WO2017150665A1 - 低温用h形鋼及びその製造方法 - Google Patents
低温用h形鋼及びその製造方法 Download PDFInfo
- Publication number
- WO2017150665A1 WO2017150665A1 PCT/JP2017/008275 JP2017008275W WO2017150665A1 WO 2017150665 A1 WO2017150665 A1 WO 2017150665A1 JP 2017008275 W JP2017008275 W JP 2017008275W WO 2017150665 A1 WO2017150665 A1 WO 2017150665A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- temperature
- less
- steel
- flange
- low
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Ceased
Links
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/0068—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for particular articles not mentioned below
-
- 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
- C21D1/56—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering characterised by the quenching agents
- C21D1/60—Aqueous agents
-
- 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
- C21D6/005—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
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/008—Heat treatment of ferrous alloys containing Si
-
- 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
-
- 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
-
- 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
-
- 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
-
- 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
-
- 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
-
- 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
-
- 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
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
-
- 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
-
- 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
- C22C38/08—Ferrous alloys, e.g. steel alloys containing nickel
-
- 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
- C22C38/12—Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
-
- 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
- C22C38/14—Ferrous alloys, e.g. steel alloys containing titanium or zirconium
-
- 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
- C22C38/16—Ferrous alloys, e.g. steel alloys containing copper
-
- 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
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/44—Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/46—Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
-
- C—CHEMISTRY; METALLURGY
- 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
-
- 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
-
- 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
-
- 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
- C21D2211/002—Bainite
-
- 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
- C21D2211/005—Ferrite
Definitions
- the present invention relates to a low-temperature H-section steel used for a structural member of a building used in a low-temperature environment and a method for manufacturing the same.
- Patent Documents 1 to 3 In response to such a demand, for example, in Patent Documents 1 to 3, by using an oxide that becomes a nucleation site of ferrite, and by performing accelerated cooling after hot rolling in order to suppress ferrite grain growth, A method for increasing the toughness of H-section steel by refining the metal structure has been proposed. According to Patent Documents 1 to 3, an H-section steel excellent in Charpy absorbed energy at ⁇ 5 ° C. or ⁇ 10 ° C. can be obtained. However, in recent years, the low-temperature toughness (for example, toughness at ⁇ 40 ° C.) required for H-section steel used in cold regions has not been sufficient.
- the low-temperature toughness for example, toughness at ⁇ 40 ° C.
- Patent Document 4 proposes an H-section steel having excellent low-temperature toughness with Charpy absorbed energy at ⁇ 40 ° C. of 27 J or more.
- Nb, V, etc. are not added, the C content and the amount of nitrogen dissolved in the steel (solid N amount) are reduced, and accelerated cooling is applied to reduce the low temperature toughness of the H-section steel. Has improved.
- the toughness of the base material is evaluated, the low temperature toughness of the weld heat affected zone is not considered.
- N is fixed by Ti, TiN is generated, and the amount of dissolved N is reduced. However, when heated to 1400 ° C. or higher by welding, TiN will dissolve in the steel.
- Japanese Unexamined Patent Publication No. 5-263182 Japanese Patent Laid-Open No. 5-271754 Japanese Unexamined Patent Publication No. 7-216498 Japanese Unexamined Patent Publication No. 2006-249475
- the present invention is a low-temperature H-section steel that has improved the low-temperature toughness of not only the base material but also the weld heat-affected zone, while ensuring the strength required for the structural member, and a method for producing the same.
- the issue is to provide
- Nb is an element that generates precipitates such as carbides and nitrides, and is generally an element that adversely affects toughness, as its content is limited in Patent Document 4.
- Nb is an element that contributes to the refinement of crystal grains by suppressing recrystallization, and is also an element useful for increasing the strength. Therefore, the present inventors tried to ensure the strength and toughness of the H-section steel by containing Nb and applying accelerated cooling.
- TiO X a general term for TiO, TiO 2 , and Ti 2 O 3 , sometimes referred to as TiO X
- TiO X a nucleation site of intragranular ferrite
- the present invention has been made on the basis of the above findings, and the gist thereof is as follows.
- the low-temperature H-section steel according to one embodiment of the present invention is, by mass, C: 0.03-0.13%, Mn: 0.80-2.00%, Nb: 0.005-0 0.060%, Ti: 0.005-0.025%, O: 0.0005-0.0100%, V: 0-0.08%, Cu: 0-0.40%, Ni: 0-0.
- CEV calculated by the following formula (a) is 0.40 or less , Ferrite and bainnai at 1/4 position from outside of flange thickness and 1/6 position from outside flange width The total area ratio of one or both of them is 90% or more, the area ratio of the hard phase is 10% or less, the effective crystal grain size is 20.0 ⁇ m or less, and the particle diameter of the hard phase is 10.0 ⁇ m or less.
- CEV C + Mn / 6 + (Cr + Mo + V) / 5 + (Ni + Cu) / 15 (a)
- C, Mn, Cr, Mo, V, Ni, and Cu are contents in mass% of each element.
- the low-temperature H-section steel described in (1) above is in mass%, V: 0.01 to 0.08%, Cu: 0.01 to 0.40%, Ni: 0.01 to 0
- One or more selected from the group consisting of .70%, Mo: 0.01 to 0.10%, and Cr: 0.01 to 0.20% may be contained.
- a method for producing a low-temperature H-section steel according to another aspect of the present invention is the method for producing a low-temperature H-section steel according to (1) or (2) above, wherein (1) or (2 ) A melting step for melting steel having the same chemical composition as the low-temperature H-section steel, a casting step for casting the steel obtained in the melting step to obtain a billet, and the billet Is heated to 1100 to 1350 ° C., and then hot-rolled to obtain a H-shaped steel by hot rolling so that the finishing temperature is (Ar 3 -30) ° C. or higher and 900 ° C.
- an accelerated cooling step in which water is cooled on the inner and outer surfaces of the flange so that the cooling rate exceeds 15 ° C./second.
- the oxygen concentration of the molten steel immediately before adding Ti is reduced to 0.
- the Ti is added, and in the accelerated cooling step, the H-section steel is added.
- the water cooling is performed so that the cooling stop temperature at 1/6 from the outside of the flange width is 300 ° C. or less at the surface temperature, and the maximum temperature after reheating the surface temperature is 350 to 700 ° C. I do.
- the toughness of the base material and the weld heat-affected zone at a low temperature of ⁇ 40 ° C. or ⁇ 60 ° C. is excellent and more stringent while ensuring the strength without containing a large amount of expensive elements. It becomes possible to obtain an H-section steel (low-temperature H-section steel) having a critical CTOD value of 0.40 mm or more at ⁇ 20 ° C. as a toughness evaluation. Therefore, according to the above aspect of the present invention, the industrial contribution is extremely significant, such as improving the reliability of buildings and the like built in cold regions without impairing the economy.
- FIG. 4 is a diagram for explaining the relationship between the number density of 0.01 to 3.0 ⁇ m Ti oxide and the limit CTOD value of HAZ at ⁇ 20 ° C.
- FIG. 4 is a diagram for explaining the relationship between recuperation temperature and the Charpy absorbed energy of the base material of H-section steel at -60 ° C.
- the low-temperature H-section steel according to one embodiment of the present invention (hereinafter sometimes referred to as H-section steel according to the present embodiment) has a predetermined chemical component and is located at a position 1/4 from the outside of the flange plate thickness.
- the total area ratio of one or both of ferrite and bainite at a position 1/6 from the outside of the flange width is 90% or more, the area ratio of the hard phase is 10% or less, and the effective crystal grain size is 20.0 ⁇ m.
- the hard phase has a particle size of 10.0 ⁇ m or less, a circle equivalent diameter of 0.01 to 3.0 ⁇ m of Ti oxide of 30 pieces / mm 2 or more, and a flange plate thickness of 12 to 50 mm. It is.
- the low-temperature H-section steel according to the present embodiment will be described.
- % related to chemical components means “% by mass” unless otherwise specified.
- C is an element effective for strengthening steel.
- the C content is set to 0.03% or more.
- the C content is preferably 0.04% or more, more preferably 0.05% or more.
- the C content is 0.13% or less.
- the C content is 0.10% or less, more preferably less than 0.08%.
- Mn is an element effective for improving the strength of steel and reducing the effective crystal grain size.
- the Mn content is set to 0.80% or more.
- the Mn content is preferably 1.00% or more, more preferably 1.20% or more, and still more preferably 1.30% or more.
- the Mn content is 2.00% or less. Preferably, it is 1.80% or less.
- Nb is an element that refines ferrite and improves the strength and toughness of steel.
- the C content and the Si content are limited in order to ensure the low temperature toughness of the base material and the weld heat affected zone. It is valid.
- the Nb content is set to 0.005% or more. Preferably it is 0.010% or more.
- the Nb content exceeds 0.060%, an increase in the hard phase and / or an increase in hardness is caused with an increase in hardenability, and the toughness is lowered. Therefore, the Nb content is set to 0.060% or less. More preferably, it is 0.050% or less.
- Ti is an element necessary for forming a Ti oxide serving as a ferrite nucleus.
- the Ti content is set to 0.005% or more. Preferably it is 0.010% or more.
- the Ti content is limited to 0.025% or less. Preferably it is 0.020% or less.
- O is an element that forms a Ti oxide.
- the O content is set to 0.0005% or more.
- it is 0.0010% or more, More preferably, it is 0.0015% or more, More preferably, it is 0.0020% or more.
- the O content is limited to 0.0100% or less.
- it is 0.0070% or less, More preferably, it is 0.0050% or less.
- Si is a deoxidizing element and is an element that contributes to the improvement of strength.
- Si like C, is an element that generates a hard phase. If the Si content exceeds 0.50%, the toughness of the base material and the weld heat affected zone decreases due to the generation of the hard phase, so the Si content is limited to 0.50% or less.
- the Si content is preferably 0.30% or less, more preferably 0.20% or less, and still more preferably 0.10% or less.
- the lower limit of the Si content is not specified and may be 0%. However, since Si is a useful deoxidizing element, it may be 0.01% or more in order to obtain this effect.
- Al is a deoxidizing element having a higher oxide generating ability than Ti, and is an element whose content should be limited when Ti oxide is sufficiently generated. If the Al content exceeds 0.008%, the generation of Ti oxides that become ferrite nuclei is inhibited by the generation of Al oxides. Therefore, the Al content is limited to 0.008% or less.
- the Al content is preferably 0.005% or less, and more preferably 0.002% or less.
- the lower limit of the Al content is not specified and may be 0%.
- REM 0.0010% or less
- Ca 0.0010% or less
- Mg 0.0010% or less
- REM rare earth element
- Ca, and Mg are elements having higher oxide generation ability than Ti, as in Al, they are elements whose contents should be limited. If the content of REM, Ca, and Mg exceeds 0.0010%, the production of Ti oxides that are ferrite nuclei is greatly inhibited, so the content of REM, Ca, and Mg is 0.0010% or less, respectively. Limit to.
- the content of REM, Ca and Mg is preferably 0.0005% or less.
- the lower limits of the REM content, Ca content, and Mg content are not defined, and may be 0%.
- N is an element that lowers the toughness of the base material and the weld heat affected zone. If the N content exceeds 0.0120%, the decrease in low temperature toughness becomes significant due to the increase in solid solution N and the formation of coarse precipitates. Therefore, the N content is limited to 0.0120% or less.
- the N content is preferably 0.0100% or less, more preferably 0.0070% or less.
- the N content may be 0%, but if the N content is reduced to less than 0.0020%, the steelmaking cost increases, so the N content may be 0.0020% or more. From the viewpoint of cost, the N content may be 0.0030% or more.
- the low-temperature H-section steel according to the present embodiment basically includes the above elements, with the balance being Fe and impurities. However, instead of a part of Fe, one or more selected from the group consisting of V, Cu, Ni, Mo, and Cr may be further included for the purpose of improving strength and toughness. However, since these elements are optional elements that are not necessarily contained, the lower limit is 0%. Moreover, even if these arbitrary elements are contained in less than the range described later, the characteristics of the low-temperature H-section steel according to the present embodiment are not hindered, and thus are allowed. Impurities are components that are mixed from raw materials such as ore or scrap or from various environments in the manufacturing process when industrially producing steel materials, and are allowed within a range that does not adversely affect the steel. Means what will be done.
- V is an element that forms nitride (VN) and increases the strength of the steel.
- the V content is preferably 0.01% or more. More preferably, it is 0.02% or more, More preferably, it is 0.03% or more.
- the upper limit of the V content is preferably 0.08%.
- Cu is an element that contributes to improvement in strength.
- the Cu content is preferably 0.01% or more. More preferably, it is 0.10%.
- the Cu content exceeds 0.40%, the strength increases excessively and the low temperature toughness decreases. Therefore, even when it contains, Cu content shall be 0.40% or less.
- the Cu content is preferably 0.30% or less, more preferably 0.20% or less.
- Ni is an extremely effective element for increasing strength and toughness.
- the Ni content is preferably 0.01% or more. More preferably, it is 0.10% or more, More preferably, it is 0.20% or more.
- Ni is an expensive element, and in order to suppress an increase in alloy cost, even when Ni is included, the Ni content is preferably set to 0.70% or less. More preferably, it is 0.50% or less.
- Mo is an element that contributes to the improvement of strength.
- the Mo content is preferably 0.01% or more.
- the Mo content exceeds 0.10%, precipitation of Mo carbide (Mo 2 C) and generation of a hard phase are promoted, and the toughness of the weld heat affected zone may be deteriorated. Therefore, even when it contains, it is preferable to make Mo content into 0.10% or less.
- the Mo content is more preferably 0.05% or less.
- Cr 0.01-0.20% Cr is also an element contributing to the improvement of strength.
- the Cr content is preferably 0.01% or more.
- the Cr content exceeds 0.20%, carbides may be generated and toughness may be reduced. Therefore, even when it is made to contain, it is preferable to make Cr content 0.20% or less. More preferably, it is 0.10% or less.
- P and S The content of P and S inevitably contained as impurities is not particularly limited. However, since P and S cause weld cracking due to solidification segregation and a decrease in toughness, they should be reduced as much as possible.
- the P content is preferably limited to 0.020% or less, and more preferably limited to 0.002% or less. Further, the S content is preferably limited to 0.002% or less.
- the low-temperature H-section steel according to the present embodiment contains the basic element and the balance is made of Fe and impurities, and the case where the balance is made of Fe and impurities, and the balance is made of Fe and impurities. Either is acceptable.
- the CEV calculated from the content of each element needs to be 0.40 or less.
- CEV is an index of hardenability and is preferably increased in order to ensure a predetermined strength. However, when CEV exceeds 0.40, the toughness of the welded portion decreases. Therefore, CEV is set to 0.40 or less.
- CEV is preferably set to 0.20 or more.
- CEV can be obtained by the following formula (1).
- C, Mn, Cr, Mo, V, Ni, and Cu are contents in mass% of each element. When not contained, CEV is obtained by setting these contents as 0.
- the characteristics of the flange are important. Therefore, in the low-temperature H-section steel according to this embodiment, the structure and characteristics of the flange are evaluated.
- the temperature tends to decrease during hot rolling at the end of the flange due to its shape, and it is difficult for the temperature to decrease at the center, so the temperature history changes depending on the position.
- the observation of the metal structure of the H-section steel and the measurement of the mechanical properties are, as shown in FIG. 4, a flange whose temperature tends to decrease during hot rolling.
- the total area ratio of one or both of ferrite and bainite is 90% or more.
- the upper limit is not particularly limited and may be 100%. Moreover, it is not necessary to limit the area ratio of each of ferrite and bainite.
- the area ratio of the hard phase composed of one or both of MA and pseudo pearlite which lowers the low temperature toughness is limited to 10% or less.
- the lower limit of the area ratio of the hard phase is not particularly limited, and may be 0%.
- pseudo-pearlite is a phase in which lamellar cementite is divided or the longitudinal direction of plate-like cementite is not aligned in the grain as compared with pearlite. Since pseudo pearlite is harder than pearlite, it lowers the low temperature toughness.
- the H-shaped steel for low temperature according to this embodiment may contain pearlite as the remainder other than ferrite, bainite, and hard phase.
- the effective crystal grain size correlates with the toughness of the metal structure in which ferrite, bainite, pseudo pearlite, MA, pearlite and the like are mixed.
- the effective crystal grain size is set to 20.0 ⁇ m or less in order to ensure toughness.
- the effective crystal grain size is a circle-equivalent diameter in a region surrounded by a large-angle grain boundary having an orientation difference of 15 ° or more.
- the hard phase that becomes the starting point of fracture needs to be finer than the effective crystal grain size, and the grain size of the hard phase is 10.0 ⁇ m or less. When the particle size of the hard phase exceeds 10.0 ⁇ m, toughness decreases.
- Evaluation of the metal structure of the low-temperature H-section steel according to the present embodiment is performed by taking a sample from the position of (1/4) t f and (1/6) F shown in FIG. Collected and performed by optical microscope and electron beam backscatter diffraction (EBSD). Specifically, an area within a rectangle of 500 ⁇ m (flange longitudinal direction) ⁇ 400 ⁇ m (flange thickness direction) is observed with an optical microscope, and the total area ratio of one or both of ferrite and bainite and the area ratio of the hard phase are determined. taking measurement. At this time, the particle size of the hard phase is also measured. The hard phase is discriminated from ferrite, bainite, and pearlite by an optical microscope, and the particle size is measured.
- EBSD electron beam backscatter diffraction
- the effective crystal grain size is determined by EBSD as the equivalent circle diameter of a region surrounded by a large-angle grain boundary having an orientation difference of 15 ° or more as an effective crystal grain.
- the effective crystal grain size is measured by EBSD without discriminating ferrite, bainite, hard phase (pseudo pearlite, MA), and remainder (pearlite).
- Ti oxide with equivalent circle diameter of 0.01 to 3.0 ⁇ m 30 pieces / mm 2 or more
- Ti oxide having an equivalent circle diameter of 0.01 to 3.0 ⁇ m serves as a nucleation site for intragranular ferrite.
- the Ti oxide having an equivalent circle diameter of 0.01 to 3.0 ⁇ m refines coarse austenite near the FL by the formation of intragranular ferrite and suppresses the formation of grain boundary ferrite and coarse bainite.
- the Charpy absorbed energy at ⁇ 40 ° C. and ⁇ 60 ° C. of HAZ is 60 J or more. Further, as shown in FIG.
- the limit CTOD value of HAZ at ⁇ 20 ° C. becomes 0.40 mm or more.
- the number of Ti oxides having an equivalent circle diameter of 0.01 to 3.0 ⁇ m is set to 30 pieces / mm 2 or more.
- the number density of the Ti oxide having an equivalent circle diameter of 0.01 to 3.0 ⁇ m is preferably 100 pieces / mm 2 or less.
- the equivalent circle diameter and number density of Ti oxides present in the steel are 4 mm 2 or more in total by using a transmission electron microscope (TEM) to obtain an extraction replica by taking a sample from the same site as the metal structure evaluation. Observe the area and measure using the photograph taken.
- the Ti oxide is not only TiO, TiO 2 , Ti 2 O 3 , a composite oxide of these and an oxide not containing Ti, and further, a Ti oxide or a composite oxide and a sulfide. And complex inclusions.
- the equivalent circle diameter of the Ti oxide contributing to the intragranular transformation is 0.01 to 3.0 ⁇ m, and it is not necessary to measure the number of Ti oxides having an equivalent circle diameter of less than 0.01 ⁇ m and more than 3.0 ⁇ m. Whether or not the observed inclusion is Ti oxide can be determined from the shape or the like, but it may be confirmed that the inclusion is Ti oxide using EDS, EPMA, or the like.
- the plate thickness of the low-temperature H-section steel flange according to this embodiment is 12 to 50 mm. This is because H-section steel having a plate thickness of 12 to 50 mm is frequently used for H-section steel used in low-temperature structures.
- the thickness of the flange of the H-section steel used for the structure for low temperature is preferably 16 mm or more. On the other hand, if the plate thickness of the flange exceeds 50 mm, the amount of reduction is insufficient and the structure becomes coarse, which may cause brittle fracture.
- the plate thickness of the flange is preferably 40 mm or less.
- the thickness of the web is generally 8 to 40 mm because it is generally thinner than the thickness of the flange.
- the thickness ratio of the flange / web is preferably set to 0.5 to 2.5 assuming that the H-shaped steel is manufactured by hot rolling. When the flange / web thickness ratio exceeds 2.5, the web may be deformed into a wavy shape. On the other hand, when the flange / web plate thickness ratio is less than 0.5, the flange may be deformed into a wavy shape.
- the yield point (YP) at normal temperature or the 0.2% proof stress is 335 MPa or more, and the tensile strength (TS) is 460 MPa or more.
- the yield ratio (YR) is preferably 0.80 or more.
- the target value of Charpy absorbed energy at ⁇ 40 ° C. and ⁇ 60 ° C. of the base metal and the weld heat affected zone is 60 J or more.
- the Charpy absorbed energy at ⁇ 40 ° C. and ⁇ 60 ° C. of the base material is preferably 100 J or more.
- the toughness (Charpy absorbed energy) is preferably 300 J or more.
- the target value of the critical CTOD value (crack tip opening amount) at ⁇ 20 ° C. of the base metal and the weld heat affected zone is 0.40 mm or more, and it is more preferable that brittle fracture such as pop-in does not occur.
- the toughness of the weld heat-affected zone is evaluated based on the melt line (FL), which is heated to the highest temperature and becomes coarse, as a notch position.
- the manufacturing method of the H-shaped steel for low temperature which concerns on this embodiment is demonstrated.
- the H-shaped steel for low temperature according to the present embodiment is heated against a steel piece obtained by casting a molten steel having a predetermined chemical composition by continuous casting or the like, as shown in FIG. Heating is performed in a furnace, hot rolling including rough rolling, intermediate rolling, and finish rolling is performed in a rough rolling mill, an intermediate rolling mill, and a finish rolling mill, and accelerated cooling is performed using a full-section water cooling apparatus.
- hot rolling rough rolling may be performed as necessary and may be omitted.
- each step will be described.
- ⁇ Melting process> (Oxygen content in molten steel immediately before Ti addition: 0.0015 to 0.0110%)
- molten steel molten steel
- it casts and obtains a steel piece.
- the amount of oxygen in the molten steel is set to 0.0015% or more in order to ensure a sufficient amount for forming the Ti oxide.
- it is 0.0025% or more.
- the amount of oxygen (oxygen concentration) in the molten steel is limited to 0.0110% or less. Preferably it is 0.0090% or less, More preferably, it is 0.0080% or less.
- casting is performed to obtain a steel piece.
- the casting is preferably continuous casting from the viewpoint of productivity.
- the thickness of the steel slab is preferably 200 mm or more from the viewpoint of productivity, and is preferably 350 mm or less in consideration of reduction of segregation, uniformity of heating temperature in hot rolling, and the like.
- Hot rolling consists of rough rolling performed using a rough rolling mill, intermediate rolling using an intermediate rolling mill, and finish rolling performed using a finish rolling mill.
- Rough rolling is a process performed as necessary before intermediate rolling, and is performed according to the thickness of the steel slab and the thickness of the product.
- the intermediate rolling may be performed by water cooling between passes using an intermediate universal rolling mill (intermediate rolling mill) and a water cooling device (not shown).
- Heating temperature of steel slab 1100 to 1350 ° C
- the heating temperature of the steel slab used for hot rolling is 1100 to 1350 ° C.
- the heating temperature is set to 1100 ° C. or higher in order to ensure the formability in hot rolling.
- the heating temperature of the steel slab is preferably set to 1150 ° C. or higher.
- the heating temperature of the steel slab is 1200 ° C. or higher.
- heating temperature of the steel slab exceeds 1350 ° C.
- the oxide on the surface of the steel slab, which is the raw material may melt and the inside of the heating furnace may be damaged. Therefore, heating temperature shall be 1350 degrees C or less.
- the heating temperature of the steel slab is 1300 ° C. or lower.
- controlled rolling is a rolling method performed by controlling the rolling temperature and the rolling reduction.
- the inter-pass water-cooled rolling process is a method of rolling by imparting a temperature difference between the surface layer portion and the inside of the flange by performing water cooling between rolling passes.
- the flange surface temperature is water-cooled to 700 ° C. or lower by water cooling between rolling passes, and then rolled in a reheating process.
- the finishing temperature of hot rolling is (Ar 3 -30) ° C. or higher and 900 ° C. or lower.
- the finishing temperature exceeds 900 ° C., coarse austenite remains after rolling.
- this coarse austenite is transformed into coarse bainite by cooling, it becomes a starting point of brittle fracture and the toughness is lowered.
- the finishing temperature is 850 ° C. or lower.
- Finishing temperature of hot rolling by considering the shape accuracy of the H-shaped steel, and a starting temperature of ferrite transformation (Ar 3 -30) °C or higher.
- Ar 3 can be obtained by the following formula (2). Following formula (2) Oite, C, Si, Mn, Ni , Cu, Cr, Mo is the content by mass percent of the respective elements, if not contained, the Ar 3 these content 0 Ask.
- Ar 3 868-396 ⁇ C + 24.6 ⁇ Si-68.1 ⁇ Mn-36.1 ⁇ Ni-20.7 ⁇ Cu-24.8 ⁇ Cr + 29.6 ⁇ Mo (2)
- the steel slab is heated to 1100 to 1350 ° C. to be hot rolled (primary rolling), cooled to 500 ° C. or lower, and then heated to 1100 to 1350 ° C. again to perform hot rolling (secondary rolling).
- accelerated cooling is performed on the inner surface and outer surface of the flange by a water cooling device (full-section water cooling device) provided on the exit side of the finishing mill.
- a water cooling device full-section water cooling device
- the start temperature of accelerated cooling is almost the same as the finishing temperature of hot rolling, or even if it is slightly lowered, it has little effect on the characteristics .
- the cooling rate of the inner and outer surfaces of the flange becomes uniform, and the material and shape accuracy can be improved.
- the upper surface side of the web is cooled by the cooling water sprayed on the inner surface of the flange. In order to suppress the warpage of the web, cooling may be performed from the lower surface side of the web.
- the accelerated cooling is performed by spray cooling (cooling by the cooling water 5 from the spray nozzle 4) on the outer surface and the inner surface of the flange 2 of the H-section steel 1 by using, for example, a water cooling device shown in FIG.
- the cooling rate of the accelerated cooling is to increase the toughness by suppressing the coarsening of the effective crystal grain size and the generation of a hard phase composed of one or both of pseudo pearlite and MA, and increase the strength by the effect of quenching. More than ° C / second. Low temperature toughness can be ensured even when 0.005% or more of Nb is contained by applying accelerated cooling with a cooling rate exceeding 15 ° C./second to refine the structure.
- the cooling rate of accelerated cooling is preferably 18 ° C./second or more, more preferably 20 ° C./second or more.
- the upper limit of the cooling rate of accelerated cooling is not limited, considering shape accuracy, 50 ° C./second or less is preferable. In this embodiment, as shown in FIG.
- the cooling rate of accelerated cooling is the difference in temperature ( ⁇ T) between the surface temperature at the start of accelerated cooling and the surface temperature after recuperation by the water cooling time ( ⁇ t 1 ). Divide and calculate. The time from completion of water cooling to completion of recuperation ( ⁇ t 2 ) is not considered.
- accelerated cooling is performed so that the maximum temperature that the surface temperature reaches after such recuperation is controlled within a certain range. Specifically, accelerated cooling is performed so that the highest surface temperature at a position 1/6 from the outside of the flange width after reheating is 350 to 700 ° C.
- the toughness decreases due to the coarsening of the effective crystal grain size and the increase in the hard phase (mainly pseudo pearlite).
- the low temperature toughness of the H-section steel (base material) is improved when the recuperated temperature after accelerated cooling is between 350 and 700 ° C., which is the target of 60 J or more.
- heat treatment may be performed to adjust strength and toughness.
- This heat treatment may be performed at a temperature (Ac 1 ) or less at which transformation to austenite starts, but is preferably performed in the range of 100 to 700 ° C. More preferably, the lower limit is 300 ° C. and the upper limit is 650 ° C. More preferably, the lower limit is 400 ° C. and the upper limit is 600 ° C.
- a sample is taken from the position where the test piece used for measuring these mechanical properties is taken, and the metal structure is observed with an optical microscope in an area within a rectangle of 500 ⁇ m (longitudinal direction) ⁇ 400 ⁇ m (flange thickness direction).
- the total area ratio of one or both of ferrite and bainite, the area ratio of the hard phase, and the particle size were measured. It was also confirmed by observation of the metal structure that the balance was pearlite.
- Effective crystal grain size was measured by EBSD.
- the number of Ti oxides with an equivalent circle diameter of 0.01 to 3.0 ⁇ m was measured by using a TEM for an area of 4 mm 2 or more by taking a sample from the same part as the evaluation of the metal structure to produce an extracted replica. did.
- CTOD test piece was prepared, and the critical CTOD value (crack tip opening amount) at ⁇ 20 ° C. of the H-shaped steel (base material) was measured.
- the CTOD test piece was cut out from the entire thickness of the flange portion to produce a smooth test piece, and the extension on the original web surface was used as a notch position.
- the test method followed BS7448.
- the CTOD value and Charpy absorbed energy of the weld heat affected zone were measured by the following method.
- the specimen collection position was in accordance with EN10225. First, a flange portion of an H-shaped steel (base material) was cut out, a groove shape was applied, and submerged arc welding was performed at a welding heat input of 35 kJ / cm. And in the bond part of the vertical side of a groove
- Results are shown in Tables 5 and 6.
- the target value of each characteristic of the H-shaped steel is that the yield point (YP) at normal temperature or the 0.2% proof stress is 335 MPa or more, the tensile strength (TS) is 460 to 620 MPa, ⁇ 40 ° C. and ⁇ 60 ° C.
- Charpy absorbed energy All are 60 J or more, and the CTOD value at ⁇ 20 ° C. is 0.40 mm or more.
- the target values of the Charpy absorbed energy and the CTOD value of the welding heat affected zone are the same as those of the base material.
- No. Nos. 1 to 21 have a high 0.2% proof stress (YP) at room temperature and are within the range of the target value of tensile strength (TS), and the Charpy absorbed energy and the critical CTOD value are both in the base material and the weld heat affected zone. The goal is well met.
- No. No. 32 has a high acceleration cooling stop temperature. Since 33 has a slow cooling rate, the effective crystal grain size is increased, and the strength and toughness are reduced. No. 34 is an example where the finishing temperature is high, and the toughness is lowered. No. In No. 40, the recuperation temperature is low, the hard phase is increased, and the base material toughness is lowered.
- the H-section steel of the present invention is, for example, FPSO (Floating Production, Storage and Offloading System), that is, oil and gas is produced on the ocean, and the product is stored in a tank in the facility. It is suitable for facilities that store in the tank and directly load it onto the transport tanker.
- FPSO Floating Production, Storage and Offloading System
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Heat Treatment Of Steel (AREA)
Abstract
Description
特許文献1~3によれば、-5℃や-10℃でのシャルピー吸収エネルギーに優れたH形鋼が得られる。しかしながら、近年、寒冷地で使用されるH形鋼に求められる低温靭性(例えば-40℃での靱性)としては十分でなかった。
しかしながら、特許文献4では母材の靭性については評価されているものの、溶接熱影響部の低温靭性については考慮されていない。特許文献4では、TiによってNを固定し、TiNを生成させて固溶N量を低減させている。しかしながら、溶接によって1400℃以上に加熱されると、TiNは鋼中に固溶してしまう。その結果、熱影響部、特に溶融線(FL)近傍において粗大な組織が生成することが懸念される。すなわち、特許文献4のようにTiNを形成させて固溶N量を低減させた場合、母材の靭性向上には一定の効果を有するものの、溶接熱影響部(HAZ)では低温靭性が低下することが懸念される。
CEV=C+Mn/6+(Cr+Mo+V)/5+(Ni+Cu)/15 ・・・(a)
ここで、C、Mn、Cr、Mo、V、Ni、Cuは、各元素の質量%での含有量である。
(2)上記(1)に記載の低温用H形鋼は、質量%で、V:0.01~0.08%、Cu:0.01~0.40%、Ni:0.01~0.70%、Mo:0.01~0.10%、Cr:0.01~0.20%からなる群から選択される1種又は2種以上を含有してもよい。
(3)本発明の別の態様に係る低温用H形鋼の製造方法は、上記(1)又は(2)に記載の低温用H形鋼の製造方法であって、(1)又は(2)に記載の低温用H形鋼と同じ化学成分からなる鋼を溶製する溶製工程と、前記溶製工程で得られた前記鋼を鋳造して鋼片を得る鋳造工程と、前記鋼片を、1100~1350℃に加熱し、その後、仕上温度が(Ar3-30)℃以上900℃以下となるように熱間圧延を行ってH形鋼を得る熱間圧延工程と、前記H形鋼を、冷却速度が15℃/秒超となるようにフランジの内外面に水冷を行う加速冷却工程と、を有し、前記溶製工程では、Tiを添加する直前の溶鋼の酸素濃度を0.0015~0.0110質量%の範囲に調整した後に、前記Tiを添加し、前記加速冷却工程では、前記H形鋼のフランジ幅の外側から1/6の位置での冷却停止温度が表面温度で300℃以下になるように、かつ、前記表面温度の復熱後の最高温度が350~700℃になるように前記水冷を行う。
以下、本実施形態に係る低温用H形鋼について説明する。
Cは、鋼の強化に有効な元素である。この効果を得るため、C含有量を0.03%以上とする。C含有量は、0.04%以上であることが好ましく、より好ましくは0.05%以上である。一方、C含有量が0.13%を超えると硬質相である島状マルテンサイト(MA)や疑似パーライトが増加し、母材や溶接熱影響部の靱性が低下する。したがって、C含有量を0.13%以下とする。好ましくはC含有量を0.10%以下、より好ましくは0.08%未満とする。
Mnは、鋼の強度向上及び有効結晶粒径の微細化に有効な元素である。これらの効果を得るため、Mn含有量を0.80%以上とする。Mn含有量は、好ましくは1.00%以上、より好ましくは1.20%以上、更に好ましくは1.30%以上である。一方、Mn含有量が2.00%を超えると、介在物の増加等によって、母材及び溶接熱影響部の靱性が低下する。したがって、Mn含有量を2.00%以下とする。好ましくは、1.80%以下である。
Nbはフェライトを微細化させ、鋼の強度及び靭性を向上させる元素である。特に、本実施形態に係る低温用H形鋼では、母材、溶接熱影響部の低温靭性の確保のためにC含有量、Si含有量を制限しており、Nbの含有による強度の確保は有効である。これらの効果を得るため、Nb含有量を0.005%以上とする。好ましくは0.010%以上である。一方、Nb含有量が0.060%を超えると、焼入れ性の向上に伴って、硬質相の増加及び/又は硬さの上昇が引き起こされ、靭性が低下する。したがって、Nb含有量を0.060%以下とする。より好ましくは0.050%以下である。
Tiは、フェライトの生成核となるTi酸化物を形成するために必要な元素である。この効果を得るため、Ti含有量を0.005%以上とする。好ましくは0.010%以上である。一方、Ti含有量が0.025%を超えると粗大なTiNやTiCが増加し、これらが脆性破壊の起点となる。そのため、Ti含有量を0.025%以下に制限する。好ましくは0.020%以下である。
Oは、Ti酸化物を形成する元素である。Ti酸化物を十分に生成させるために、O含有量を0.0005%以上とする。好ましくは0.0010%以上、より好ましくは0.0015%以上、さらに好ましくは0.0020%以上である。一方、O含有量が過剰になると、粗大な酸化物の生成が生成して靭性が低下する。粗大な酸化物の生成を抑制して靭性を確保するため、O含有量を0.0100%以下に制限する。好ましくは0.0070%以下、より好ましくは0.0050%以下である。
Siは、脱酸元素であり、強度の向上にも寄与する元素である。しかしながら、Siは、Cと同様、硬質相を生成させる元素である。Si含有量が0.50%を超えると、硬質相の生成によって母材及び溶接熱影響部の靭性が低下するので、Si含有量を0.50%以下に制限する。Si含有量は、0.30%以下が好ましく、0.20%以下がより好ましく、0.10%以下が更に好ましい。Si含有量の下限は規定せず、0%でもよいが、Siは有用な脱酸元素であるので、この効果を得るために0.01%以上としてもよい。
Alは、Tiよりも酸化物生成能が高い脱酸元素であり、Ti酸化物を十分に生成させる場合、含有量を制限すべき元素である。Al含有量が0.008%を超えると、Al酸化物の生成によって、フェライトの生成核となるTi酸化物の生成が阻害される。そのため、Al含有量を0.008%以下に制限する。Al含有量は、0.005%以下が好ましく、0.002%以下がより好ましい。Al含有量の下限は規定せず、0%でもよい。
(Ca:0.0010%以下)
(Mg:0.0010%以下)
REM(希土類元素)、Ca及びMgは、Alと同様、何れもTiより酸化物生成能が高い元素であるので、含有量を制限すべき元素である。REM、Ca及びMgの含有量が0.0010%を超えると、フェライトの生成核となるTi酸化物の生成が大きく阻害されるので、REM、Ca、Mgの含有量をそれぞれ0.0010%以下に制限する。REM、Ca及びMgの含有量は、0.0005%以下が好ましい。REM含有量、Ca含有量及びMg含有量の下限は規定せず、0%でもよい。
Nは、母材及び溶接熱影響部の靭性を低下させる元素である。N含有量が0.0120%を超えると、固溶Nの増大や粗大な析出物の形成によって低温靭性の低下が著しくなる。そのため、N含有量を0.0120%以下に制限する。N含有量は好ましくは0.0100%以下、より好ましくは0.0070%以下とする。一方、N含有量は0%でもよいが、N含有量を0.0020%未満に低減しようとすると製鋼コストが高くなるので、N含有量を0.0020%以上としてもよい。コストの観点から、N含有量は0.0030%以上であってもよい。
Vは、窒化物(VN)を形成し、鋼の強度を高める元素である。この効果を得る場合、V含有量を0.01%以上とすることが好ましい。より好ましくは0.02%以上、さらに好ましくは0.03%以上である。一方、Vは高価な元素であるので、含有させる場合でも、V含有量の上限は0.08%が好ましい。
Cuは、強度の向上に寄与する元素である。この効果を得る場合、Cu含有量を0.01%以上とすることが好ましい。より好ましくは0.10%である。一方、Cu含有量が0.40%を超えると強度が過剰に上昇し、低温靭性が低下する。そのため、含有させる場合でも、Cu含有量を0.40%以下とする。Cu含有量は好ましくは0.30%以下、より好ましくは0.20%以下である。
Niは、強度及び靭性を高めるために、極めて有効な元素である。これらの効果を得る場合、Ni含有量を0.01%以上とすることが好ましい。より好ましくは0.10%以上、更に好ましくは0.20%以上である。一方、Niは高価な元素であり、合金コストの上昇を抑制するため、含有させる場合でもNi含有量を0.70%以下とすることが好ましい。より好ましくは0.50%以下である。
Moは、強度の向上に寄与する元素である。この効果を得る場合、Mo含有量を0.01%以上とすることが好ましい。一方、Mo含有量が0.10%を超えると、Mo炭化物(Mo2C)の析出や硬質相の生成が促進され、溶接熱影響部の靱性が劣化することがある。そのため、含有させる場合でも、Mo含有量を0.10%以下とすることが好ましい。Mo含有量は、0.05%以下がより好ましい。
Crも強度の向上に寄与する元素である。この効果を得る場合、Cr含有量を0.01%以上とすることが好ましい。一方、Cr含有量が0.20%を超えると炭化物が生成し、靭性が低下することがある。そのため、含有させる場合でも、Cr含有量を0.20%以下とすることが好ましい。より好ましくは0.10%以下である。
不可避的に不純物として含有されるP、Sについては、含有量を特に限定しない。ただし、P、Sは、凝固偏析による溶接割れ、靱性低下の原因となるので、極力低減すべきである。P含有量は0.020%以下に制限することが好ましく、0.002%以下に制限することがより好ましい。また、S含有量は、0.002%以下に制限することが好ましい。
本実施形態に係る低温用H形鋼は、上述の通り、基本元素を含有し残部がFe及び不純物からなる場合、及び、基本元素と任意元素とを含有し残部がFe及び不純物からなる場合のいずれも許容される。
さらに、本実施形態に係る低温用H形鋼では、各元素の含有量に加えて、各元素の含有量から計算されるCEVを0.40以下にする必要がある。
CEVは、焼入れ性の指標であり、所定の強度を確保するためには高めることが好ましい。しかしながら、CEVが0.40を超えると、溶接部の靱性が低下する。そのため、CEVを0.40以下とする。一方、CEVを低減させると焼入れ性が低下し、組織が粗大化するおそれがあるので、CEVを0.20以上とすることが好ましい。
CEVは、下記式(1)で求めることができる。下記式(1)において、C、Mn、Cr、Mo、V、Ni、Cuは、各元素の質量%での含有量であり、含有されない場合は、これらの含有量を0としてCEVを求める。
(硬質相の面積率:10%以下)
本実施形態に係る低温用H形鋼の金属組織は、フェライト及びベイナイトの一方又は両方の面積率の合計が90%以上である。上限は特に制限せず、100%でもよい。また、フェライト、ベイナイトのそれぞれの面積率を限定する必要はない。
一方、低温靭性を低下させるMA、疑似パーライトの一方又は両方からなる硬質相の面積率は10%以下に制限する。硬質相の面積率の下限は特に制限せず、0%でもよい。硬質相のうち、疑似パーライトは、パーライトに比べ、ラメラ状のセメンタイトが分断されているか、板状のセメンタイトの長手方向が粒内で揃っていない相である。疑似パーライトは、パーライトに比べて硬質であるため、低温靭性を低下させる。
本実施形態に係る低温用H形鋼は、フェライト、ベイナイト、硬質相以外の残部として、パーライトが含まれる場合がある。
(硬質相の粒径:10.0μm以下)
有効結晶粒径は、フェライト、ベイナイト、疑似パーライト、MA、パーライトなどが混在する金属組織の靱性と相関がある。本実施形態に係る低温用H形鋼では、靱性を確保するために、有効結晶粒径を20.0μm以下とする。有効結晶粒径は、15°以上の方位差からなる大角粒界で囲まれる領域の円相当径である。
破壊の起点となる硬質相は、有効結晶粒径よりも微細にすることが必要であり、硬質相の粒径を10.0μm以下とする。硬質相の粒径が10.0μmを超えると、靭性が低下する。
具体的には、光学顕微鏡によって、500μm(フランジ長手方向)×400μm(フランジ厚方向)の長方形内の領域を観察し、フェライト、ベイナイトの一方又は両方の面積率の合計、硬質相の面積率を測定する。このとき、硬質相の粒径の測定も行う。硬質相は、光学顕微鏡によってフェライト、ベイナイト、パーライトと判別して粒径を測定する。また、有効結晶粒径は、EBSDによって、15°以上の方位差からなる大角粒界で囲まれる領域を有効結晶粒として、その円相当径として求める。有効結晶粒径は、フェライト、ベイナイト、硬質相(疑似パーライト、MA)、残部(パーライト)を判別せず、EBSDによって測定する。
円相当径が0.01~3.0μmのTi酸化物は粒内フェライトの核生成サイトとなる。円相当径0.01~3.0μmのTi酸化物は、FL近傍の粗大化したオーステナイトを粒内フェライトの生成によって微細化させ、粒界フェライトや粗大なベイナイトの生成を抑制する。0.01~3.0μmのTi酸化物の個数密度が30個/mm2以上の場合、HAZの-40℃、-60℃でのシャルピー吸収エネルギーが60J以上になる。また、図2に示すように、-20℃におけるHAZの限界CTOD値が0.40mm以上になる。一方、Ti酸化物が30個/mm2未満では、粒内フェライトの生成が不十分となり、HAZ靭性が低下する。従って、HAZ靭性を確保するために、円相当径が0.01~3.0μmのTi酸化物を30個/mm2以上とする。
上述の成分組成の範囲内では靱性に悪影響を及ぼすほどのTi酸化物が生成することはないので個数密度の上限を規定する必要はない。ただし、HAZ靭性を高めるために、円相当径が0.01~3.0μmのTi酸化物の個数密度は100個/mm2以下が好ましい。
観察された介在物がTi酸化物であるかどうかは、形状等からも判断できるが、EDSやEPMA等を用いて、Ti酸化物であることを確認してもよい。
本実施形態に係る低温用H形鋼のフランジの板厚は、12~50mmとする。これは、低温用構造物に用いられるH形鋼には、板厚が12~50mmのサイズのH形鋼が多用されるためである。低温用構造物に用いられるH形鋼のフランジの板厚は、16mm以上であることが好ましい。一方、フランジの板厚が50mmを超えると、圧下量が不足するために組織が粗大化し、脆性破壊を引き起こす可能性がある。フランジの板厚は、40mm以下であることが好ましい。
また、母材及び溶接熱影響部の-40℃及び-60℃でのシャルピー吸収エネルギーの目標値は60J以上である。母材の-40℃及び-60℃でのシャルピー吸収エネルギーは、好ましくは100J以上である。また、遷移曲線(シャルピー試験温度と吸収エネルギーとの関係を示す曲線)を作成した際の吸収エネルギーの最高値が高い方が、構造物の信頼性が高くなるので、-5℃での母材の靭性(シャルピー吸収エネルギー)は、300J以上であることが好ましい。更に、母材及び溶接熱影響部の-20℃における限界CTOD値(き裂先端開口量)の目標値は0.40mm以上であり、pop-inなどの脆性破壊が生じないことがより好ましい。溶接熱影響部の靱性は、最も高温に加熱され、粗粒になる溶融線(FL)をノッチ位置として評価する。鋼の靭性を示す指標として、シャルピー吸収エネルギーとCTOD値とは同様の傾向を示す。しかしながら、その相関は明確でなく、シャルピー吸収エネルギーが目標値を満足しても、CTOD値が目標値を満足するとは言えない。本実施形態に係る低温用H形鋼では、シャルピー吸収エネルギー、CTOD値の両方が目標値を満足する場合に、低温靭性に優れると判断する。
以下、各工程について説明する。
<鋳造工程>
(Ti添加直前の溶鋼中の酸素量:0.0015~0.0110%)
溶製工程及び鋳造工程(図示しない)では、任意の方法で上述した範囲に鋼(溶鋼)の化学成分を調整した後、鋳造し、鋼片を得る。
しかしながら、本実施形態に係る低温用H形鋼を得る場合、鋼中にTi酸化物を形成させるため、成分調整時、Tiを添加する直前の溶鋼に含まれる酸素量を制御する必要がある。溶鋼中の酸素量は、Ti酸化物の形成に十分な量を確保するため、0.0015%以上とする。好ましくは0.0025%以上である。一方、低温靭性を確保するには粗大な酸化物の生成を抑制する必要がある。そのため、溶鋼中の酸素量(酸素濃度)を0.0110%以下に制限する。好ましくは0.0090%以下、より好ましくは0.0080%以下である。Tiを添加し、必要に応じて溶鋼の化学成分を調整した後、鋳造し、鋼片を得る。鋳造は、生産性の観点から、連続鋳造が好ましい。また、鋼片の厚みは、生産性の観点から、200mm以上とすることが好ましく、偏析の低減や、熱間圧延における加熱温度の均質性などを考慮すると、350mm以下が好ましい。
次に、加熱炉を用いて鋼片を加熱し、熱間圧延を行う。熱間圧延は、粗圧延機を用いて行う粗圧延、中間圧延機を用いる中間圧延、仕上圧延機を用いて行う仕上げ圧延からなる。粗圧延は中間圧延の前に、必要に応じて行う工程であり、鋼片の厚みと製品の厚みに応じて行う。また、中間圧延は、中間ユニバーサル圧延機(中間圧延機)と水冷装置(図示しない)とを用いてパス間水冷圧延を行ってもよい。
熱間圧延に供する鋼片の加熱温度は、1100~1350℃とする。加熱温度が低いと変形抵抗が高くなるので、熱間圧延における造形性を確保するために加熱温度を1100℃以上とする。Nbなど、析出物を形成する元素を十分に固溶させるためには、鋼片の加熱温度を1150℃以上とすることが好ましい。特に、製品の板厚が薄い場合は、累積圧下率が大きくなるので、鋼片の加熱温度を1200℃以上にすることが好ましい。一方、鋼片の加熱温度が1350℃を超えると、素材である鋼片の表面の酸化物が溶融して加熱炉内が損傷することがある。そのため、加熱温度は1350℃以下とする。組織を微細にするためには、鋼片の加熱温度を1300℃以下にすることが好ましい。
熱間圧延の仕上温度は(Ar3-30)℃以上900℃以下とする。仕上温度が900℃を超えると圧延後に粗大なオーステナイトが残存する。この粗大なオーステナイトが冷却によって粗大なベイナイトに変態すると脆性破壊の起点となり、靱性が低下する。好ましくは仕上温度を850℃以下とする。熱間圧延の仕上温度は、H形鋼の形状精度等を考慮して、フェライト変態の開始温度である(Ar3-30)℃以上とする。Ar3は、下記式(2)によって求めることができる。下記式(2)おいて、C、Si、Mn、Ni、Cu、Cr、Moは、各元素の質量%での含有量であり、含有しない場合は、これらの含有量を0としてAr3を求める。
熱間圧延の終了後は、そのまま、仕上圧延機の出側に設けた水冷装置(全断面水冷装置)によって、フランジの内面及び外面に加速冷却を施す。仕上圧延機から全断面水冷装置までの間は空冷されるが、加速冷却の開始温度は熱間圧延の仕上温度と同等であるか、やや低下することがあっても、特性にはほとんど影響しない。また、フランジの内面及び外面に加速冷却を施すことにより、フランジの内外面の冷却速度が均一になり、材質及び形状精度を向上させることができる。ウェブの上面はフランジの内面に噴射した冷却水によって、上面側が冷却される。ウェブの反りを抑制するため、ウェブの下面側から冷却してもよい。
加速冷却は、例えば、図1に示す水冷装置によって、H形鋼1のフランジ2の外面、内面ともに、スプレー冷却(スプレーノズル4からの冷却水5による冷却)によって行う。加速冷却の冷却速度は、有効結晶粒径の粗大化や、疑似パーライト及びMAの一方または両方からなる硬質相の生成を抑制して靭性を向上させ、かつ焼入れの効果によって強度を高めるため、15℃/秒超とする。冷却速度が15℃/秒超の加速冷却を施し、組織の微細化を図ることで、0.005%以上のNbを含有させても、低温靭性を確保できる。一方、本実施形態に係る低温用H形鋼ではTiOXを生成させているので、鋼中のTiNが減少し、初期オーステナイトが粗大化しやすい。そのため、加速冷却速度が15℃/秒以下では粗大組織の生成による靭性低下が顕著となる。加速冷却の冷却速度は、好ましくは18℃/秒以上、より好ましくは20℃/秒以上とする。加速冷却の冷却速度の上限は限定しないが、形状精度を考慮すると、50℃/秒以下が好ましい。
本実施形態において、加速冷却の冷却速度とは、図7に示すように、加速冷却開始時の表面温度と復熱後の表面温度との温度差(ΔT)を、水冷時間(Δt1)で割って算出する。水冷終了から復熱完了までの時間(Δt2)は、考慮しない。
加速冷却は、H形鋼の表面温度が300℃以下になるまで行う。冷却停止時(水冷終了時)のH形鋼の表面温度が300℃超では、硬質相の増加や組織の粗大化により靭性が低下する。
H形鋼の表面の温度は、加速冷却によって内部の温度に比べて早く低下するが、加速冷却を停止した後、内部からの熱伝導によって上昇し、内部温度と等しくなる。本実施形態では、このような復熱後に表面温度が到達する最高温度を一定の範囲内に制御するように加速冷却を行う。具体的には、復熱後のフランジ幅の外側から1/6の位置での表面の最高到達温度が、350~700℃となるように加速冷却を行う。復熱による最高到達温度が700℃を超えると、有効結晶粒径の粗大化や硬質相(主に疑似パーライト)の増加によって靱性が低下する。一方、最高到達温度が350℃未満になると強度の上昇や硬質相(主にMA)の増加によって低温靭性が低下する。図3に示すように、加速冷却後の復熱温度が350~700℃の間でH形鋼(母材)の低温靭性が向上しており、目標である60J以上になる。
加速冷却後、強度及び靭性を調整するために熱処理を施してもよい。この熱処理は、オーステナイトへの変態が開始する温度(Ac1)以下で行えばよいが、100~700℃の範囲で行うことが好ましい。より好ましくは、下限を300℃、上限を650℃とする。更に好ましくは、下限を400℃、上限を600℃とする。
得られた鋼片を表3及び4に示す条件で、加熱し、熱間圧延を行い、加速冷却を施した。表3及び4の復熱温度は、加速冷却停止後の復熱による最高到達温度を意味する。熱間圧延では、粗圧延に続いて、中間ユニバーサル圧延機と、その前後に設けた水冷装置とを用いて、フランジ外側面のスプレー冷却とリバース圧延とを行った。表1及び表2に示した成分は、製造後のH形鋼から採取した試料を化学分析して求めた。
2 フランジ
3 ウェブ
4 スプレーノズル
5 冷却水
Claims (3)
- 質量%で、
C:0.03~0.13%、
Mn:0.80~2.00%、
Nb:0.005~0.060%、
Ti:0.005~0.025%、
O:0.0005~0.0100%、
V:0~0.08%、
Cu:0~0.40%、
Ni:0~0.70%、
Mo:0~0.10%、
Cr:0~0.20%、
を含有し、
Si:0.50%以下、
Al:0.008%以下、
Ca:0.0010%以下、
REM:0.0010%以下、
Mg:0.0010%以下、
N:0.0120%以下
に制限し、残部がFe及び不純物からなり、
下記式(1)によって求められるCEVが0.40以下であり、
フランジの板厚の外側から1/4の位置かつフランジ幅の外側から1/6の位置での、フェライト及びベイナイトの一方又は両方の面積率の合計が90%以上、かつ、硬質相の面積率が10%以下であり、
有効結晶粒径が20.0μm以下、かつ、硬質相の粒径が10.0μm以下であり、
円相当径が0.01~3.0μmのTi酸化物を30個/mm2以上有し、
前記フランジの板厚が12~50mmである
ことを特徴とする低温用H形鋼。
CEV=C+Mn/6+(Cr+Mo+V)/5+(Ni+Cu)/15 ・・・(1)
ここで、C、Mn、Cr、Mo、V、Ni、Cuは、各元素の質量%での含有量である。 - 質量%で、
V:0.01~0.08%、
Cu:0.01~0.40%、
Ni:0.01~0.70%、
Mo:0.01~0.10%、
Cr:0.01~0.20%
からなる群から選択される1種又は2種以上を含有する
ことを特徴とする請求項1に記載の低温用H形鋼。 - 請求項1又は2に記載の低温用H形鋼の製造方法であって、
請求項1又は2に記載の低温用H形鋼と同じ化学成分からなる鋼を溶製する溶製工程と、
前記溶製工程で得られた前記鋼を鋳造して鋼片を得る鋳造工程と、
前記鋼片を、1100~1350℃に加熱し、その後、仕上温度が(Ar3-30)℃以上900℃以下となるように熱間圧延を行ってH形鋼を得る熱間圧延工程と、
前記H形鋼を、冷却速度が15℃/秒超となるようにフランジの内外面に水冷を行う加速冷却工程と、
を有し、
前記溶製工程では、Tiを添加する直前の溶鋼の酸素濃度を0.0015~0.0110質量%の範囲に調整した後に、前記Tiを添加し、
前記加速冷却工程では、前記H形鋼のフランジ幅の外側から1/6の位置での冷却停止温度が表面温度で300℃以下になるように、かつ、前記表面温度の復熱後の最高温度が350~700℃になるように前記水冷を行う
ことを特徴とする低温用H形鋼の製造方法。
Priority Applications (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201780012914.1A CN108699651A (zh) | 2016-03-02 | 2017-03-02 | 低温用h形钢及其制造方法 |
| KR1020187023882A KR20180102175A (ko) | 2016-03-02 | 2017-03-02 | 저온용 h형강 및 그 제조 방법 |
| US16/079,265 US10900099B2 (en) | 2016-03-02 | 2017-03-02 | Steel H-shape for low temperature service and manufacturing method therefor |
| EP17760128.3A EP3425080B2 (en) | 2016-03-02 | 2017-03-02 | Steel h-shape for low temperature service and manufacturing method therefor |
| JP2018503395A JP6390813B2 (ja) | 2016-03-02 | 2017-03-02 | 低温用h形鋼及びその製造方法 |
| PH12018501726A PH12018501726A1 (en) | 2016-03-02 | 2018-08-15 | Steel h-shape for low temperature service and manufacturing method therefor |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2016-039957 | 2016-03-02 | ||
| JP2016039957 | 2016-03-02 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2017150665A1 true WO2017150665A1 (ja) | 2017-09-08 |
Family
ID=59744079
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/JP2017/008275 Ceased WO2017150665A1 (ja) | 2016-03-02 | 2017-03-02 | 低温用h形鋼及びその製造方法 |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US10900099B2 (ja) |
| EP (1) | EP3425080B2 (ja) |
| JP (1) | JP6390813B2 (ja) |
| KR (1) | KR20180102175A (ja) |
| CN (1) | CN108699651A (ja) |
| PH (1) | PH12018501726A1 (ja) |
| WO (1) | WO2017150665A1 (ja) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20200058524A (ko) * | 2017-10-31 | 2020-05-27 | 제이에프이 스틸 가부시키가이샤 | H 형강 및 그 제조 방법 |
| JP2023505172A (ja) * | 2019-12-09 | 2023-02-08 | 山東鋼鉄股▲ふん▼有限公司 | ビームブランク圧延成形に基づく熱間圧延h字型鋼及びその作製方法 |
| JP2024532648A (ja) * | 2022-07-20 | 2024-09-10 | 山東鋼鉄股▲ふん▼有限公司 | 高強靱性を有する建築用の熱間圧延されたh字型鋼及びその製造方法 |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113604735B (zh) * | 2021-07-20 | 2022-07-12 | 山东钢铁股份有限公司 | 一种屈服强度420MPa级热轧耐低温H型钢及其制备方法 |
| KR20250094963A (ko) * | 2023-12-19 | 2025-06-26 | 현대제철 주식회사 | 형강 및 형강 제조 방법 |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2000045042A (ja) * | 1998-07-29 | 2000-02-15 | Nippon Steel Corp | 引張り強度が490N平方mm以上の曲げ加工性の良いトンネル支保工用H形鋼およびその製造方法 |
| JP2006144087A (ja) * | 2004-11-22 | 2006-06-08 | Jfe Steel Kk | ウエブ薄肉高強度h形鋼及びその製造方法 |
| JP2011157573A (ja) * | 2010-01-29 | 2011-08-18 | Nippon Steel Corp | 靱性に優れた高強度極厚h形鋼およびその製造方法 |
| WO2015093321A1 (ja) * | 2013-12-16 | 2015-06-25 | 新日鐵住金株式会社 | H形鋼及びその製造方法 |
Family Cites Families (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US972A (en) * | 1838-10-08 | Machine fob shei | ||
| JP2579842B2 (ja) * | 1991-03-08 | 1997-02-12 | 新日本製鐵株式会社 | 圧延ままで靱性に優れ、かつ溶接部靱性に優れた粒内フェライト系形鋼の製造方法 |
| JP2607796B2 (ja) | 1992-03-16 | 1997-05-07 | 新日本製鐵株式会社 | 靭性の優れた低合金圧延形鋼の製造方法 |
| JP2543282B2 (ja) | 1992-03-25 | 1996-10-16 | 新日本製鐵株式会社 | 靭性の優れた制御圧延形鋼の製造方法 |
| JP2760713B2 (ja) | 1992-09-24 | 1998-06-04 | 新日本製鐵株式会社 | 耐火性及び靱性の優れた制御圧延形鋼の製造方法 |
| JP3241199B2 (ja) | 1994-02-07 | 2001-12-25 | 新日本製鐵株式会社 | 酸化物粒子分散鋳片及びその鋳片を素材とする靭性の優れた圧延形鋼の製造方法 |
| US5743972A (en) * | 1995-08-29 | 1998-04-28 | Kawasaki Steel Corporation | Heavy-wall structural steel and method |
| JP3426425B2 (ja) | 1995-10-05 | 2003-07-14 | 新日本製鐵株式会社 | 耐火圧延形鋼用鋳片およびそれを素材とする耐火用圧延形鋼の製造方法 |
| JP3472017B2 (ja) | 1996-02-23 | 2003-12-02 | 新日本製鐵株式会社 | 耐火圧延形鋼およびその製造方法 |
| DE19757485A1 (de) † | 1997-12-23 | 1999-06-24 | Schloemann Siemag Ag | Vorrichtung zum kontrollierten Abkühlen von warmgewalzten Profilen, insbesondere Trägern, direkt aus der Walzhitze |
| JP4736205B2 (ja) | 2001-03-02 | 2011-07-27 | Jfeスチール株式会社 | 耐震性および小入熱溶接性に優れたTS590MPa以上の高強度H形鋼の製造方法 |
| JP4329583B2 (ja) † | 2004-03-17 | 2009-09-09 | Jfeスチール株式会社 | 耐震性に優れた低降伏比h形鋼およびその製造方法 |
| JP4631299B2 (ja) | 2004-03-25 | 2011-02-16 | Jfeスチール株式会社 | 耐火性に優れた低降伏比圧延h形鋼およびその製造法 |
| JP4696602B2 (ja) | 2005-03-09 | 2011-06-08 | Jfeスチール株式会社 | 低温靭性に優れる圧延h形鋼の製造方法 |
| US8647564B2 (en) | 2007-12-04 | 2014-02-11 | Posco | High-strength steel sheet with excellent low temperature toughness and manufacturing thereof |
| EP2305850B1 (en) * | 2008-07-30 | 2013-11-27 | Nippon Steel & Sumitomo Metal Corporation | High-strength thick steel products excellent in toughness and weldability, high-strength ultra-thick h shape steel and processes for manufacturing both |
| WO2011065479A1 (ja) † | 2009-11-27 | 2011-06-03 | 新日本製鐵株式会社 | 高強度極厚h形鋼及びその製造方法 |
| US9644372B2 (en) * | 2011-12-15 | 2017-05-09 | Nippon Steel & Sumitomo Metal Corporation | High-strength H-beam steel exhibiting excellent low-temperature toughness and method of manufacturing same |
| CN104487604B (zh) * | 2012-11-26 | 2016-11-02 | 新日铁住金株式会社 | H 型钢及其制造方法 |
| KR101883588B1 (ko) | 2014-04-15 | 2018-07-30 | 신닛테츠스미킨 카부시키카이샤 | H형강 및 그 제조 방법 |
-
2017
- 2017-03-02 EP EP17760128.3A patent/EP3425080B2/en active Active
- 2017-03-02 JP JP2018503395A patent/JP6390813B2/ja active Active
- 2017-03-02 KR KR1020187023882A patent/KR20180102175A/ko not_active Ceased
- 2017-03-02 WO PCT/JP2017/008275 patent/WO2017150665A1/ja not_active Ceased
- 2017-03-02 CN CN201780012914.1A patent/CN108699651A/zh active Pending
- 2017-03-02 US US16/079,265 patent/US10900099B2/en active Active
-
2018
- 2018-08-15 PH PH12018501726A patent/PH12018501726A1/en unknown
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2000045042A (ja) * | 1998-07-29 | 2000-02-15 | Nippon Steel Corp | 引張り強度が490N平方mm以上の曲げ加工性の良いトンネル支保工用H形鋼およびその製造方法 |
| JP2006144087A (ja) * | 2004-11-22 | 2006-06-08 | Jfe Steel Kk | ウエブ薄肉高強度h形鋼及びその製造方法 |
| JP2011157573A (ja) * | 2010-01-29 | 2011-08-18 | Nippon Steel Corp | 靱性に優れた高強度極厚h形鋼およびその製造方法 |
| WO2015093321A1 (ja) * | 2013-12-16 | 2015-06-25 | 新日鐵住金株式会社 | H形鋼及びその製造方法 |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20200058524A (ko) * | 2017-10-31 | 2020-05-27 | 제이에프이 스틸 가부시키가이샤 | H 형강 및 그 제조 방법 |
| KR20220060560A (ko) * | 2017-10-31 | 2022-05-11 | 제이에프이 스틸 가부시키가이샤 | H 형강 및 그 제조 방법 |
| KR102419239B1 (ko) * | 2017-10-31 | 2022-07-08 | 제이에프이 스틸 가부시키가이샤 | H 형강 및 그 제조 방법 |
| KR102419241B1 (ko) | 2017-10-31 | 2022-07-11 | 제이에프이 스틸 가부시키가이샤 | H 형강 및 그 제조 방법 |
| JP2023505172A (ja) * | 2019-12-09 | 2023-02-08 | 山東鋼鉄股▲ふん▼有限公司 | ビームブランク圧延成形に基づく熱間圧延h字型鋼及びその作製方法 |
| JP2024532648A (ja) * | 2022-07-20 | 2024-09-10 | 山東鋼鉄股▲ふん▼有限公司 | 高強靱性を有する建築用の熱間圧延されたh字型鋼及びその製造方法 |
Also Published As
| Publication number | Publication date |
|---|---|
| EP3425080A4 (en) | 2019-10-30 |
| EP3425080A1 (en) | 2019-01-09 |
| JP6390813B2 (ja) | 2018-09-19 |
| PH12018501726B1 (en) | 2019-05-20 |
| KR20180102175A (ko) | 2018-09-14 |
| JPWO2017150665A1 (ja) | 2018-10-18 |
| EP3425080B2 (en) | 2024-07-24 |
| CN108699651A (zh) | 2018-10-23 |
| PH12018501726A1 (en) | 2019-05-20 |
| US10900099B2 (en) | 2021-01-26 |
| US20190048435A1 (en) | 2019-02-14 |
| EP3425080B1 (en) | 2021-05-26 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP3042976B1 (en) | Steel sheet for thick-walled high-strength line pipe having exceptional corrosion resistance, crush resistance properties, and low-temperature ductility, and line pipe | |
| JP6665525B2 (ja) | 低温用h形鋼及びその製造方法 | |
| JP5574059B2 (ja) | 低温靭性に優れた高強度h形鋼及びその製造方法 | |
| CN101652495B (zh) | 高温特性和韧性优良的钢材及其制造方法 | |
| JP6123973B2 (ja) | 高強度・高靭性鋼板およびその製造方法 | |
| CN101657555B (zh) | 高温强度和韧性优良的钢材及其制造方法 | |
| JP4897126B2 (ja) | 厚鋼板の製造方法 | |
| JP6354572B2 (ja) | 低温用h形鋼及びその製造方法 | |
| JP6123972B2 (ja) | 高強度・高靭性鋼板およびその製造方法 | |
| US12195817B2 (en) | Hot-rolled steel sheet and weld joint, and methods for producing same | |
| WO2014175122A1 (ja) | H形鋼及びその製造方法 | |
| JP6390813B2 (ja) | 低温用h形鋼及びその製造方法 | |
| JP2016079443A (ja) | 靭性に優れた高強度極厚h形鋼及びその製造方法 | |
| JP2017071827A (ja) | H形鋼及びその製造方法 | |
| JP7155703B2 (ja) | ラインパイプ用厚鋼板およびその製造方法 | |
| JP6421907B1 (ja) | 圧延h形鋼及びその製造方法 | |
| JP6421638B2 (ja) | 低温用h形鋼及びその製造方法 | |
| JP6624145B2 (ja) | 高強度・高靭性厚鋼板の製造方法 | |
| JP6662156B2 (ja) | 低温用h形鋼及びその製造方法 | |
| JP2017057483A (ja) | H形鋼及びその製造方法 |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ENP | Entry into the national phase |
Ref document number: 2018503395 Country of ref document: JP Kind code of ref document: A |
|
| ENP | Entry into the national phase |
Ref document number: 20187023882 Country of ref document: KR Kind code of ref document: A |
|
| WWE | Wipo information: entry into national phase |
Ref document number: 1020187023882 Country of ref document: KR |
|
| NENP | Non-entry into the national phase |
Ref country code: DE |
|
| WWE | Wipo information: entry into national phase |
Ref document number: 2017760128 Country of ref document: EP |
|
| ENP | Entry into the national phase |
Ref document number: 2017760128 Country of ref document: EP Effective date: 20181002 |
|
| 121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 17760128 Country of ref document: EP Kind code of ref document: A1 |