US20220033944A1 - Cr-based stainless steel having excellent hydrogen embrittlement resistance - Google Patents
Cr-based stainless steel having excellent hydrogen embrittlement resistance Download PDFInfo
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- US20220033944A1 US20220033944A1 US17/312,693 US201917312693A US2022033944A1 US 20220033944 A1 US20220033944 A1 US 20220033944A1 US 201917312693 A US201917312693 A US 201917312693A US 2022033944 A1 US2022033944 A1 US 2022033944A1
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- stainless steel
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- 229910001220 stainless steel Inorganic materials 0.000 title claims abstract description 64
- 239000010935 stainless steel Substances 0.000 title claims abstract description 63
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 title claims description 140
- 229910052739 hydrogen Inorganic materials 0.000 title claims description 122
- 239000001257 hydrogen Substances 0.000 title claims description 122
- 239000013078 crystal Substances 0.000 claims abstract description 31
- 238000005096 rolling process Methods 0.000 claims abstract description 27
- 229910000831 Steel Inorganic materials 0.000 claims description 52
- 239000010959 steel Substances 0.000 claims description 52
- 229910052751 metal Inorganic materials 0.000 claims description 11
- 239000002184 metal Substances 0.000 claims description 11
- 150000002739 metals Chemical class 0.000 claims description 10
- 239000012535 impurity Substances 0.000 claims description 8
- 229910052742 iron Inorganic materials 0.000 claims description 3
- 239000011651 chromium Substances 0.000 description 62
- 230000009467 reduction Effects 0.000 description 19
- 230000000694 effects Effects 0.000 description 17
- 239000000463 material Substances 0.000 description 16
- 229910052758 niobium Inorganic materials 0.000 description 14
- 229910052719 titanium Inorganic materials 0.000 description 14
- 238000005097 cold rolling Methods 0.000 description 13
- 229910052761 rare earth metal Inorganic materials 0.000 description 13
- 230000007704 transition Effects 0.000 description 12
- 229910000963 austenitic stainless steel Inorganic materials 0.000 description 10
- 238000004519 manufacturing process Methods 0.000 description 10
- 238000005204 segregation Methods 0.000 description 10
- 239000000203 mixture Substances 0.000 description 9
- 229910052698 phosphorus Inorganic materials 0.000 description 9
- 238000005482 strain hardening Methods 0.000 description 9
- 238000012360 testing method Methods 0.000 description 9
- 229910052718 tin Inorganic materials 0.000 description 9
- 239000000126 substance Substances 0.000 description 8
- 238000000137 annealing Methods 0.000 description 7
- 229910052796 boron Inorganic materials 0.000 description 7
- 230000007423 decrease Effects 0.000 description 7
- 230000003993 interaction Effects 0.000 description 7
- 229910052717 sulfur Inorganic materials 0.000 description 7
- 238000009864 tensile test Methods 0.000 description 7
- 229910052727 yttrium Inorganic materials 0.000 description 7
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 6
- 238000001887 electron backscatter diffraction Methods 0.000 description 6
- 238000011156 evaluation Methods 0.000 description 6
- 239000000446 fuel Substances 0.000 description 6
- 229910052735 hafnium Inorganic materials 0.000 description 6
- 238000005098 hot rolling Methods 0.000 description 6
- 229910052746 lanthanum Inorganic materials 0.000 description 6
- 229910052750 molybdenum Inorganic materials 0.000 description 6
- 229910045601 alloy Inorganic materials 0.000 description 5
- 239000000956 alloy Substances 0.000 description 5
- 229910052802 copper Inorganic materials 0.000 description 5
- 238000005260 corrosion Methods 0.000 description 5
- 230000007797 corrosion Effects 0.000 description 5
- 229910052733 gallium Inorganic materials 0.000 description 5
- 238000005259 measurement Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 5
- 229910052759 nickel Inorganic materials 0.000 description 5
- 229910052757 nitrogen Inorganic materials 0.000 description 5
- 238000007670 refining Methods 0.000 description 5
- 229910052721 tungsten Inorganic materials 0.000 description 5
- 229910052720 vanadium Inorganic materials 0.000 description 5
- 229910052726 zirconium Inorganic materials 0.000 description 5
- 229910000838 Al alloy Inorganic materials 0.000 description 4
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 4
- 230000000052 comparative effect Effects 0.000 description 4
- 238000009792 diffusion process Methods 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 238000001953 recrystallisation Methods 0.000 description 4
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 3
- 238000010521 absorption reaction Methods 0.000 description 3
- 229910052787 antimony Inorganic materials 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 3
- 230000002349 favourable effect Effects 0.000 description 3
- 150000002431 hydrogen Chemical class 0.000 description 3
- 239000011261 inert gas Substances 0.000 description 3
- 230000000149 penetrating effect Effects 0.000 description 3
- 238000002791 soaking Methods 0.000 description 3
- 238000007711 solidification Methods 0.000 description 3
- 230000008023 solidification Effects 0.000 description 3
- 229910000859 α-Fe Inorganic materials 0.000 description 3
- 229910000851 Alloy steel Inorganic materials 0.000 description 2
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 2
- 230000002411 adverse Effects 0.000 description 2
- 230000004888 barrier function Effects 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 229910002092 carbon dioxide Inorganic materials 0.000 description 2
- 239000001569 carbon dioxide Substances 0.000 description 2
- 229910052804 chromium Inorganic materials 0.000 description 2
- 230000003749 cleanliness Effects 0.000 description 2
- 239000010960 cold rolled steel Substances 0.000 description 2
- 238000002425 crystallisation Methods 0.000 description 2
- 230000008025 crystallization Effects 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 238000004090 dissolution Methods 0.000 description 2
- 229910001039 duplex stainless steel Inorganic materials 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 238000009863 impact test Methods 0.000 description 2
- 229910052748 manganese Inorganic materials 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 150000001247 metal acetylides Chemical class 0.000 description 2
- 230000035515 penetration Effects 0.000 description 2
- 238000001556 precipitation Methods 0.000 description 2
- 238000011160 research Methods 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000006104 solid solution Substances 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- 239000000758 substrate Substances 0.000 description 2
- 229910021364 Al-Si alloy Inorganic materials 0.000 description 1
- 229910000975 Carbon steel Inorganic materials 0.000 description 1
- 229910052684 Cerium Inorganic materials 0.000 description 1
- 229910052765 Lutetium Inorganic materials 0.000 description 1
- 238000009825 accumulation Methods 0.000 description 1
- 230000033228 biological regulation Effects 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 239000010962 carbon steel Substances 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical compound [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000007598 dipping method Methods 0.000 description 1
- 229910001651 emery Inorganic materials 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 239000005431 greenhouse gas Substances 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 229910052747 lanthanoid Inorganic materials 0.000 description 1
- 150000002602 lanthanoids Chemical class 0.000 description 1
- OHSVLFRHMCKCQY-UHFFFAOYSA-N lutetium atom Chemical compound [Lu] OHSVLFRHMCKCQY-UHFFFAOYSA-N 0.000 description 1
- 229910000734 martensite Inorganic materials 0.000 description 1
- 229910001105 martensitic stainless steel Inorganic materials 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 239000003960 organic solvent Substances 0.000 description 1
- 230000000737 periodic effect Effects 0.000 description 1
- 238000005554 pickling Methods 0.000 description 1
- 238000004881 precipitation hardening Methods 0.000 description 1
- 230000002441 reversible effect Effects 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 229910052706 scandium Inorganic materials 0.000 description 1
- SIXSYDAISGFNSX-UHFFFAOYSA-N scandium atom Chemical compound [Sc] SIXSYDAISGFNSX-UHFFFAOYSA-N 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 150000003568 thioethers Chemical class 0.000 description 1
- 238000010792 warming Methods 0.000 description 1
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 description 1
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- 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
- C22C38/52—Ferrous alloys, e.g. steel alloys containing chromium with nickel with cobalt
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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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- 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
- C22C38/60—Ferrous alloys, e.g. steel alloys containing lead, selenium, tellurium, or antimony, or more than 0.04% by weight of sulfur
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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
- C21D2201/00—Treatment for obtaining particular effects
- C21D2201/05—Grain orientation
Definitions
- the present invention relates to a Cr-based stainless steel sheet with excellent hydrogen embrittlement resistance, specifically to a Cr-based stainless steel sheet suitable for metals for high pressure hydrogen gaseous equipment.
- Non-Patent Literature 1 discloses hydrogen embrittlement properties of all steel materials including stainless steel that are evaluated in a high pressure hydrogen gas at room temperature.
- Typical austenitic stainless steel SUS304 and the Cr-based stainless steel are reported to be prone to hydrogen embrittlement. Accordingly, use of SUS316L and SUS316 is also typically recommended in the high pressure hydrogen gas at a pressure of about 20 MPa.
- the Cr-based stainless steel having a body-centered cubic structure decreases in toughness at a low temperature (lower than or equal to a room temperature) (i.e., low-temperature embrittlement) as compared with the austenitic stainless steel having a face-centered cubic structure.
- Patent Literature 3 discloses a pressure tank for high pressure hydrogen gas and high pressure hydrogen gaseous piping, which are coated with Al or an Al alloy. Examples thereof concern formation of a film on the austenitic stainless steel and duplex stainless steel including an austenitic phase but do not disclose formation of a film on a steel material that is prone to hydrogen embrittlement (e.g., the Cr-based stainless steel) and hydrogen penetration properties thereof.
- Patent Literature 4 discloses a substrate for hydrogen equipment obtained by: hot-dipping a steel material that is by itself prone to hydrogen embrittlement with the use of an Al-Si alloy added with Si in an amount in a range from 1 to 5%; and forming a hydrogen-impermeable film.
- the steel material for the substrate is set as carbon steel, low alloy steel or the Cr-based stainless steel, which prevents hydrogen embrittlement and keeps a manufacturing cost low.
- Examples thereof are limited to SUS304, SUS630 (15Cr-4Ni-3Cu) and SCM435 (low alloy steel). Hydrogen embrittlement properties and use of the Cr-based stainless steel sheet having high economic efficiency are also not disclosed.
- Patent Literature 1 JP 2014-114471 A
- Patent Literature 2 JP 2016-183412 A
- Patent Literature 3 JP 2004-324800 A
- Patent Literature 4 WO 2015-098981
- Non-Patent Literature 1 PVP2007-26820
- Non-Patent Literature 2 Michihiko Nagumo, “Fundamentals of Hydrogen Embrittlement”, Uchida Rokakuho (December 2008)
- Patent Literatures 1 to 4 is only austenitic stainless steel, duplex stainless steel and SUS630 (precipitation hardening type).
- the Cr-based stainless steel disclosed in Non-Patent Literature 1 is prone to hydrogen embrittlement and thus does not have hydrogen embrittlement resistance for use in the high pressure hydrogen gas.
- the Cr-based stainless steel also has a problem of the low-temperature embrittlement.
- an object of the invention is to provide a Cr-based stainless steel sheet with excellent hydrogen embrittlement resistance, the Cr-based stainless steel sheet having hydrogen embrittlement resistance for use in a high pressure hydrogen gas and thus being suitable for metals for high pressure hydrogen gaseous equipment.
- an object thereof is to achieve low-temperature embrittlement resistance together with hydrogen embrittlement resistance.
- the invention adopts a configuration below.
- a Cr-based stainless steel sheet having excellent low-temperature toughness together with excellent hydrogen embrittlement resistance can be provided. Further, the Cr-based stainless steel sheet according to the invention can be suitably used for metals for the high pressure hydrogen gaseous equipment.
- the inventors have intensely studied an influence of alloy elements and a texture on hydrogen embrittlement resistance and low-temperature embrittlement resistance in a Cr-based stainless steel sheet, thereby obtaining the following novel findings to arrive at the invention.
- hydrogen embrittlement is a phenomenon that a fracture of the metals progresses due to an interaction between hydrogen penetrating into the steel material from the high pressure hydrogen gas and plastic deformation.
- Hydrogen-Enhanced Strain-Induced Vacancy Theory which states that the interaction between hydrogen and plastic deformation promotes generation of vacancy-type lattice defects in the steel to progress the fracture, is considered as reliable in explaining a mechanism of hydrogen embrittlement (Non-Patent Literature 2).
- Non-Patent Literature 2 Hydrogen-Enhanced Strain-Induced Vacancy Theory
- the Cr amount is reduced to 18% or less in the invention.
- the inventors have found that added amounts of Si, Mn, P, Ti and Nb are preferably controlled to be in respective predetermined ranges.
- a Cr-based stainless steel sheet is a Cr-based stainless steel sheet with excellent hydrogen embrittlement resistance and low-temperature embrittlement resistance, the Cr-based stainless steel sheet including: 0.020 mass % or less of C; 1.00 mass % or less of Si; 1.00 mass % or less of Mn; 0.040 mass % or less of P; 0.0030 mass % or less of S, 10.0 to 18.0 mass % of Cr; 0.020 mass % or less of N; 0.10 mass % or less of Al; one or both of 0.5 mass % or less of Nb and 0.5 mass % or less of Ti; and a balance consisting of Fe and impurities, in which a texture in a sheet surface of the chromium stainless sheet satisfies (i) and (ii) below.
- the Cr-based stainless steel sheet according to the exemplary embodiment further contains 0.001 to 0.3 mass % of Sn and 0.005 mass % or less of B, and satisfies Formula (1) below.
- the Cr-based stainless steel sheet according to the exemplary embodiment may further contain one or more selected from 1 mass % or less of Ni, 1 mass % or less of Cu, 1 mass % or less of Mo, 0.2 mass % or less of Sb, 0.5 mass % or less of V, 0.5 mass % or less of W, 0.5 mass % or less of Zr, 0.5 mass % or less of Co, 0.005 mass % or less of Mg, 0.005 mass % or less of Ca, 0.020 mass % or less of Ga, 0.1 mass % or less of La, 0.1 mass % or less of Y, 0.1 mass % or less of Hf, and 0.1 mass % or less of REM.
- the Cr-based stainless steel sheet according to the exemplary embodiment is used for metals for high pressure hydrogen gaseous equipment.
- C is 0.020% or less.
- C increases work-hardening of steel through solid-dissolution thereof and precipitation of carbides to deteriorate hydrogen embrittlement resistance. C further decreases toughness to deteriorate low-temperature embrittlement resistance.
- the C content is preferably as small as possible and thus has an upper limit of 0.020% or less.
- a reduction in the C content requires a complex refining process, thereby resulting in an increase in cost.
- the C content is preferably 0.001% or more.
- the C content is preferably in a range from 0.003 to 0.015%, more preferably in a range from 0.003 to 0.010%.
- Si is 1.00% or less.
- Si is an effective deoxidizing element.
- excessive addition of Si increases solid solution strengthening and work-hardening, thereby resulting in a reduction in hydrogen embrittlement resistance and low-temperature embrittlement resistance.
- an upper limit of the Si content is set at 1.00% or less.
- a lower limit of the Si content is preferably 0.01% or more.
- the Si content is preferably in a range from 0.05 to 0.50% and may be in a range from 0.05 to 0.30%.
- Mn is 1.00% or less.
- Mn is an effective deoxidizing element and also an element effective in achieving low-temperature embrittlement resistance through improvement in toughness by fixing S.
- an upper limit of the Mn content is set at 1.00% or less.
- a lower limit of the Mn content is preferably 0.01% or more.
- the Mn content is preferably in a range from 0.05 to 0.50% and may be in a range from 0.05 to 0.30%.
- P 0.040% or less.
- the P content is an element reducing low-temperature embrittlement resistance through grain boundary segregation. Accordingly, the P content is preferably as small as possible, and thus has an upper limit of 0.040% or less. However, an excessive reduction in the P content results in an increase in a refining cost. Accordingly, a lower limit of the P content is preferably 0.005% or more. In view of production cost and properties, the P content is more preferably in a range from 0.010 to 0.030% and may be in a range from 0.010 to 0.020%.
- S is 0.0030% or less.
- the S content is preferably as small as possible, and thus has an upper limit of 0.0030% or less.
- an excessive reduction in the S content results in an increase in material and refining costs.
- a lower limit of the S content is preferably 0.0001% or more.
- the S content is more preferably in a range from 0.0002 to 0.0015% and may be in a range from 0.0002 to 0.0008%.
- Cr is a basic element in the Cr-based stainless steel according to the exemplary embodiment and is also an essential element for maintaining hydrogen embrittlement resistance and low-temperature embrittlement resistance in addition to corrosion resistance of the steel.
- a lower limit of the Cr content is set at 10.0% or more.
- an upper limit of the Cr content is set at 18.0% or less.
- the Cr content may be more preferably 11.0 or more and less than 17.0% or in a range from 12.0 to 15.0%.
- N 0.020% or less.
- N increases work-hardening of steel through solid dissolution thereof and precipitation of carbides to deteriorate hydrogen embrittlement resistance.
- the N content decreases toughness to deteriorate low-temperature embrittlement resistance. Accordingly, the N content is preferably as small as possible and thus has an upper limit of 0.020% or less. However, a reduction in the N content requires a complex refining process, thereby resulting in an increase in cost. Accordingly, the N content is preferably 0.001% or more. In view of properties and production cost, the N content is preferably in a range from 0.005 to 0.015%.
- Al is 0.10% or less.
- Al is a highly effective deoxidizing element.
- Al decreases toughness of steel to deteriorate low-temperature embrittlement resistance and sometimes causes the texture to fall outside the preferable ranges of the invention.
- an upper limit of the Al content is set at 0.10% or less.
- a lower limit of the Al content is preferably 0.005% or more.
- the Al content is preferably in a range from 0.01 to 0.07% and may be in a range from 0.01 to 0.05%.
- Nb and Ti segregate at a grain boundary to suppress grain boundary segregation of P and S, thereby improving low-temperature embrittlement resistance. Further, Nb and Ti are also likely to improve hydrogen embrittlement resistance by preventing work-hardening of steel by functioning as stabilizing elements for fixing C, N, P and S. Nb and Ti both exhibit these two functions and thus are elements effective in improving hydrogen embrittlement resistance and low-temperature embrittlement resistance, which are the object of the invention. When Nb and Ti are contained, the Nb and Ti contents are each preferably 0.01% or more in order to exhibit the effects. However, excessive addition of Nb and Ti increases work-hardening, thereby resulting in a reduction in hydrogen embrittlement resistance or an increase in alloy cost.
- an upper limit of each of the Nb and Ti contents is set at 0.5% or less.
- a total content of one or both of Nb and Ti is preferably in a range from 0.05 to 0.5%.
- the total content of one or both of Nb and Ti is more preferably in a range from 0.08 to 0.4% and may be 0.1 to 0.3%.
- the Sn and B contents are further preferably in respective ranges below.
- Sn is 0.001 to 0.3%.
- Sn is an effective element for improving hydrogen embrittlement resistance and low-temperature embrittlement resistance, which are the object of the invention.
- Sn which is a grain boundary segregation element, forms a diffusion barrier at a grain boundary with hydrogen, thereby reducing an interaction between hydrogen and plastic deformation. Further, Sn suppresses segregation of P and S at a grain boundary to alleviate an adverse effect of low-temperature embrittlement resistance.
- the Sn content being in a predetermined range is likely to achieve both hydrogen embrittlement resistance and low-temperature embrittlement resistance. Accordingly, the Sn content is preferably in a range from 0.001 to 0.5% in the invention. 0.001% or more of Sn is to be contained to exhibit the above effects, thereby improving hydrogen embrittlement resistance.
- an upper limit of the Sn content is set at 0.5% or less.
- the Sn content is preferably in a range from 0.005 to 0.3% and may be in a range from 0.010 to 0.2%.
- B is 0.005% or less.
- B is a grain boundary segregation element and is also an element for improving hydrogen embrittlement resistance and low-temperature embrittlement resistance similarly to Sn. Accordingly, it is effective to contain B in the Cr-based stainless steel according to the exemplary embodiment.
- the B content is preferably 0.0003% or more in the invention.
- an upper limit of the B content is set at 0.005% or less.
- the B content is preferably in a range from 0.0005 to 0.002% and may be in a range from 0.001 to 0.002%.
- Si, Mn, P, Nb and Ti are contained in the above respective ranges and further satisfy Formula (1) below in order to improve hydrogen embrittlement resistance and low-temperature embrittlement resistance, which are the target of the invention.
- the left side of Formula (1) is less than 2.00 and a lower limit thereof is 0.05 in terms of properties and productivity.
- the left side of Formula (1) is preferably in a range from 0.35 to 1.80, more preferably in a range from 0.50 to 1.50.
- Ni is 1% or less.
- Cu is 1% or less.
- Mo is 1% or less.
- Ni, Cu and Mo are elements effective in improving corrosion resistance. Ni and Cu are also effective in improving low-temperature toughness. In order to exhibit these effects, Ni, Cu and Mo may be each contained at 0.05% or more. Excessive addition thereof increases solid solution strengthening and work-hardening of stainless steel, resulting in a reduction in hydrogen embrittlement resistance. Accordingly, an upper limit of each of the Ni, Cu and Mo contents is set at 1% or less.
- Ni, Cu and Mo contents are each more preferably in a range from 0.1% to 0.8%, further preferably in a range from 0.2% to 0.5%.
- Sb is 0.2% or less.
- V is 0.5% or less.
- W is 0.5% or less.
- Zr is 0.5% or less.
- Co 0.5% or less.
- Sb, V, W, Zr and Co are elements effective in improving corrosion resistance and also improving low-temperature embrittlement resistance by suppressing grain boundary segregation of P and S, and thus are contained as required.
- Sb is a strong grain boundary segregation element and has an effect of blocking grain boundary segregation of impurity elements such as P and S similarly to Sn and B.
- the Sb, V, W, Zr and Co contents are each preferably 0.01% or more in order to exhibit the effects. Since excessive addition thereof reduces productivity and low-temperature embrittlement resistance, the Sb content is set at 0.2% or less and V, W, Zr and Co are each set at 0.5% or less.
- Sb content is more preferably in a range from 0.02 to 0.15%, further preferably in a range from 0.02 to 0.1%.
- the V, W, Zr and Co contents are each more preferably in a range from 0.02 to 0.3%, further preferably in a range from 0.02 to 0.2%.
- Mg is 0.005% or less.
- Mg acts as a deoxidizer by forming an Mg oxide with Al in molten steel and also as a crystallization nucleus of TiN. Since TiN becomes a solidification nucleus of a ferrite phase in a solidification process, Mg facilitates crystallization of TiN to finely generate the ferrite phase in solidification. Refinement of a solidified structure also can improve low-temperature embrittlement resistance.
- the Mg content is preferably 0.0001% or more in order to exhibit the effects. However, since more than 0.005% of Mg deteriorates productivity and corrosion resistance, an upper limit of the Mg content is set at 0.005% or less.
- the Mg content is preferably in a range from 0.0003 to 0.002%, further preferably in a range from 0.0003 to 0.001%.
- Ca is 0.005% or less.
- Ga is 0.020% or less.
- Ca and Ga are elements for improving cleanliness of steel and are contained as required in order to suppress an increase in work-hardening and thereby increase hydrogen embrittlement resistance.
- the Ca and Ga contents are each preferably 0.0003% or more in order to exhibit the effects.
- an upper limit of the Ca content is set at 0.005% or less and an upper limit of the Ga content is set at 0.020% or less. It is preferable that the Ca content is in a range from 0.0003 to 0.0030% and the Ga content is in a range from 0.0030 to 0.015%.
- La is 0.1% or less.
- Y is 0.1% or less.
- Hf is 0.1% or less.
- REM is 0.1% or less.
- La, Y, Hf and REM are elements for improving cleanliness of steel similarly to Ca and Ga and may be contained as required in order to suppress an increase in work-hardening and thereby increase hydrogen embrittlement resistance.
- the La, Y, Hf and REM contents are each preferably 0.001% or more in order to exhibit the effects.
- an upper limit of the La, Y, Hf and REM contents are each set at 0.1% or less.
- the La, Y, Hf and REM contents are each preferably in a range from 0.001 to 0.05%, further preferably in a range from 0.001 to 0.03%.
- REM rare-earth elements
- Sc scandium
- Y yttrium
- lanthanoid lanthanoid from cerium (Ce) to lutetium (Lu) in the periodic table.
- impurities contained in the balance mean components mixed from ores or scraps used as a material or due to a manufacturing environment in industrially manufacturing steel, which are acceptable as long as the objects of the invention can be achieved.
- 0.1% or less of Ta, 0.01% or less of Bi, 0.05% of Zn and 0.0005% or less of H may be contained as required.
- the Cr-based stainless steel according to the exemplary embodiment contains ferrite crystal grains and further may contain martensite crystal grains.
- the texture in the sheet surface of the chromium stainless sheet according to the exemplary embodiment satisfies (i) and (ii) below.
- the ⁇ 211 ⁇ -plane orientation refers to a normal direction of the ⁇ 211 ⁇ -plane.
- the ⁇ 211 ⁇ orientation is referred to as an a-fiber, which is a rolling texture aggregated through cold-rolling. According to the invention, it has been found that it is effective to control, in the sheet surface, the area ratio and a size of the ⁇ 211 ⁇ 10-degree-oriented grains, which are frequently sites of crack generation, in order to improve hydrogen embrittlement resistance.
- the area ratio of the ⁇ 211 ⁇ 10-degree-oriented grains is set at less than 30% and an abundance ratio of a recrystallization texture in a form of a ⁇ 111 ⁇ orientation is increased in the sheet surface, thereby contributing to improving hydrogen embrittlement resistance.
- the area ratio of the ⁇ 211 ⁇ 10-degree-oriented grains is preferably in a range from 5 to 20%, more preferably in a range from 3 to 15% in terms of hydrogen embrittlement resistance and productivity.
- the size of the ⁇ 211 ⁇ 10-degree-oriented grains is set such that the length in the rolling direction and the length in the sheet width direction (rolling vertical direction) are each less than 0.15 mm on average.
- a reduction in the size of the ⁇ 211 ⁇ 10-degree-oriented grains reduces introduction of strains to and accumulation of the strains in the ⁇ 211 ⁇ 10-degree-oriented grains, thereby contributing to improving hydrogen embrittlement resistance.
- the size of the ⁇ 211 ⁇ 10-degree-oriented grains is preferably less than 0.10 mm, more preferably less than 0.07 mm in terms of hydrogen embrittlement resistance and productivity.
- the “sheet surface” refers to regions reaching at most t/8 of a thickness t of the steel sheet, i.e., regions on respective two sides of the steel sheet reaching at most a thickness 1/8t from the respective surfaces of the steel sheet in a surface direction.
- the ⁇ 211 ⁇ 10-degree-oriented grains refer to crystal grains having a crystal orientation whose orientation difference between the normal direction of the surface of the steel sheet and the ⁇ 211 ⁇ -plane orientation is 10 degrees or less.
- the texture can be analyzed using electron backscatter diffraction (hereinafter, EBSD).
- EBSD electron backscatter diffraction
- the area ratio and the grain size of the ⁇ 211 ⁇ 10-degree-oriented grains can be quantified by displaying a crystal orientation map of the crystal orientation group divided into the ⁇ 211 ⁇ 10-degree-oriented grains and other regions in the sheet surface.
- a measurement region (sheet width direction: 850 ⁇ m, rolling direction: 2250 ⁇ m) is subjected to EBSD measurement at a magnification of 100 to display the crystal orientation map of the crystal grains (i.e., the ⁇ 211 ⁇ 10-degree-oriented grains) whose orientation difference between the normal direction of the plane parallel to the surface of the steel sheet and the ⁇ 211 ⁇ -plane orientation is 10 degrees or less, whereby the area ratio and the grain size (in the rolling direction and the sheet width direction) thereof can be quantified.
- regions reaching at most t/8 of the thickness t of the steel sheet from the surface of the steel sheet are defined as an inspection surface, the texture in the sheet surface can be reproducibly evaluated.
- the hydrogen embrittlement resistance is evaluated by a slow strain rate tensile test for which a relatively slow strain rate is used.
- the strain rate is preferably 10 ⁇ 5 /s.
- the strain rate is relatively large, i.e., 10 ⁇ 4 /s or more, penetration and diffusion of hydrogen into the steel do not progress, sometimes resulting in a reduction in hydrogen embrittlement of the steel.
- the strain rate is small, i.e., 10 ⁇ 6 /s, excessive test time is required and the effect of the strain rate to hydrogen embrittlement properties is saturated.
- the hydrogen embrittlement resistance is evaluated for tensile strength and fracture elongation in the slow strain rate tensile test.
- a value of the tensile strength and the fracture elongation in the high pressure hydrogen gas is more unlikely to be lowered as compared with the value thereof in an atmosphere or in an inert gas.
- a value obtained by dividing the tensile strength in the high pressure hydrogen gas by the tensile strength in the atmosphere or in the inert gas is referred to as a “relative tensile strength”.
- a value obtained by dividing the fracture elongation in the high pressure hydrogen gas by the fracture elongation in the atmosphere or in the inert gas is referred to as a “relative elongation”.
- the relative tensile strength is 0.98 or more and the relative elongation is 0.75 or more. It is more preferable that the relative tensile strength is in a range from 0.98 to 1.05 and the relative elongation is a range from 0.85 to 1.05.
- the low-temperature embrittlement resistance is evaluated by a Charpy impact test according to JIS Z 2242. For instance, a 2-mm-thick test piece having a V-notch shape is used to measure absorption energy.
- the low-temperature embrittlement resistance is evaluated in terms of an energy transition temperature according to Annex D of JIS. A lower energy transition temperature is more favorable.
- the energy transition temperature refers to a temperature corresponding to a half value of the absorption energy at a temperature at which a fracture rate due to a ductile fracture is 100%.
- the energy transition temperature is preferably ⁇ 10 degrees or less in terms of use of the Cr-based stainless steel sheet according to the exemplary embodiment for outdoor and on-vehicle hydrogen equipment.
- the energy transition temperature is more preferably ⁇ 40 degrees or less in terms of the use thereof in a cold region.
- the hydrogen embrittlement resistance and low-temperature embrittlement resistance (the object of the invention) sometimes can be ensured even if typical process conditions such as casting, hot-rolling and cold-rolling are used for manufacturing thereof.
- the Cr-based stainless steel sheet according to the exemplary embodiment satisfies the above chemical composition and manufactured by the following method in order to improve the hydrogen embrittlement resistance by forming the texture of the invention.
- the steel having the above chemical composition is hot-rolled, annealed after the hot-rolling at a temperature of 900 degrees C. or less, subsequently cold-rolled at a rolling reduction rate of 40% or more, and is subjected to finish annealing at a temperature of more than 900 degrees C.
- the heat treatment after the hot-rolling is preferably performed at a temperature of 900 degrees C. or less, more preferably in a temperature range from 700 to 900 degrees C. in order to suppress a growth of the ⁇ 211 ⁇ -oriented grains, which are generated at the hot-rolling stage.
- the cold-rolling may be performed by a reversible 20-stage Sendzimir rolling mill, a 6 or 12-stage rolling mill, ora tandem rolling mill configured to continuously roll a plurality of passes.
- a larger work roll diameter is preferable. Accordingly, the work roll diameter is preferable 200 mm or more. Rolling with such a large-diameter roll is preferably performed in a primary cold-rolling (initial cold-rolling in a case where plural times of cold-rolling are repeatedly performed).
- the cold-rolling grows the recrystallization texture in a form of the ⁇ 111 ⁇ -oriented grains to reduce the area ratio of the rolling texture in a form of the ⁇ 211 ⁇ 10-degree-oriented grains, thereby being effective in forming the target texture of the invention.
- the cold-rolling is preferably performed at a rolling reduction rate of 40% or more. When the cold-rolling rate is less than 40%, the area ratio and the size of the ⁇ 211 ⁇ 10-degree-oriented grains in the recrystallization texture are likely to increase, sometimes resulting in a reduction in the hydrogen embrittlement resistance.
- the rolling reduction rate is preferably in a range from 40 to 90%, more preferably in a range from 50 to 80% in terms of the hydrogen embrittlement resistance and the productivity.
- the finish annealing after the cold-rolling is preferably performed through the heat treatment at a temperature of more than 900 degrees C. in order to reduce the area ratio and the size of the ⁇ 211 ⁇ -oriented grains by growing the ⁇ 111 ⁇ -oriented grains. Since an excessive temperature rise increases the size of the ⁇ 211 ⁇ 10-degree-oriented grains through the crystal grain growth, an upper limit of a finish annealing temperature is preferably 1050 degrees C.
- An atmosphere for the finish annealing is not particularly defined but preferably an atmospheric air, an LNG fuel atmosphere and a BA atmosphere.
- a soaking time for the heat treatment is preferably in a range from 10 seconds to 10 minutes.
- the soaking time is preferably 10 seconds or more in order to soften a material for the cold-rolling.
- the texture effective for the hydrogen embrittlement resistance can be ensured by suppressing the growth of the ⁇ 211 ⁇ 10-degree-oriented grains to reduce the size of the crystal grains.
- the Cr-based stainless steel was hot-rolled by being heated to a heating temperature in a range from 1150 to 1250 degrees C. to manufacture a 5.0-mm-thick hot-rolled steel sheet.
- the hot-rolled steel sheet was annealed after the hot-rolling in a temperature range from 700 to 900 degrees C. and, subsequent to being pickled, was cold-rolled in a thickness range from 1.5 to 2.5 mm to provide a cold-rolled steel sheet.
- Conditions for the cold-rolling are shown in Table 2.
- the cold-rolling was performed by a Sendzimir rolling mill and a tandem rolling mill having respective different work roll diameters.
- the former used a small diameter roll (60 mm) (indicated as “S” in Table 2) and the latter used a large diameter roll (200 mm) (indicated as “L” in Table 2).
- the cold-rolled steel sheet was subjected to finish annealing in a temperature range from 920 to 1020 degrees C. and pickling to manufacture a Cr-based stainless steel sheet.
- a texture was analyzed using EBSD.
- a crystal orientation group contributing to hydrogen embrittlement resistance was quantified by displaying a crystal orientation map of the crystal orientation group divided into ⁇ 211 ⁇ 10-degree-oriented grains and other regions in the sheet surface.
- a measurement region sheet width direction: 850 ⁇ m, rolling direction: 2250 ⁇ m
- EBSD measurement at a magnification of 100
- displayed the crystal orientation map of the crystal grains i.e., the ⁇ 211 ⁇ 10-degree-oriented grains
- the crystal orientation difference between a normal direction of the plane parallel to the surface of the steel sheet and the ⁇ 211 ⁇ -plane orientation was 10 degrees or less and also displayed a grain boundary, so that an area ratio and average grain size (in the rolling direction and the sheet width direction) of the crystal grains were measured.
- Notations shown in the column of “Size” of the ⁇ 211 ⁇ 10-degree-oriented grains in Table 2 mean respective sizes in the “rolling direction/sheet width direction”. For some comparatives, measurement results at a thickness center (t/2) were also shown for reference. A site having a difference in a crystal orientation of 15 degrees or more was defined as a grain boundary.
- Hydrogen embrittlement resistance A relative tensile strength of 0.98 or more and relative elongation of 0.85 or more
- B relative tensile strength of 0.98 or more and relative elongation of 0.75 or more
- X one or both of relative tensile strength of less than 0.98 and relative elongation of less than 0.75
- Low-temperature embrittlement resistance A energy transition temperature of ⁇ 40 degrees C. or less
- B energy transition temperature of ⁇ 10 degrees or less
- X energy transition temperature of more than ⁇ 10 degrees C.
- the obtained Cr-based stainless steel sheet was subjected to an evaluation for hydrogen embrittlement and low-temperature embrittlement.
- an SUS316L steel sheet (17.5%Cr-12%Ni-2%Mo) and an SUS316 steel sheet (17.5%Cr-10%Ni-2%Mo), each of which had a thickness of 2 mm and was commercially available, were used to evaluate the hydrogen embrittlement resistance.
- the hydrogen embrittlement was evaluated according to the following steps.
- a tensile test piece (width: 4 mm, length: 20mm) was prepared from a parallel portion. A surface thereof was polished with a dry #600 Emery paper and was subsequently degreased with an organic solvent immediately prior to a tensile test in a high pressure hydrogen gas. As shown in Table 1, the tensile test in the high pressure hydrogen gas was performed at a hydrogen gaseous pressure of 20 MPa or 45 MPa, a test temperature of ⁇ 40 degrees C. and a strain rate of 10 ⁇ 5 1s. A comparative tensile test was performed in nitrogen ( ⁇ 40 degrees C. and 0.1 MPa).
- a tensile strength in the high pressure hydrogen gas divided by a tensile strength in nitrogen (0.1 MPa) was defined as a relative tensile strength.
- a fracture elongation in the high pressure hydrogen gas divided by a fracture elongation in nitrogen (0.1 MPa) was defined as a relative elongation.
- the hydrogen embrittlement resistance was evaluated using the relative tensile strength and the relative elongation as evaluation indices. Evaluation criteria were as follows. A and B were evaluated to pass.
- the SUS316L steel sheet had the relative elongation of less than 0.75 and thus was evaluated as X.
- the hydrogen gaseous pressure was 20 MPa and the test temperature was -40 degrees C.
- the SUS316 steel sheet had the relative elongation of less than 0.75 and thus was evaluated as X.
- the low-temperature embrittlement was evaluated by a Charpy impact test according to JIS Z 2242.
- a test piece was set to have a V-notch shape (1.5 to 2.5 mm thickness ⁇ 10 mm width ⁇ 55 mm length).
- a test temperature was set to be in a range from ⁇ 100 degrees C. to a room temperature (20 degrees C.).
- An energy transition temperature was calculated based on an absorption energy measured in the Charpy test and set to be an evaluation index of low-temperature embrittlement resistance. Evaluation criteria were as follows. A and B were evaluated to pass.
- the energy transition temperature was more than ⁇ 10 degrees C.
- Nos. 1 to 11 were each a Cr-based stainless steel sheet having chemical composition and a texture that were within respective ranges of the invention, thereby showing favorable hydrogen embrittlement resistance and low-temperature embrittlement resistance.
- Nos. 5, 6, 9 and 10 which were within preferable ranges of the components and the texture, were evaluated as “B” or “A” for the index of the hydrogen embrittlement resistance at a hydrogen gaseous pressure of 45 MPa.
- the hydrogen embrittlement resistance thereof was superior to that of SUS316L.
- Nos. 6, 8 and 10 the ⁇ 211 ⁇ 10-degree-oriented grains were reduced using a large-diameter roll. Although having the same chemical composition, the hydrogen embrittlement resistance thereof further improved as compared with that of Nos. 5, 7 and 9.
- Nos. 12 to 20 were each a Cr-based stainless steel sheet that did not have chemical composition within the respective ranges of the invention and thus unable to form a texture within the range of the invention, so that one or both of the hydrogen embrittlement resistance and low-temperature embrittlement resistance thereof were deteriorated.
- the area ratio of the ⁇ 211 ⁇ 10-degree-oriented grains at a thickness center was less than 30% but the area ratio thereof in the sheet surface was more than 30%. Accordingly, it has been found that controlling of the area ratio in the sheet surface is important in order to obtain both the hydrogen embrittlement resistance and the low-temperature embrittlement resistance.
- each of the Cr-based stainless steel sheets exhibited superior hydrogen embrittlement resistance to that of the commonly available SUS316. It also has been found that each of the Cr-based stainless steel sheets is controlled using the large-diameter roll to have a preferable texture with preferable components, thereby achieving the hydrogen embrittlement resistance superior to that of SUS316L.
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PCT/JP2019/049717 WO2020130060A1 (ja) | 2018-12-21 | 2019-12-18 | 耐水素脆性に優れたCr系ステンレス鋼板 |
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Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2008208412A (ja) * | 2007-02-26 | 2008-09-11 | Nippon Steel & Sumikin Stainless Steel Corp | 加工肌荒れの小さい成形性に優れたフェライト系ステンレス鋼板およびその製造方法 |
US20130011294A1 (en) * | 2010-03-08 | 2013-01-10 | Matsuhashi Tooru | Ferritic stainless steel excellent in corrosion resistance in environment of condensed water from hydrocarbon combustion gas |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH04371550A (ja) * | 1991-06-18 | 1992-12-24 | Nisshin Steel Co Ltd | 封着用合金部材 |
EP1225242B1 (en) * | 2001-01-18 | 2004-04-07 | JFE Steel Corporation | Ferritic stainless steel sheet with excellent workability and method for making the same |
JP3788311B2 (ja) * | 2001-10-31 | 2006-06-21 | Jfeスチール株式会社 | フェライト系ステンレス鋼板及びその製造方法 |
JP3886864B2 (ja) * | 2002-08-26 | 2007-02-28 | 日新製鋼株式会社 | 二次加工性に優れるフェライト系ステンレス鋼冷延焼鈍材及びその製造方法 |
JP4167587B2 (ja) * | 2003-02-28 | 2008-10-15 | 新日本製鐵株式会社 | 耐水素脆化に優れた高強度薄鋼板及びその製造方法 |
JP4700263B2 (ja) | 2003-04-25 | 2011-06-15 | 新日本製鐵株式会社 | 高圧水素ガス用タンク及び配管 |
JP3886933B2 (ja) * | 2003-06-04 | 2007-02-28 | 日新製鋼株式会社 | プレス成形性,二次加工性に優れたフェライト系ステンレス鋼板及びその製造方法 |
JP5088021B2 (ja) | 2007-07-05 | 2012-12-05 | 新日本製鐵株式会社 | 高剛性高強度冷延鋼板及びその製造方法 |
US9175361B2 (en) | 2010-09-29 | 2015-11-03 | Nippon Steel & Sumikin Stainless Steel Corporation | Austenitic high Mn stainless steel and method production of same and member using that steel |
JP5842537B2 (ja) | 2010-10-28 | 2016-01-13 | Jfeスチール株式会社 | 高圧水素貯蔵容器用高強度鋼材 |
JP5869922B2 (ja) | 2012-03-09 | 2016-02-24 | 新日鐵住金ステンレス株式会社 | 面内異方性が小さいフェライト・オーステナイト2相ステンレス鋼板およびその製造方法 |
JP5793459B2 (ja) * | 2012-03-30 | 2015-10-14 | 新日鐵住金ステンレス株式会社 | 加工性に優れた耐熱フェライト系ステンレス冷延鋼板、冷延素材用フェライト系ステンレス熱延鋼板及びそれらの製造方法 |
JP6089657B2 (ja) | 2012-12-07 | 2017-03-08 | 愛知製鋼株式会社 | 低温での水素脆化感受性に優れた高圧水素用オーステナイト系ステンレス鋼及びその製造方法 |
JP5843982B2 (ja) * | 2013-02-04 | 2016-01-13 | 新日鐵住金ステンレス株式会社 | 加工性に優れたフェライト系ステンレス鋼板およびその製造方法 |
JPWO2015098981A1 (ja) | 2013-12-27 | 2017-03-23 | 国立大学法人九州大学 | 水素機器用の基材及びその製造方法 |
JP5908936B2 (ja) * | 2014-03-26 | 2016-04-26 | 新日鐵住金ステンレス株式会社 | フランジ用フェライト系ステンレス鋼板とその製造方法およびフランジ部品 |
EP3133179B8 (en) | 2014-04-17 | 2019-09-11 | Nippon Steel Corporation | Austenitic stainless steel and method for producing same |
MX2017005210A (es) * | 2014-10-31 | 2017-07-26 | Nippon Steel & Sumikin Sst | Chapa de acero inoxidable con base en ferrita, tubo de acero, y metodo de produccion de estos. |
JP6684620B2 (ja) | 2015-03-26 | 2020-04-22 | 日鉄ステンレス株式会社 | 耐水素脆化特性に優れた高強度オーステナイト系ステンレス鋼およびその製造方法、ならびに高圧水素ガスおよび液体水素環境中で用いる水素用機器 |
EP3480334B1 (en) * | 2016-07-04 | 2021-10-20 | NIPPON STEEL Stainless Steel Corporation | Ferritic stainless steel, steel sheet thereof, and methods for producing these |
JP6820757B2 (ja) | 2017-01-27 | 2021-01-27 | 日鉄ステンレス株式会社 | 耐熱性に優れた耐熱部材締結部品用フェライト系ステンレス鋼板および締結部品並びに耐熱管状部材用円状クランプ |
-
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Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2008208412A (ja) * | 2007-02-26 | 2008-09-11 | Nippon Steel & Sumikin Stainless Steel Corp | 加工肌荒れの小さい成形性に優れたフェライト系ステンレス鋼板およびその製造方法 |
US20130011294A1 (en) * | 2010-03-08 | 2013-01-10 | Matsuhashi Tooru | Ferritic stainless steel excellent in corrosion resistance in environment of condensed water from hydrocarbon combustion gas |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114107630A (zh) * | 2021-11-19 | 2022-03-01 | 北京科技大学 | 提高马氏体不锈钢抗氢脆性的热处理方法、不锈钢及应用 |
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CN113227414B (zh) | 2023-08-11 |
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KR102539588B1 (ko) | 2023-06-01 |
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