb are components which are inevitably introduced with raw materials and other sources, and Ti of more than 0.005 % and 0.010 % or less and Nb of more than 0.005 % and 0.010 % or less are typically introduced into steel. Thus, according to the method described below, it is necessary to avoid inevitable introduction of Ti and Nb and limit the content of each of Ti and Nb to 0.0050 % or less. By limiting the content of each of Ti and Nb to 0.0050 % or less, the adverse effect of carbonitrides can be eliminated, and excellent low-temperature toughness and ductility can be guaranteed. The content of each of Ti and Nb is preferably set to less than 0.0050 %, and more preferably 0.003 % or less.
- Cu has an effect of improving chloride stress corrosion cracking resistance under an environment with low chloride concentration. From this point of view, a Cu content of 0.2 % or more is effective. On the other hand, Cu conversely deteriorates chloride stress corrosion cracking resistance under an environment with high chloride concentration. Therefore, when Cu is contained, the Cu content is set to less than 2.0 %. A Cu content of less than 0.2 % does not produce an effect on stress corrosion cracking properties, and a Cu content of 2.0 % or more causes the above problem and incurs cost increase. The Cu content is preferably 0.3 % or more. The Cu content is preferably 0.8 % or less. The Cu content is more preferably 0.3 % or more and 0.8 % or less.
- Here, in high Mn steel containing Cu and Ni, in order to ensure excellent chloride corrosion cracking resistance regardless of the chloride concentration, it is important to control the Cu and Ni contents within the range described above and additionally optimize the balance between the Cu content and the Ni content so as to satisfy 0 < Cu/Ni ≤ 2. In the case of Cu/Ni > 2, the Ni content is excessively small relative to the Cu content and excellent chloride stress corrosion cracking resistance cannot be achieved under an environment with high chloride concentration.
- The balance other than the aforementioned essential components is Fe and inevitable impurities. The inevitable impurities include H, and a total content of 0.01 % or less may be allowed.
- In this disclosure, in order to further improve strength and low-temperature toughness, the following elements can be contained as necessary in addition to the above essential components:
at least one selected from the group consisting of Mo: 2.0 % or less, V: 2.0 % or less, W: 2.0 % or less, Mg: 0.0005 % or more and 0.0050 % or less, REM: 0.0010 % or more and 0.0200 % or less. - Mo, V, and W stabilize austenite and improve base metal strength. To obtain such effects, Mo, V, and/or W is preferably contained in an amount of 0.001 % or more. On the other hand, when the content of each added element is beyond 2.0 %, coarse carbonitrides are generated, which may become an origin of fracture, and additionally increase manufacturing cost. Therefore, when any of these alloying elements is/are added, the content of each added element is preferably 2.0 % or less. The content of each added element is more preferably 0.003 % or more. The content of each added element is preferably 1.7 % or less, and more preferably 1.5 % or less. Further, the content of each added element is preferably 0.003 % or more and 1.7 % or less, and more preferably 0.003 % or more and 1.5 % or less.
- Mg and REM are elements useful for morphological control of inclusions and can be contained as necessary. The morphological control of inclusions means granulating elongated sulfide inclusions. The morphological control of inclusions improves ductility, toughness, and sulfide stress corrosion cracking resistance. To obtain such effects, Mg is preferably contained in an amount of 0.0005 % or more and REM is preferably contained in an amount of 0.0010 % or more. On the other hand, when these elements are contained in a large amount, not only the amount of nonmetallic inclusions may be increased, ending up deteriorating ductility, toughness, and sulfide stress corrosion cracking resistance, but also an economic disadvantage may be entailed. Therefore, when Mg are contained, the Mg content is preferably 0.0005 % or more. The Mg content is preferably 0.0050 % or less. When REM is contained, the REM content is preferably 0.0010 % or more. The REM content is preferably 0.0200 % or less. The Mg content is more preferably 0.0010 % or more. The Mg content is more preferably 0.0040 % or less. The Mg content is further preferably 0.0010 % or more and 0.0040 % or less. The REM content is more preferably 0.0020 % or more. The REM content is more preferably 0.0150 % or less. The REM content is further preferably 0.0020 % or more and 0.0150 % or less.
- When a steel material has a body centered cubic (bcc) crystal structure, the steel material may cause brittle fracture in a low-temperature environment, and thus, is not suitable for use in a low-temperature environment. When the steel material is assumed to be used in a low-temperature environment, the steel material is required to have, as a matrix, an austenite microstructure, which has a face centered cubic (fcc) crystal structure. As used herein, the terms of "containing austenite as a matrix" means that the area ratio of austenite phase is 90 % or more. The remainder besides the austenite phase is ferrite or martensite phase. Of course, the area ratio of the austenite phase may be 100 %.
- The manufacturing method of high-Mn steel of this disclosure comprises: heating a steel material having the aforementioned chemical composition; hot rolling the heated steel material to obtain a hot-rolled plate; and subjecting the hot-rolled plate to cooling treatment. Further, in the manufacturing method of high-Mn steel of this disclosure, the temperature range in the heating of the steel material is 1100 °C to 1300 °C, the rolling finish temperature in the hot rolling is 750 °C or higher and lower than 950 °C, and the average cooling rate from a temperature at or above (the rolling finish temperature - 100 °C) to a temperature range of 300 °C to 650 °C in the cooling treatment is 0.5 °C/s or more.
- In manufacturing the high-Mn steel of this disclosure, the steel material can be obtained from molten steel having the aforementioned chemical composition which is prepared by steelmaking using a publicly-known method such as using a converter or an electric heating furnace. In addition, the high-Mn steel may also be subjected to secondary refinement in a vacuum degassing furnace. During the secondary refinement, to limit the contents of Ti and Nb which hinder suitable microstructural control within the aforementioned range, it is necessary to prevent Ti and Nb from being inevitably introduced with raw materials and other sources so as to reduce the contents of Ti and Nb. For example, by reducing the basicity of slag during the refining stage, these alloy elements are concentrated in the slag to be discharged, thus reducing Ti and Nb concentrations in a final slab product. Alternatively, the molten steel can be oxidized by blowing in oxygen, and the Ti and Nb alloys can be suspended and separated during reflux. Subsequently, it is preferable to make the steel into a steel material such as a slab having a determined size by a publicly-known steelmaking method such as continuous casting or ingot casting. The slab after continuous casting may be subjected to blooming to obtain a steel material.
- Further, manufacturing conditions are specifically defined below to make the aforementioned steel material into a steel material exhibiting high strength, excellent low-temperature toughness and ductility.
- To coarsen the crystal grain size in the microstructure of the steel material, the heating temperature before hot rolling is set to 1100 °C or higher. However, the heating temperature beyond 1300 °C may trigger local melting. Thus, the upper limit of the heating temperature is set to 1300 °C. The temperature is controlled based on a surface temperature of the steel material.
- The steel material (steel ingot or a billet) is heated and subsequently subjected to hot rolling. To make coarse crystal grains, it is preferable to increase the accumulated rolling reduction ratio at high temperature. That is, hot rolling at low temperature refines the microstructure and excessively introduces working strain, thus deteriorating low-temperature toughness. Therefore, the lower limit of the rolling finishing temperature in the hot rolling is set to 750 °C in terms of a surface temperature of the steel plate. On the other hand, finishing of rolling in a temperature range of 950 °C or higher will result in excessively coarse grain size, and thus desired yield stress cannot be obtained. Therefore, final finish rolling needs to be performed in one pass or more at lower than 950 °C.
- Average cooling rate from a temperature at or above (the rolling finish temperature - 100 °C) to a temperature range of 300 °C to 650 °C: 0.5 °C/s or more
After the hot rolling, cooling is immediately performed. Slowly cooling the steel plate after the hot rolling promotes formation of precipitates, thus deteriorating low-temperature toughness. Cooling the steel plate at a cooling rate of 0.5 °C/s or more in a predetermined temperature range can prevent formation of these precipitates. Further, excessive cooling distorts the steel plate, deteriorating productivity. Therefore, the upper limit of the cooling start temperature can be set at 900 °C. Further, the lower limit of the cooling start temperature is set at (the rolling finish temperature - 100 °C). Starting the cooling from a temperature lower than this temperature promotes formation of precipitates after the hot rolling, thus deteriorating low-temperature toughness. Further, the cooling end temperature is within a temperature range of 300 °C to 650 °C. This is because cooling to the above temperature range can suppress the precipitation of carbides which lower toughness. For the aforementioned reasons, in the cooling after the hot rolling, the average cooling rate at a surface of the steel plate from a temperature at or above (the rolling finish temperature - 100 °C) in terms of a surface temperature of the steel plate to a temperature range of 300 °C to 650 °C is set to 0.5 °C/s or more. On the other hand, from the viewpoint of industrial production, the average cooling rate is preferably 200 °C/s or less. The cooling rate is calculated as an average cooling rate of the steel plate by simulation calculation based on the temperature change of its surface. - Furthermore, in the aforementioned casting process, during the cooling, the cooling time in the temperature range of 1400 °C to 1300 °C in terms of a surface temperature of the steel is preferably controlled to 100 s or less. Controlling the cooling time in the casting process as described above promotes composite precipitation of MnS containing Ca-based inclusions such as Ca(O,S) as nucleus and the number of (Ca,Mn)S is increased. As a result, MnS does not grow at crystal grain boundaries or within crystal grains and thus the ratio of elongated MnS is lowered. Through such morphological control of Ca-based inclusions, high-Mn steel having a good reduction of area as high as 51 % or more can be obtained.
- This disclosure will be described in further detail below by way of Examples. Note that this disclosure is not limited to the following examples.
- Steel slabs having the chemical compositions listed in Table 1 were made as steel materials by a process for refining with converter and ladle and continuous casting. Next, the obtained steel slabs were subjected to blooming and hot rolling to obtain steel plates having a thickness up to 32 mm under the conditions listed in Table 2. Tensile properties, toughness, and microstructures of the steel plates were evaluated as described below.
- JIS NO. 4 tensile test pieces were collected from the obtained steel plates having a plate thickness of more than 15 mm. Round bar tensile test pieces having a parallel portion diameter of 6 mm and a gauge length of 25 mm were collected from the obtained steel plates having a plate thickness of less than 15 mm. Then, the test pieces were subjected to a tensile test to investigate tensile test properties. In this disclosure, when a test piece had a yield stress of 400 MPa or more and a tensile strength of 800 MPa or more, the corresponding steel plate was determined to have excellent tensile properties and high strength. Further, when a test piece had a reduction of area of 50 % or more, the corresponding steel plate was determined to have excellent ductility.
- Charpy V-notch full-sized test pieces were taken from the direction parallel to the rolling direction at a position from the steel plate surface to a depth of 1/4 of the plate thickness (hereinafter, referred to as 1/4 position of the plate thickness) of each steel plate over 20 mm in thickness, or at a position from the steel plate surface to a depth of 1/2 of the plate thickness (hereinafter, referred to as 1/2 position of the plate thickness) of each steel plate not over 20 mm in thickness, in conformity with JIS Z 2202 (1998). Then, the test pieces were subjected to the Charpy impact test in conformity with JIS Z 2242 (1998), where three test pieces were used for each steel plate, to determine absorbed energy at -196 °C and evaluate base metal toughness. In this disclosure, when the three test pieces had an average absorbed energy (vE-196) of 100 J or more, the corresponding steel plate was determined to have excellent base metal low-temperature toughness. For steel plates having a plate thickness of less than 10 mm, Charpy V-notch half-sized test pieces were collected from the steel plates and similarly subjected to the Charpy impact test. For steel plates having a plate thickness of less than 10 mm, when the test pieces had an average absorbed energy of 20 J or more, the corresponding steel plate was determined to have excellent base metal low-temperature toughness.
- Stress corrosion cracking resistance of samples 32 and 33 was evaluated in a boiling magnesium chloride solution in conformity with ASTM G36 (herein, it may be referred to "Boiling magnesium chloride solution test"). As the test piece, a U-bending test piece in conformity with ASTM G30 Example a was used. A test piece of 2.5 mm thick × 20 mm wide × 80 mm long was taken in the C-direction from a position of 1 mm below the surface of each steel plate. The test piece was bent at the center thereof in the longitudinal direction with 5R and subjected to the test.
- The test time was 400 hours. After the test, test pieces with no cracks observed on the surface thereof was judged to have excellent chloride stress corrosion cracking resistance. In Table 3, cases where no cracks were visually observed on the surface are indicated as "good", and cases where cracks were visually observed on the surface as "poor".
- High-Mn steel of this disclosure was confirmed to satisfy the aforementioned desired performance (a base metal yield stress of 400 MPa or more, a reduction of area of 50 % or more, an average absorbed energy (vE-196) of 100 J or more (20 J or more for a half-sized test piece) for low-temperature toughness). On the other hand, the comparative examples out of the scope of this disclosure did not satisfy the aforementioned desired performance in terms of one or more of yield stress, reduction of area, and low-temperature toughness.
- Further, sample 32, in which Cu and Ni were contained so that Cu/Ni was within the predetermined range. exhibited excellent chloride stress corrosion cracking resistance. On the other hand, in sample 33 where Cu/Ni was outside the predetermined range, sufficient chloride stress corrosion cracking resistance could not be confirmed.
[Table 2] Sample No. Steel No. Cooling time from 1400 °C to 1300 °C during casting Plate thickness Hot rolling method Remarks Heating temperature of steel material Rolling finish temperature Cooling start temperature Average cooling rate to temperature range of 300 °C to 650 °C (s) (mm) (°C) (°C) (°C) (°C/s) 1 A 20 32 1160 863 836 8 Example 2 B 50 23 1180 825 795 11 Example 3 C 60 12 1150 781 726 13 Example 4 D 80 21 1120 792 760 10 Example 5 E 20 24 1130 860 830 9 Example 6 F 30 14 1130 842 787 11 Example 7 G 30 8 1260 885 821 15 Example 8 H 40 9 1200 832 773 12 Example 9 I 50 14 1140 828 772 4 Example 10 J 70 29 1160 858 831 0.9 Example 11 K 30 11 1110 755 705 11 Example 12 J 20 12 1150 775 723 11 Example 13 L 30 19 1230 765 733 8 Comparative Example 14 M 50 30 1180 885 858 7 Comparative Example 15 N 30 13 1100 820 765 11 Comparative Example 16 O 40 24 1130 853 823 9 Comparative Example 17 P 50 20 1190 804 761 6 Comparative Example 18 R 20 20 1150 801 764 9 Comparative Example 19 S 40 14 1110 814 758 11 Comparative Example 20 T 30 28 1150 852 828 2 Comparative Example 21 C 50 11 1170 669 614 10 Comparative Example 22 D 20 18 1220 807 775 0.3 Comparative Example 23 E 30 24 1020 853 823 10 Comparative Example 24 U 50 10 1120 760 713 11 Comparative Example 25 V 30 12 1180 805 742 12 Example 26 W 20 22 1150 773 738 10 Comparative Example 27 X 30 10 1090 741 693 12 Comparative Example 28 A 50 30 1290 984 952 8 Comparative Example 29 Y 20 8 1130 852 796 12 Comparative Example 30 Z 30 28 1150 821 788 9 Comparative Example 31 A 300 32 1160 863 836 8 Example 32 AA 20 30 1100 900 850 10 Example 33 BB 30 30 1100 900 850 10 Reference Example [Table 3] Sample No. Steel No. Yield stress (MPa) Tensile strength (MPa) Reduction of area (%) Absorbed energy at ―196 °C (VE-196) (J) Boiling magnesium chloride solution test Remarks 1 A 421 854 55 137 - Example 2 B 548 940 57 121 - Example 3 C 568 970 60 119 - Example 4 D 562 956 53 116 - Example 5 E 483 885 52 137 - Example 6 F 455 855 55 141 - Example 7 G 421 940 59 62∗ - Example 8 H 506 967 57 54∗ - Example 9 I 449 850 51 127 - Example 10 J 404 842 64 133 - Example 11 K 569 969 56 116 - Example 12 J 559 953 61 127 - Example 13 L 625 974 51 58 - Comparative Example 14 M 357 817 55 127 - Comparative Example 15 N 445 869 51 36 - Comparative Example 16 O 450 882 54 72 - Comparative Example 17 P 523 939 50 79 - Comparative Example 18 R 521 939 53 48 - Comparative Example 19 S 449 849 52 83 - Comparative Example 20 T 419 854 52 75 - Comparative Example 21 C 670 1061 54 42 - Comparative Example 22 D 541 942 54 67 - Comparative Example 23 E 479 879 53 69 - Comparative Example 24 U 553 942 44 108 - Comparative Example 25 V 553 962 51 126 - Example 26 W 583 960 48 108 - Comparative Example 27 X 579 982 45 112 - Comparative Example 28 A 369 847 54 139 - Comparative Example 29 Y 501 994 55 17 ∗ - Comparative Example 30 Z 428 848 50 35 - Comparative Example 31 A 421 854 50 112 - Example 32 AA 435 851 55 105 good Example 33 BB 437 853 60 120 poor Reference Example ∗ half-sized test piece
Claims (5)
- High-Mn steel comprising:a chemical composition containing, in mass%,C: 0.10 % or more and 0.70 % or less,Si: 0.10 % or more and 0.90 % or less,Mn: 20 % or more and 30 % or less,P: 0.030 % or less,S: 0.0070 % or less,Al: 0.01 % or more and 0.07 % or less,Cr: 1.8 % or more and 7.0 % or less,Ni: 0.01 % or more and less than 1.0 %,Ca: 0.0005 % or more and 0.010 % or less,N: 0.0050 % or more and 0.0500 % or less,O: 0.0050 % or less,Ti: 0.0050 % or less, andNb: 0.0050 % or less, within a range satisfying the following formula (1), with the balance being Fe and inevitable impurities,a microstructure containing austenite as a matrix;a yield stress of 400 MPa or more; andan average Charpy impact absorbed energy at -196 °C of 100 J or more for a full-sized test piece and 20 J or more for a half-sized test piece.
- The High-Mn steel according to claim 1, wherein the chemical composition further contains, in mass%, at least one selected from the group consisting ofCu: less than 2.0 %,Mo: 2.0 % or less,V: 2.0 % or less,W: 2.0 % or less,Mg: 0.0005 % or more and 0.0050 % or less, andREM: 0.0010 % or more and 0.0200 % or less.
- A manufacturing method of high-Mn steel, comprising: heating a steel material having the chemical composition according to claim 1 or 2 to a temperature range of 1100 °C to 1300 °C; then hot rolling the steel material with a rolling finish temperature of 750 °C or higher and lower than 950 °C to obtain a hot-rolled plate; and then subjecting the hot-rolled plate to cooling treatment at an average cooling rate of 0.5 °C/s or more from a temperature at or above (the rolling finish temperature - 100 °C) to a temperature range of 300 °C to 650 °C.
- High-Mn steel comprising:
a chemical composition containing, in mass%,C: 0.10 % or more and 0.70 % or less,Si: 0.10 % or more and 0.90 % or less,Mn: 20 % or more and 30 % or less,P: 0.030 % or less,S: 0.0070 % or less,Al: 0.01 % or more and 0.07 % or less,Cr: 1.8 % or more and 7.0 % or less,Cu: 0.2 % or more and less than 2.0 %Ni: 0.1 % or more and less than 1.0 %,Ca: 0.0005 % or more and 0.010 % or less,N: 0.0050 % or more and 0.0500 % or less,O: 0.0050 % or less,Ti: 0.0050 % or less and - A manufacturing method of high-Mn steel, comprising: heating a steel material having the chemical composition according to claim 4 to a temperature range of 1100 °C to 1300 °C; then hot rolling the steel material with a rolling finish temperature of 750 °C or higher and lower than 950 °C to obtain a hot-rolled plate; and then subjecting the hot-rolled plate to cooling treatment at an average cooling rate of 0.5 °C/s or more from a temperature at or above (the rolling finish temperature - 100 °C) to a temperature range of 300 °C to 650 °C.
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