WO2016190397A1 - 鋼板及びその製造方法 - Google Patents
鋼板及びその製造方法 Download PDFInfo
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- WO2016190397A1 WO2016190397A1 PCT/JP2016/065630 JP2016065630W WO2016190397A1 WO 2016190397 A1 WO2016190397 A1 WO 2016190397A1 JP 2016065630 W JP2016065630 W JP 2016065630W WO 2016190397 A1 WO2016190397 A1 WO 2016190397A1
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
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- 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
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- C21D6/00—Heat treatment of ferrous alloys
- C21D6/005—Heat treatment of ferrous alloys containing Mn
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- 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
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- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0205—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips of ferrous alloys
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- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0226—Hot rolling
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- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
- C21D8/0263—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment following hot rolling
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/002—Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/008—Ferrous alloys, e.g. steel alloys containing tin
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/08—Ferrous alloys, e.g. steel alloys containing nickel
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- 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
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/14—Ferrous alloys, e.g. steel alloys containing titanium or zirconium
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- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/16—Ferrous alloys, e.g. steel alloys containing copper
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/22—Ferrous alloys, e.g. steel alloys containing chromium with molybdenum or tungsten
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/24—Ferrous alloys, e.g. steel alloys containing chromium with vanadium
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- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/26—Ferrous alloys, e.g. steel alloys containing chromium with niobium or tantalum
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/28—Ferrous alloys, e.g. steel alloys containing chromium 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
- C22C38/32—Ferrous alloys, e.g. steel alloys containing chromium with boron
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/60—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
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23G—CLEANING OR DE-GREASING OF METALLIC MATERIAL BY CHEMICAL METHODS OTHER THAN ELECTROLYSIS
- C23G1/00—Cleaning or pickling metallic material with solutions or molten salts
- C23G1/02—Cleaning or pickling metallic material with solutions or molten salts with acid solutions
- C23G1/08—Iron or steel
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- 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
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- 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
- C21D2211/009—Pearlite
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23G—CLEANING OR DE-GREASING OF METALLIC MATERIAL BY CHEMICAL METHODS OTHER THAN ELECTROLYSIS
- C23G1/00—Cleaning or pickling metallic material with solutions or molten salts
Definitions
- the present invention relates to a steel plate and a manufacturing method thereof.
- Automotive parts, blades, and other machine parts are manufactured through processing steps such as punching, bending, and pressing.
- processing steps such as punching, bending, and pressing.
- it is necessary to improve the workability of the carbon steel plate as a raw material in order to improve and stabilize the product quality and reduce the manufacturing cost.
- the carbon steel sheet may be deformed by high-speed rotation or the like, and may be broken due to insufficient ductility. Therefore, ductility after heat treatment is required.
- a carbon steel plate is subjected to cold rolling and spheroidizing annealing, and a carbon steel plate is used as a soft material having good workability made of ferrite and spheroidized carbide. And until now, several techniques for improving the workability of carbon steel sheets have been proposed.
- Patent Document 1 C: 0.15 to 0.90 mass%, Si: 0.40 mass% or less, Mn: 0.3 to 1.0 mass%, P: 0.03 mass% or less, Total Al: 0.10 mass% or less, Ti: 0.01 to 0.05 mass%, B: 0.0005 to 0.0050 mass%, N: 0.01 mass% or less, Cr: 1.2 mass%
- a high-carbon steel sheet for precision punching having a structure in which carbides having an average carbide particle size of 0.4 to 1.0 ⁇ m and a spheroidization rate of 80% or more are dispersed in a ferrite matrix, and a notch tensile elongation is 20% or more; The manufacturing method is disclosed.
- Patent Document 2 C: 0.3 to 1.3% by mass, Si: 1.0% by mass or less, Mn: 0.2 to 1.5% by mass, P: 0.02% by mass or less, S: 0.02% by mass or less, and carbide is dispersed so that the relationship of C GB / C IG ⁇ 0.8 is established between the carbide C GB on the ferrite grain boundary and the number of carbides C IG in the ferrite crystal grain
- a medium and high carbon steel sheet excellent in workability and a method for producing the same are disclosed, characterized by having a texture that is made and having a cross-sectional hardness of 160 HV or less.
- Patent Document 3 C: 0.30 to 1.00 mass%, Si: 1.0 mass% or less, Mn: 0.2 to 1.5 mass%, P: 0.02 mass% or less, S: A relationship of C GB / C IG ⁇ 0.8 holds between the carbide C GB on the ferrite grain boundary and the number of carbides C IG in the ferrite crystal grain including 0.02% by mass or less, and all carbides
- a medium and high carbon steel sheet excellent in workability is disclosed, characterized by having a structure in which a carbide occupying 90% or more of the spheroidized carbide having a major axis / minor axis of 2 or less is dispersed in ferrite. .
- S gb ⁇ S on / (S on + S in ) ⁇ ⁇ 100 (where S on : per unit area) of the carbides present, the total area occupied by the carbides present on the grain boundary, S in: out of the carbides present per unit area, the ferrite grain boundary carbides, which is defined by the total occupied area)
- Patent Document 5 promotes the spheroidization of carbides and suppresses the grain growth of ferrite by performing appropriate hot-rolled sheet annealing on a hot-rolled sheet having a pearlite structure of almost 100%, It is characterized in that many carbides are present on the ferrite grain boundaries.
- Patent Document 6 is a solid solution of ferrite by actively utilizing Si as a structural structure mainly composed of ferrite, the second phase with a low martensite fraction and mainly composed of carbides such as cementite. It is characterized by ensuring strength by strengthening and ensuring ductility by improving the work hardening ability of ferrite itself.
- Patent Document 7 discloses a technique for producing a soft medium carbon steel sheet excellent in induction hardenability by controlling the ferrite grain size to 10 ⁇ m or more.
- the manufacturing method disclosed in Patent Document 7 is characterized in that the ferrite grains of the steel sheet are coarsened by box annealing that is heated to 600 ° C. to 750 ° C., thereby softening the steel sheet.
- the steel sheet disclosed in Patent Document 8 10 to 50% of the C content is graphitized, and the steel structure of the cross section is C weight% ⁇ 10 2 pieces / mm 2 or more C weight% of 3 ⁇ m-sized graphite particles. It is characterized in that it is a ferrite phase in which spheroidized cementite is dispersed, containing 10 3 / mm 2 or less.
- the production method disclosed in Patent Document 8 is characterized in that a hot-rolled sheet is annealed in the range of 600 ° C. to 720 ° C. from the viewpoint of graphitization of the steel sheet.
- the steel sheet disclosed in Patent Document 9 includes a bainite phase having an area ratio of 90% or more, and among all Fe-based carbides precipitated in the bainite phase, Fe precipitated in bainitic ferrite grains. It is characterized by having a structure in which the number ratio of the system carbide is 30% or more and the average particle diameter of the Fe system carbide precipitated in the bainitic ferrite grains is 150 nm or less.
- Patent Documents 2 and 3 both describe that the low spheroidization rate of carbides precipitated at grain boundaries (referred to as “grain boundary carbides”) is a cause of deterioration of workability.
- grain boundary carbides the low spheroidization rate of carbides precipitated at grain boundaries
- Patent Documents 2 and 3 has a problem of improving workability by improving the spheroidization rate of grain boundary carbides.
- the tissue factor is only defined, and the relationship between workability and mechanical properties is not studied.
- Patent Documents 5 to 9 do not specify the conditions for the annealing process from the viewpoint of promoting the precipitation of carbides on the ferrite grain boundaries. Further, since the cooling conditions after the annealing process are not specified in Patent Documents 5 to 9, in the manufacturing methods disclosed in Patent Documents 5 to 9, the austenite generated after the annealing is transformed into pearlite and the steel sheet is hardened. There is a risk that the cold formability will be reduced.
- Patent Document 10 after the finish-rolled steel sheet is wound at a winding temperature of 400 ° C. or higher and lower than 650 ° C., the first annealing at 680 ° C. or higher and 720 ° C. or lower and the second annealing at 730 ° C. or higher and 790 ° C. or lower are performed. It discloses that after annealing for the second time, the steel sheet is annealed at a cooling rate of 20 ° C./hr from the viewpoint of cementite spheroidization. However, in the manufacturing method of Patent Document 10, the finish rolling is finished at 600 ° C.
- the present invention is based on the prior art, and an object of the present invention is to improve cold formability and post-heat treatment ductility in a steel sheet, and an object of the present invention is to provide a steel sheet that solves the problem and a method for manufacturing the same.
- the cold formability refers to the deformability of a steel plate that can be easily plastically deformed into a required shape without defects when the steel plate is plastically deformed into a required shape by cold working or cold forging.
- the ductility after heat treatment is the ductility of the steel plate after heat treatment.
- the ferrite grain size is increased, and carbide (mainly cementite) is obtained.
- carbide mainly cementite
- the ferrite phase has low hardness and high ductility. Therefore, it is possible to improve the material formability by increasing the grain size in a structure mainly composed of ferrite.
- carbides in the steel sheet are strong particles that prevent slipping, and by allowing carbides to exist at the ferrite grain boundaries, it is possible to prevent the propagation of slips across the crystal grain boundaries and suppress the formation of shear bands. It can improve the cold forgeability and at the same time improve the formability of the steel sheet.
- cementite is a hard and brittle structure, and if it exists in the state of pearlite, which is a layered structure with ferrite, the steel becomes hard and brittle, so it must be present in a spherical shape. In consideration of cold forgeability and generation of cracks during forging, the particle size needs to be in an appropriate range.
- the metal structure of the steel sheet after coiling after hot rolling becomes a bainite structure in which cementite is dispersed in fine pearlite or fine ferrite with a small lamellar spacing, so that the temperature is relatively low (400 ° C to 550 ° C). Take up with.
- cementite dispersed in the ferrite is also easily spheroidized.
- the cementite is partially spheroidized by annealing at a temperature just below the Ac1 point as the first stage annealing.
- annealing is performed at a temperature between Ac1 point and Ac3 point (so-called two-phase region of ferrite and austenite), and a part of the ferrite grains is left, and a part thereof is austenite transformed. Thereafter, the ferrite grains left by slow cooling were grown, and austenite was transformed into ferrite by using the ferrite grains as a nucleus, so that cementite was precipitated at the grain boundaries while obtaining a large ferrite phase, and the above structure was found to be realized.
- the present inventors have optimized the dispersion state of carbides in the steel sheet structure before cold working of the steel sheet with the optimized component composition and the manufacturing conditions in the integrated process from hot rolling to annealing.
- the steel sheet structure can be controlled to allow carbides having an appropriate particle size to precipitate at the ferrite grain boundaries.
- the present inventors have found that excellent cold formability and post-heat treatment ductility can be secured in a steel sheet when the ferrite grain size is 5 ⁇ m or more and the Vickers hardness is 170 or less.
- the present invention has been made on the basis of the above findings, and the gist thereof is as follows.
- the component composition is mass%, C: 0.10 to 0.40%, Si: 0.30 to 1.00%, Mn: 0.30 to 1.00% Al: 0.001 to 0.10%, P: 0.02% or less, S: In a steel plate containing 0.01% or less, the balance being Fe and impurities,
- the ratio (B / A) of the number of carbides (B) in the ferrite grain boundary to the number of carbides (A) in the ferrite grains exceeds 1,
- the ferrite particle size is 5 ⁇ m or more and 50 ⁇ m or less,
- the average particle size of the carbide is 0.4 ⁇ m or more and 2.0 ⁇ m or less, Perlite area ratio is 6% or less, A steel sheet having a Vickers hardness of 120HV or more and 170HV or less.
- the steel sheet is further in mass%, N: 0.01% or less, O 2: Steel plate according to (1) above, containing 0.02% or less of one type or two or more types.
- the steel sheet is further in mass%, Ti: 0.10% or less, Cr: 0.50% or less, Mo: 0.50% or less, B: 0.01% or less, Nb: 0.10% or less, V: 0.10% or less, Cu: 0.10% or less, W: 0.10% or less, Ta: 0.10% or less, Ni: 0.10% or less, Sn: 0.05% or less, Sb: 0.05% or less, As: 0.05% or less, Mg: 0.05% or less, Ca: 0.05% or less, Y: 0.05% or less, Zr: 0.05% or less, La: 0.05% or less, Ce: The steel plate according to (1) or (2) above, containing one or more of 0.05% or less.
- a manufacturing method for manufacturing the steel sheet according to any one of (1) to (3) (I) The steel slab having the component composition described in any one of (1) to (3) is directly or once cooled and heated and then subjected to hot rolling, in a temperature range of 800 ° C to 900 ° C. The hot rolled steel sheet that has been finish-rolled is scraped at 400 ° C. or higher and 550 ° C. or lower, (Ii) The rolled hot-rolled steel sheet is taken out and subjected to pickling, and then subjected to a first stage annealing that is held in a temperature range of 650 ° C. to 720 ° C. for 3 hours to 60 hours, and further 725 ° C. or more.
- a second step annealing is performed in which a second stage annealing is performed in a temperature range of 790 ° C. or lower and held for 3 hours or more and 50 hours or less,
- (Iii) A method for producing a steel sheet, characterized in that the hot-rolled steel sheet after annealing is cooled to 650 ° C. at a cooling rate controlled to 1 ° C./hour or more and 30 ° C./hour or less and then cooled to room temperature.
- the steel sheet of the present invention has high ductility after heat treatment, is excellent in plate formability before heat treatment, and can be suitably used for fatigue parts to which repeated stress is applied, such as automobile undercarriage structural parts.
- % means mass%.
- C is an element that forms carbides and is effective in strengthening steel and refining ferrite grains.
- C is made 0.10% or more.
- C is made 0.14% or more.
- C exceeds 0.40%, the volume fraction of carbide increases, and cold formability and ductility after heat treatment decrease, so C is made 0.40% or less.
- it is 0.38% or less.
- Si 0.30 to 1.00%
- Si is an element that affects the form of carbide and contributes to the improvement of ductility after heat treatment.
- two-step annealing (hereinafter sometimes referred to as “two-stage annealing”) is used to austenite during annealing. It is necessary to generate a phase, once dissolve the carbide, and then slowly cool to promote precipitation of the carbide on the ferrite grain boundary.
- the Si content is 0.30% or more. Preferably it is 0.35% or more.
- the Si content is made 1.00% or less. Preferably it is 0.90% or less.
- Mn is an element that controls the form of carbide in two-stage annealing. If it is less than 0.30%, it becomes difficult to generate carbides at the ferrite grain boundaries in the slow cooling after the two-stage annealing, so Mn is set to 0.30% or more. Preferably it is 0.33% or more. On the other hand, if it exceeds 1.00%, the hardness of the ferrite increases and the cold formability decreases, so Mn is made 1.00% or less. Preferably it is 0.96% or less.
- Al 0.001 to 0.10%
- Al is an element that acts as a deoxidizer and stabilizes ferrite. If the content is less than 0.001%, the above-described effect due to addition cannot be obtained sufficiently, so Al is made 0.001% or more. Preferably it is 0.004% or more. On the other hand, if it exceeds 0.10%, the number of carbides at the ferrite grain boundary decreases and the cold formability deteriorates, so Al is made 0.10% or less. Preferably it is 0.09% or less.
- P is an element that segregates at the ferrite grain boundaries and suppresses the formation of carbides at the ferrite grain boundaries. Therefore, the content of P is preferably as low as possible, and may be 0%. However, if the content is reduced to less than 0.0001%, the refining cost is greatly increased, so it may be 0.0001% or more. The content of P may be 0.0013% or more. On the other hand, if P exceeds 0.02%, the formation of carbides at the ferrite grain boundaries is suppressed, the number of carbides decreases, and the cold formability deteriorates, so P is made 0.02% or less. Preferably it is 0.01% or less.
- S is an element that forms non-metallic inclusions such as MnS. Since non-metallic inclusions are the starting point of cracking during cold forming, S is preferably as small as possible, and may be 0%. However, if the content is reduced to less than 0.0001%, the refining cost will be greatly increased. It may be 0001% or more. The S content may be 0.0012% or more. On the other hand, if it exceeds 0.01%, non-metallic inclusions are generated and the cold formability deteriorates, so S is made 0.01% or less. Preferably it is 0.009% or less.
- the steel sheet of the present invention may contain the following elements in addition to the above elements.
- N is an element that embrittles ferrite when present in a large amount. Therefore, N is preferably as small as possible, and the content of N may be 0, but if it is reduced to less than 0.0001%, the refining cost will be greatly increased, so it may be 0.0001% or more. The N content may be 0.0006% or more. On the other hand, if it exceeds 0.01%, ferrite becomes brittle and cold formability deteriorates, so N is made 0.01% or less. Preferably it is 0.007% or less.
- O when present in a large amount, is an element that forms a coarse oxide. Therefore, O is preferably as small as possible, and may be 0%, but if it is reduced to less than 0.0001%, the refining cost will be greatly increased, so it may be 0.0001% or more. The O content may be 0.0011% or more. On the other hand, if it exceeds 0.02%, a coarse oxide is generated in the steel and becomes a starting point of cracking during cold forming, so O is made 0.02% or less. Preferably it is 0.01% or less.
- the steel sheet of the present invention may further contain one or more of the following elements.
- the content may be 0%.
- Ti 0.10% or less
- Ti is an element that forms a nitride and contributes to refinement of crystal grains. If it is less than 0.001%, the effect of addition cannot be sufficiently obtained, so Ti is preferably made 0.001% or more. More preferably, it is 0.005% or more. On the other hand, if it exceeds 0.10%, coarse Ti nitrides are produced and cold formability deteriorates, so Ti is made 0.10% or less. Preferably it is 0.07% or less.
- Cr 0.50% or less
- Cr is an element that contributes to the improvement of hardenability, stabilizes the carbide by concentrating on the carbide, and forms a stable carbide even in the austenite phase. If it is less than 0.001%, the effect of improving hardenability cannot be obtained, so Cr is preferably made 0.001% or more. More preferably, it is 0.007% or more. On the other hand, if it exceeds 0.50%, stable carbides are generated in the austenite phase, the dissolution of carbides is delayed during quenching, and the required quenching strength cannot be obtained, so Cr is 0.50% or less. Preferably it is 0.48% or less.
- Mo 0.50% or less
- Mo is an element that is effective in controlling the morphology of carbides, and is an element that contributes to improving ductility by refining the structure. If it is less than 0.001%, the effect of addition cannot be obtained, so Mo is preferably 0.001% or more. More preferably, it is 0.017% or more. On the other hand, if it exceeds 0.50%, the in-plane anisotropy of the r value is lowered and the cold formability is lowered, so Mo is made 0.50% or less. Preferably it is 0.45% or less.
- B is an element that contributes to improving hardenability. If it is less than 0.0004%, the effect of addition cannot be obtained, so B is preferably made 0.0004% or more. More preferably, it is 0.0010% or more. On the other hand, if it exceeds 0.01%, a coarse B compound is produced and the cold formability deteriorates, so B is made 0.01% or less. Preferably it is 0.008% or less.
- Nb is an element effective for controlling the form of carbides, and is an element that contributes to improving ductility by refining the structure. If it is less than 0.001%, the effect of addition cannot be obtained, so Nb is preferably 0.001% or more. More preferably, it is 0.002% or more. On the other hand, if it exceeds 0.10%, a large number of fine Nb carbides are generated, the strength is excessively increased, the number of carbides at the ferrite grain boundaries is decreased, and the cold formability is decreased. 10% or less. Preferably it is 0.09% or less.
- V 0.10% or less
- Nb is an element that is effective in controlling the morphology of carbides, and is an element that contributes to improving ductility by refining the structure. If it is less than 0.001%, the effect of addition cannot be obtained, so V is preferably 0.001% or more. More preferably, it is 0.004% or more. On the other hand, if it exceeds 0.10%, a lot of fine V carbides are generated, the strength is excessively increased, the number of carbides at the ferrite grain boundaries is decreased, and the cold formability is decreased. 10% or less. Preferably it is 0.09% or less.
- Cu is an element that segregates at the ferrite grain boundary, and is an element that contributes to improvement in strength by forming fine precipitates. If it is less than 0.001%, the effect of improving the strength cannot be obtained, so Cu is preferably made 0.001% or more. More preferably, it is 0.004% or more. On the other hand, if it exceeds 0.10%, segregation to the ferrite grain boundary causes red heat embrittlement, and the productivity in hot rolling decreases, so it is made 0.10% or less. Preferably it is 0.09% or less.
- W is an element effective for controlling the form of carbide. If less than 0.001%, the effect of addition cannot be obtained, so W is preferably 0.001% or more. More preferably, it is 0.003% or more. On the other hand, if it exceeds 0.10%, a large number of fine W carbides are formed and the strength is excessively increased, and the number of carbides at the ferrite grain boundaries is reduced and the cold formability is lowered. 10% or less. Preferably it is 0.08% or less.
- Ta 0.10% or less
- Nb, V, and W is an element effective for controlling the morphology of carbides. If less than 0.001%, the effect of addition cannot be obtained, so Ta is preferably 0.001% or more. More preferably, it is 0.007% or more. On the other hand, if it exceeds 0.10%, a large number of fine Ta carbides are produced, the strength is excessively increased, the number of carbides at the ferrite grain boundaries is reduced, and the cold formability is lowered. 10% or less. Preferably, it is 0.09% or less.
- Ni is an element effective for improving ductility. If it is less than 0.001%, the effect of addition cannot be obtained, so Ni is preferably made 0.001% or more. More preferably, it is 0.002% or more. On the other hand, if it exceeds 0.10%, the number of carbides at the ferrite grain boundary decreases and the cold formability deteriorates, so Ni is made 0.10% or less. Preferably it is 0.09% or less.
- Sn is an element inevitably mixed from the steel raw material. Therefore, Sn is preferably as small as possible, and may be 0%. However, if it is reduced to less than 0.001%, the refining cost is greatly increased, so Sn may be 0.001% or more. The Sn content may be 0.002% or more. On the other hand, if it exceeds 0.05%, the ferrite becomes brittle and the cold formability deteriorates, so Sn is made 0.05% or less. Preferably, it is 0.04% or less.
- Sb 0.05% or less
- Sb is an element that is inevitably mixed from the steel raw material, segregates at the ferrite grain boundary, and reduces the number of carbides at the ferrite grain boundary. Therefore, Sb is preferably as small as possible, and may be 0%. However, if it is reduced to less than 0.001%, the refining cost increases significantly, so Sb may be 0.001% or more. The Sb content may be 0.002% or more. On the other hand, if it exceeds 0.05%, Sb segregates at the ferrite grain boundary, the number of carbides at the ferrite grain boundary decreases, and the cold formability deteriorates, so Sb is made 0.05% or less. Preferably it is 0.04% or less.
- Mg is an element that can control the form of sulfide by addition of a small amount. If it is less than 0.0001%, the effect of addition cannot be obtained, so Mg is preferably 0.0001% or more. More preferably, it is 0.0008% or more. On the other hand, if it exceeds 0.05%, ferrite becomes brittle and cold formability deteriorates, so Mg is made 0.05% or less. Preferably it is 0.04% or less.
- Ca is an element that can control the form of sulfide with a small amount of addition. If it is less than 0.001%, the effect of addition cannot be obtained, so Ca is preferably made 0.001% or more. More preferably, it is 0.003% or more. On the other hand, if it exceeds 0.05%, coarse Ca oxide is generated and becomes a starting point of cracking during cold forming, so Ca is made 0.05% or less. Preferably it is 0.04% or less.
- Y like Mg and Ca, is an element that can control the form of sulfide by addition of a trace amount. If it is less than 0.001%, the effect of addition cannot be obtained, so Y is preferably 0.001% or more. More preferably, it is 0.003% or more. On the other hand, if it exceeds 0.05%, coarse Y oxide is generated and becomes a starting point of cracking during cold forming, so Y is set to 0.05% or less. Preferably it is 0.03% or less.
- Zr 0.05% or less
- Zr is an element that can control the form of sulfide by adding a small amount. If it is less than 0.001%, the effect of addition cannot be obtained, so Zr is preferably 0.001% or more. More preferably, it is 0.004% or more. On the other hand, if it exceeds 0.05%, coarse Zr oxide is generated and becomes a starting point of cracking during cold forming, so Zr is made 0.05% or less. Preferably it is 0.04% or less.
- La is an element that can control the form of sulfide by adding a small amount, but is also an element that segregates at the ferrite grain boundary and reduces the number of carbides at the ferrite grain boundary. If it is less than 0.001%, the effect of controlling the form of sulfide cannot be obtained, so La is preferably 0.001% or more. More preferably, it is 0.003% or more. On the other hand, if it exceeds 0.05%, it segregates at the ferrite grain boundary, the number of carbides at the ferrite grain boundary decreases, and the cold formability deteriorates, so La is made 0.05% or less. Preferably it is 0.04% or less.
- Ce is an element that can control the form of sulfide by addition of a small amount, but is also an element that segregates at the ferrite grain boundary and reduces the number of carbides at the ferrite grain boundary. If it is less than 0.001%, the effect of controlling the form of sulfide cannot be obtained, so Ce is preferably 0.001% or more. More preferably, it is 0.003% or more. On the other hand, if it exceeds 0.05%, it segregates at the ferrite grain boundary, the number of carbides at the ferrite grain boundary decreases, and the cold formability deteriorates, so Ce is made 0.05% or less. Preferably it is 0.04% or less.
- the balance of the above component composition is Fe and inevitable impurities.
- the ratio (B / A) of the number of carbides (B) in the ferrite grain boundary to the number of carbides (A) in the ferrite grains exceeds 1, and (b ) Ferrite particle size is 5 ⁇ m or more and 50 ⁇ m or less, (c) carbide average particle size is 0.4 ⁇ m or more and 2.0 ⁇ m or less, (d) pearlite area ratio is 6% or less, (e) Vickers hardness
- the characteristic requirement is that the length is 120 HV or more and 170 HV or less.
- the steel sheet of the present invention can have excellent cold formability and post-heat treatment ductility by providing the above-mentioned component composition and the characteristic requirements of the above (a) to (e). This is a new finding found by the present inventors. This will be described below.
- the structure of the steel sheet of the present invention is substantially a structure composed of ferrite and carbide.
- the ratio (B / A) of the number of carbides (B) in the ferrite grain boundary to the number of carbides (A) in the ferrite grains (B / A) exceeds 1.
- the carbide is a compound obtained by substituting Fe atoms in the cementite with an alloy element such as Mn or Cr, or an alloy carbide (M 23 C 6 , M 6 C, MC, etc. [M: Fe and other metal elements added as alloys]).
- a shear band is formed in the macro structure of the steel sheet, and slip deformation is concentrated near the shear band. Slip deformation is accompanied by dislocation growth, and a region having a high dislocation density is formed in the vicinity of the shear band. As the amount of strain applied to the steel sheet increases, slip deformation is promoted and the dislocation density increases. In order to improve the cold formability, it is effective to suppress the formation of shear bands.
- a shear band is understood as a phenomenon in which a slip generated in a certain crystal grain overcomes the grain boundary and continuously propagates to adjacent crystal grains. Therefore, in order to suppress the formation of shear bands, it is necessary to prevent the propagation of slip across the grain boundary.
- Carbides in the steel sheet are strong particles that prevent slipping, and by allowing the carbides to exist at the ferrite grain boundaries, it is possible to prevent the propagation of slips across the crystal grain boundaries and suppress the formation of shear bands. It becomes possible to improve cold formability.
- the present inventors did not adopt the above observation method as a general analysis method, and searched for a simpler and more accurate evaluation index. As a result, if the ratio (B / A) of the number of carbides (B) in the ferrite grain boundary to the number of carbides (A) in the ferrite grains is used as an index, the cold formability can be quantitatively evaluated, and It has been found that when the ratio (B / A) exceeds 1, the cold formability is remarkably improved.
- Any of buckling, folding, and folding that occurs during cold forming of a steel sheet is caused by the localization of strain associated with the formation of a shear band. Formation and strain localization are mitigated, and buckling, folding, and folding are suppressed.
- the cold formability can be improved by setting the ferrite grain size to 5 ⁇ m or more. If the ferrite particle size is less than 5 ⁇ m, the hardness increases and cracks and cracks are likely to occur during cold forming, so the ferrite particle size is set to 5 ⁇ m or more. Preferably it is 7 micrometers or more. On the other hand, if the ferrite grain size exceeds 50 ⁇ m, the number of carbides at the grain boundaries that suppress the propagation of slip is reduced and the cold formability is lowered, so the ferrite grain size is set to 50 ⁇ m or less. Preferably it is 38 micrometers or less.
- the average particle size of the carbide contained in the structure of the steel sheet of the present invention is less than 0.4 ⁇ m, the hardness of the steel plate is remarkably increased and the cold formability is lowered. 4 ⁇ m or more. Preferably it is 0.6 micrometer or more.
- the average particle diameter of the carbide contained in the structure of the steel sheet of the present invention exceeds 2.0 ⁇ m, the carbide becomes the starting point of cracking during cold forming, so the average particle diameter of the carbide is 2.0 ⁇ m or less. . Preferably it is 1.95 ⁇ m or less.
- the pearlite area ratio exceeds 6%, the hardness of the steel sheet is remarkably increased and the cold formability is lowered. Therefore, the pearlite area ratio is set to 6% or less. Preferably it is 5% or less.
- the cold formability can be improved by setting the Vickers hardness of the steel sheet to 120 HV or more and 170 HV or less. If the Vickers hardness is less than 120 HV, buckling is likely to occur during cold forming, so the Vickers hardness is 120 HV or more. Preferably it is 130HV or more. On the other hand, if the Vickers hardness exceeds 170 HV, the ductility is lowered and internal cracking is likely to occur during cold forming, so the Vickers hardness is set to 170 HV or less. Preferably it is 160HV or less.
- Carbide is observed with a scanning electron microscope. Prior to observation, a sample for tissue observation was wet-polished with emery paper and polished with diamond abrasive grains having an average particle size of 1 ⁇ m, and the observation surface was finished to a mirror surface, and the tissue was then washed with a 3% nitric acid-alcohol solution. Etch.
- the magnification for observation is selected from among magnifications of 3000 times so that the structure of ferrite and carbide can be distinguished.
- a plurality of fields of view of 30 ⁇ m ⁇ 40 ⁇ m in the 1/4 layer thickness are randomly photographed at the selected magnification. For example, eight or more areas that do not overlap each other are photographed.
- carbonized_material is measured.
- the area of the carbide included in the analysis region may be measured in detail using image analysis software (for example, Win ROOF manufactured by Mitani Corporation).
- image analysis software for example, Win ROOF manufactured by Mitani Corporation.
- carbides having an area of 0.01 ⁇ m 2 or less are excluded from evaluation targets.
- the number of carbides present in the ferrite grain boundary is counted using the above-described structure image, and the number of carbides in the ferrite grain boundary is subtracted from the total number of carbides to calculate the number of carbides in the ferrite grain. Based on the counted and calculated number of carbides, the ratio (B / A) of the number of carbides (B) in the ferrite grain boundaries to the number of carbides (A) in the ferrite grains is calculated. Carbides having an area of 0.01 ⁇ m 2 or less are not counted.
- the ferrite grain size was determined by polishing the observation surface of the sample to a mirror surface and etching with a 3% nitric acid-alcohol solution, and observing the etched structure with an optical microscope or scanning electron microscope. Can be measured by applying the line segment method.
- the production method of the present invention is characterized by consistently managing the conditions of the hot rolling process, the condition of the scraping process, and the condition of the two-stage annealing process to control the structure of the steel sheet.
- a steel piece obtained by continuously casting molten steel having the required composition is directly or after cooling and heated to hot rolling, and finishes the hot rolling in the temperature range of 800 ° C to 900 ° C. To do.
- a steel sheet structure composed of fine pearlite and bainite can be obtained.
- the hot rolled steel sheet that has been subjected to the finish rolling is scraped off in a temperature range of 400 ° C. or higher and 550 ° C. or lower.
- the hot-rolled steel sheet that has been scraped off is discharged, pickled, and then subjected to two-stage annealing. After annealing, the steel sheet is cooled to 650 ° C. at a cooling rate controlled to 1 ° C./hour to 30 ° C./hour, and then to room temperature. Allow to cool.
- the hot-rolled steel sheet is held in a temperature range of 650 ° C. or more and 720 ° C. or less for 3 hours or more and 60 hours or less in the first-stage annealing step, and in the second-stage annealing step, 725 ° C. or more.
- the heating temperature is preferably 1000 ° C. or more and 1250 ° C. or less, and the heating time is preferably 0.5 hours or more and 3 hours or less.
- the steel slab temperature is preferably 1000 ° C. or higher and 1250 ° C. or lower.
- the billet temperature or billet heating temperature is preferably 1250 ° C. or less, and the billet heating time is preferably 3 hours or less. More preferably, it is 1200 degrees C or less and 2.5 hours or less.
- the billet temperature or billet heating temperature is preferably 1000 ° C. or more, and the billet heating time is preferably 0.5 hours or more. More preferably, it is 1050 ° C. or more and 1 hour or more.
- finishing temperature shall be 800 degreeC or more. Preferably it is 830 ° C or more.
- finishing temperature exceeds 900 ° C, a thick scale is generated while passing through the Run Out Table (ROT). Due to this scale, wrinkles are generated on the steel sheet surface, and cracks start from the wrinkles during cold forming. Will occur. For this reason, finishing temperature shall be 900 degrees C or less. Preferably it is 870 degrees C or less.
- the cooling rate is preferably 10 ° C./second or more and 100 ° C./second or less.
- the cooling rate is preferably 10 ° C./second or more. More preferably, it is 15 ° C./second or more.
- the cooling rate is preferably 100 ° C./second or less. More preferably, it is 90 ° C./second or less.
- the cooling rate is determined at each water injection section from the time when the hot-rolled steel sheet after finish rolling passes through the non-water injection section and is subjected to water cooling in the water injection section to the time when it is cooled on the ROT to the target temperature of scooping. It refers to the cooling capacity received from the cooling equipment, and does not indicate the average cooling rate from the water injection start point to the temperature taken by the take-up machine.
- the cutting temperature is 400 ° C. or higher and 550 ° C. or lower. If the milling temperature is less than 400 ° C., the austenite that has not been transformed before the milling is transformed into hard martensite, and when the hot-rolled steel sheet coil is discharged, cracks occur in the surface layer of the hot-rolled steel sheet, Formability is reduced.
- the scraping temperature is set to 400 ° C. or higher. Preferably it is 430 degreeC or more.
- the harvesting temperature exceeds 550 ° C, pearlite with large lamella spacing is generated, and thick needle-like carbide with high thermal stability is generated. This acicular carbide remains even after two-stage annealing.
- the cutting temperature is 550 ° C. or less. Preferably it is 520 degrees C or less.
- ⁇ ⁇ Take out the hot-rolled steel sheet coil, pickle it, and then perform two-step annealing (two-step annealing) to keep it in two temperature ranges.
- two-step annealing two-step annealing
- the hot-rolled steel sheet is not cold-rolled until the two-stage annealing step and the cooling step after the two-step annealing process are completed after the hot-rolled steel sheet coil is dispensed.
- the ferrite grains are refined and the steel sheet is difficult to soften, and the Vickers hardness of the steel sheet may not be 120 HV or more and 170 HV or less.
- the first stage annealing is performed in the temperature range below the A C1 point.
- the carbide is coarsened and the alloy elements are concentrated to increase the thermal stability of the carbide.
- the temperature is raised to a temperature range from A C1 point to A 3 point, and austenite is generated in the structure. Thereafter, it is slowly cooled to transform austenite into ferrite, and the carbon concentration in the austenite is increased.
- a temperature range of A less than point C1 the thermal stabilization of carbides is promoted, the temperature range below A C1 points or more A 3 points above
- the number of residual carbides can be increased by holding at.
- the annealing temperature in the first stage annealing is 650 ° C. or more and 720 ° C. or less. If the first stage annealing temperature is less than 650 ° C., the carbide is not sufficiently stabilized, and it becomes difficult to leave the carbide in the austenite during the second stage annealing. For this reason, the first stage annealing temperature is set to 650 ° C. or higher. Preferably it is 670 degreeC or more. On the other hand, if the first-stage annealing temperature exceeds 720 ° C., austenite is generated before the stability of the carbide is increased, and it becomes difficult to control the above-described structure change. Therefore, the first-stage annealing temperature is set to 720 ° C. or less. . Preferably it is 700 degrees C or less.
- the annealing time in the first stage annealing is 3 hours or more and 60 hours or less. If the first stage annealing time is less than 3 hours, the carbide is not sufficiently stabilized, and it is difficult to leave the carbide in the austenite during the second stage annealing. For this reason, the first stage annealing time is set to 3 hours or more. Preferably it is 5 hours or more. On the other hand, if the first stage annealing time exceeds 60 hours, the carbide cannot be further stabilized, and the productivity is further lowered. Therefore, the first stage annealing time is set to 60 hours or less. Preferably it is 55 hours or less.
- An annealing temperature (second stage annealing temperature) in the second stage annealing is set to 725 ° C. or more and 790 ° C. or less. If the second stage annealing temperature is less than 725 ° C., the amount of austenite produced is small, and the number of carbides (B) at the ferrite grain boundaries decreases. For this reason, the second stage annealing temperature is set to 725 ° C. or higher. Preferably it is 715 degrees C or less.
- the second stage annealing temperature exceeds 790 ° C., it becomes difficult to leave the carbides in the austenite and it becomes difficult to control the above-described structure change, so the second stage annealing temperature is set to 790 ° C. or less. Preferably it is 770 degrees C or less.
- the annealing time in the second stage annealing is 3 hours or more and 50 hours or less. If the second stage annealing time is less than 3 hours, the amount of austenite produced is small, and the carbides in the ferrite grains are not sufficiently dissolved, making it difficult to increase the number of carbides at the ferrite grain boundaries. For this reason, the second stage annealing time is set to 3 hours or more. Preferably it is 6 hours or more. On the other hand, if the second stage annealing time exceeds 50 hours, it becomes difficult to leave the carbide in the austenite, so the second stage annealing time is set to 50 hours or less. Preferably it is 45 hours or less.
- the steel sheet is cooled to 650 ° C. at a cooling rate controlled to 1 ° C./hour or more and 30 ° C./hour or less.
- the austenite produced by the second stage annealing is gradually cooled to transform it into ferrite, and carbon is adsorbed on the carbide remaining in the austenite.
- the cooling rate is low, if it is less than 1 ° C./hour, the time required for cooling increases and the productivity decreases, so the cooling rate is 1 ° C./hour or more. Preferably, it is 5 ° C./hour or more.
- the cooling rate exceeds 30 ° C./hour, austenite is transformed into pearlite, the hardness of the steel sheet is increased, and the cold formability is lowered. Therefore, the cooling rate is 30 ° C./hour or less. Preferably it is 26 degrees C / hour or less.
- the annealed steel sheet After the annealed steel sheet is cooled to 650 ° C. at the above cooling rate, it is cooled to room temperature.
- the cooling rate In cooling to room temperature, the cooling rate is not particularly limited.
- the first-stage annealing and the second-stage annealing may be either box annealing or continuous annealing. Box annealing may be performed using a box-type annealing furnace. Further, the atmosphere in the two-stage annealing is not particularly limited to a specific atmosphere. For example, any atmosphere of 95% or more nitrogen atmosphere, 95% or more hydrogen atmosphere, or air atmosphere may be used.
- the ferrite grain boundary substantially has the structure of ferrite and spheroidized carbide having a particle diameter of 5 ⁇ m or more and 50 ⁇ m or less, and the number of carbides (A) in the ferrite grains. It is possible to obtain a steel sheet that has a ratio (B / A) of the number of carbides (B) of greater than 1 and a Vickers hardness of 120 HV or more and 170 HV or less and excellent in cold formability and post-heat treatment ductility.
- the conditions in the examples are examples of conditions adopted for confirming the feasibility and effects of the present invention, and the present invention is based on this one example of conditions. It is not limited.
- the present invention can adopt various conditions as long as the object of the present invention is achieved without departing from the gist of the present invention.
- Example 1 In order to investigate the influence of the component composition, continuous casting casting of the component composition shown in Table 1-1, Table 1-2 (component composition of the steel plate of the present invention) and Table 2-1, Table 2-2 (component composition of the comparative steel plate)
- the pieces (steel pieces) were subjected to the steps from the hot rolling step to the two-step annealing step under the following conditions, and samples for characteristic evaluation shown in Table 3 (Invention Steels A-1 to Z-1) And comparative steels AA-1 to AZ-1).
- the steel pieces of Nos. A to Z in Table 1-1 and Table 1-2 all have the composition of the steel sheet of the present invention.
- the composition of the steel slabs of Nos. AA to AZ in Table 2-1 and Table 2-2 are all outside the range of the composition of the steel sheet of the present invention.
- each steel slab having the composition shown in Tables 1 and 2 was heated at 1240 ° C. for 1.8 hours and then subjected to hot rolling, and finish rolling was completed at a finishing temperature of 820 ° C. Thereafter, the steel sheet was cooled on the ROT at a cooling rate of 45 ° C./second, and scraped off at a scraping temperature of 510 ° C. to produce a hot-rolled steel sheet coil. Next, the hot-rolled steel sheet coil is discharged, and after pickling, the hot-rolled steel sheet coil after pickling is charged into a box-type annealing furnace to perform first-stage annealing, and 95% hydrogen and 5% nitrogen are added.
- the annealing atmosphere was controlled so that it was included, heated from room temperature to 705 ° C. and held for 36 hours, and the temperature distribution in the hot-rolled steel sheet coil was made uniform. Then, in order to perform the second stage annealing, it is heated to 760 ° C. and held for 10 hours, then cooled to 650 ° C. at a cooling rate of 10 ° C./hour, and then cooled to room temperature for furnace evaluation. A sample of was prepared.
- the structure of the sample was observed by the method described above, and the ferrite particle size and the number of carbides were measured.
- the sample was placed in an atmospheric annealing furnace, and held at 950 ° C. for 20 minutes. After holding, oil cooling at 50 ° C. was performed. Thereafter, tempering was performed so that the hardness was 400 HV.
- the ductility after heat treatment was obtained by searching the surface of the sample after annealing, preparing a JIS No. 5 test piece having a thickness of 2 mm, and conducting a tensile test at room temperature. A tensile test was performed at a test speed of 3 mm / min with a distance between the gauge points of 50 mm. 10% or more was considered good.
- Table 3 shows ferrite grain size ( ⁇ m), Vickers hardness (HV), ratio of the number of carbides in the ferrite grain boundary to the number of carbides in the ferrite grain (number of grain boundary carbides / number of carbides in grain), and heat treatment. It shows the backward ductility (%).
- the comparative steel sheet AA-1 has a large amount of Si
- the comparative steel sheet AB-1 has a large amount of C
- the comparative steel sheet AD-1 has a large amount of Mn
- the Vickers hardness is 170 HV. Is over.
- Comparative steel AH-1 Small amount of C in Comparative steel AH-1, for A 3 points higher, quenching is impossible.
- the comparative steel sheet AE-1 not only the amount of Si was small and the Vickers hardness was less than 120 HV, but also the ductility after heat treatment was lowered.
- the component composition is outside the range of the component composition of the steel plate of the present invention, so the ductility after heat treatment is reduced.
- No. A-2 to Z-2 test steel sheets were prepared as follows. That is, first, each of the steel slabs Nos. A to Z having the composition shown in Table 1-1 and Table 1-2 was heated at 1240 ° C. for 1.8 hours and then subjected to hot rolling, as shown in Table 4. The hot-rolled steel sheet coil having a thickness of 3.0 mm was completed after finishing the hot rolling and rolling at the cooling rate of 45 ° C./second on the ROT at the cooling conditions shown in Table 4. Manufactured.
- the hot-rolled steel sheet coil was pickled and then subjected to a two-step box annealing under the annealing conditions shown in Table 4.
- Material for property evaluation with a thickness of 3.0 mm is collected from the hot-rolled steel sheet after annealing, and ferrite grain boundary carbides with respect to the ferrite grain size ( ⁇ m), Vickers hardness (HV), and the number of carbides in the ferrite grains.
- the number ratio (number of grain boundary carbides / number of carbides in grains) and ductility after heat treatment (%) were measured. The results are shown in Table 5.
- the Vickers hardness is 170 HV or less, and the ratio of the number of carbides in the ferrite grain boundary to the number of carbides in the ferrite grains exceeds 1. Since hardness is an index of cold formability, it can be seen that all the steel sheets of the present invention are excellent in cold formability. Furthermore, since all the steel sheets of the present invention have a ductility after heat treatment of 10% or more, it can be understood that the steel sheet after heat treatment is good.
- the manufacturing conditions are outside the range of the manufacturing conditions of the manufacturing method of the present invention, the Vickers hardness is increased.
- the number of grain boundary carbides / number of intragranular carbides also decreases.
- this invention has a high applicability in steel plate manufacture and utilization industry.
Abstract
Description
C :0.10~0.40%、
Si:0.30~1.00%、
Mn:0.30~1.00%、
Al:0.001~0.10%、
P :0.02%以下、
S :0.01%以下
を含有し、残部がFe及び不純物からなる鋼板において、
フェライト粒内の炭化物の個数(A)に対するフェライト粒界の炭化物の個数(B)の比率(B/A)が1を超え、
フェライト粒径が5μm以上50μm以下であり、
炭化物の平均粒子径が0.4μm以上2.0μm以下であり、
パーライト面積率が6%以下であり、
ビッカース硬さが120HV以上170HV以下であることを特徴とする鋼板。
N :0.01%以下、
O :0.02%以下
の1種又は2種以上を含有することを特徴とする前記(1)に記載の鋼板。
Ti:0.10%以下、
Cr:0.50%以下、
Mo:0.50%以下、
B :0.01%以下、
Nb:0.10%以下、
V :0.10%以下、
Cu:0.10%以下、
W :0.10%以下、
Ta:0.10%以下、
Ni:0.10%以下、
Sn:0.05%以下、
Sb:0.05%以下、
As:0.05%以下、
Mg:0.05%以下、
Ca:0.05%以下、
Y :0.05%以下、
Zr:0.05%以下、
La:0.05%以下、
Ce:0.05%以下
の1種又は2種以上を含有することを特徴とする前記(1)又は(2)に記載の鋼板。
(i)前記(1)~(3)のいずれかに記載の成分組成の鋼片を、直接、又は、一旦冷却後加熱して熱間圧延に供し、800℃以上900℃以下の温度域で仕上げ圧延を完了した熱延鋼板を400℃以上550℃以下で捲き取り、
(ii)巻き取った熱延鋼板を払い出し、酸洗を施した後、650℃以上720℃以下の温度域で3時間以上60時間以下保持する1段目の焼鈍を施し、さらに、725℃以上790℃以下の温度域で3時間以上50時間以下保持する2段目の焼鈍を施す、2段ステップ型の焼鈍を施し、
(iii)上記焼鈍後の熱延鋼板を、1℃/時間以上30℃/時間以下に制御した冷却速度で650℃まで冷却し、次いで、室温まで冷却する
ことを特徴とする鋼板の製造方法。
Cは、炭化物を形成し、鋼の強化及びフェライト粒の微細化に有効な元素である。冷間成形時、鋼板表面に梨地が発生することを抑制し、冷間成形品の表面美観を確保するためには、フェライト粒の粗大化を抑制する必要がある。0.10%未満では、炭化物の体積率が不足し、焼鈍中、フェライト粒の粗大化を抑制できないので、Cは0.10%以上とする。好ましくは0.14%以上である。一方、Cが0.40%を超えると、炭化物の体積率が増加し、冷間成形性及び熱処理後延性が低下するので、Cは0.40%以下とする。好ましくは0.38%以下である。
Siは、炭化物の形態に影響を及ぼし、熱処理後の延性の向上に寄与する元素である。フェライト粒内の炭化物の個数を低減し、フェライト粒界の炭化物の個数を増大するためには、2段ステップ型の焼鈍(以下「2段焼鈍」ということがある。)により、焼鈍中にオーステナイト相を生成させ、一旦、炭化物を溶解した後、徐冷し、フェライト粒界への炭化物の析出を促進する必要がある。
Mnは、2段焼鈍において、炭化物の形態を制御する元素である。0.30%未満では、2段焼鈍後の徐冷において、フェライト粒界に、炭化物を生成させることが困難となるので、Mnは0.30%以上とする。好ましくは0.33%以上である。一方、1.00%を超えると、フェライトの硬度が増大し、冷間成形性が低下するので、Mnは1.00%以下とする。好ましくは0.96%以下である。
Alは、脱酸剤として作用するとともに、フェライトを安定化する元素である。0.001%未満では、添加による前記効果が十分に得られないので、Alは0.001%以上とする。好ましくは0.004%以上である。一方、0.10%を超えると、フェライト粒界の炭化物の個数が減少し、冷間成形性が低下するので、Alは0.10%以下とする。好ましくは0.09%以下である。
Pは、フェライト粒界に偏析し、フェライト粒界における炭化物の生成を抑制する作用をなす元素である。それ故、Pの含有量は、少ないほど好ましく、0%でも良いが、0.0001%未満に低減すると、精錬コストが大幅に増加するので、0.0001%以上としても良い。Pの含有量は0.0013%以上であっても良い。一方、Pが0.02%を超えると、フェライト粒界における炭化物の生成が抑制されて、炭化物の個数が減少し、冷間成形性が低下するので、Pは0.02%以下とする。好ましくは0.01%以下である。
Sは、MnSなどの非金属介在物を形成する元素である。非金属介在物は、冷間成形時に割れの起点となるので、Sは、少ないほど好ましく、0%でも良いが、0.0001%未満に低減すると、精錬コストが大幅に増加するので、0.0001%以上としても良い。Sの含有量は0.0012%以上としても良い。一方、0.01%を超えると、非金属介在物が生成し、冷間成形性が低下するので、Sは0.01%以下とする。好ましくは0.009%以下である。
Nは、多量に存在すると、フェライトを脆化させる元素である。それ故、Nは、少ないほど好ましく、Nの含有量は0でも良いが、0.0001%未満に低減すると、精錬コストが大幅に増加するので、0.0001%以上として良い。Nの含有量は0.0006%以上としても良い。一方、0.01%を超えると、フェライトが脆化し、冷間成形性が低下するので、Nは0.01%以下とする。好ましくは0.007%以下である。
Oは、多量に存在すると、粗大な酸化物を形成する元素である。それ故、Oは、少ないほど好ましく、0%でも良いが、0.0001%未満に低減すると、精錬コストが大幅に増加するので、0.0001%以上として良い。Oの含有量は0.0011%以上として良い。一方、0.02%を超えると、鋼中に粗大な酸化物が生成し、冷間成形時に割れの起点となるので、Oは0.02%以下とする。好ましくは0.01%以下である。
Tiは、窒化物を形成し、結晶粒の微細化に寄与する元素である。0.001%未満では、添加による効果が十分に得られないので、Tiは0.001%以上とすることが好ましい。より好ましくは0.005%以上である。一方、0.10%を超えると、粗大なTi窒化物が生成し、冷間成形性が低下するので、Tiは0.10%以下とする。好ましくは0.07%以下である。
Crは、焼入れ性の向上に寄与する一方で、炭化物に濃化して炭化物を安定化し、オーステナイト相内でも安定な炭化物を形成する元素である。0.001%未満では、焼入れ性向上効果が得られないので、Crは0.001%以上とすることが好ましい。より好ましくは0.007%以上である。一方、0.50%を超えると、オーステナイト相内で安定な炭化物が生成し、焼入れ時に炭化物の溶解が遅れ、所要の焼入れ強度が得られないので、Crは0.50%以下とする。好ましくは0.48%以下である。
Moは、Mnと同様に、炭化物の形態制御に有効な元素であり、また、組織を微細化して延性の向上に寄与する元素である。0.001%未満では、添加による効果が得られないので、Moは0.001%以上とすることが好ましい。より好ましくは0.017%以上である。一方、0.50%を超えると、r値の面内異方性が低下し、冷間成形性が低下するので、Moは0.50%以下とする。好ましくは0.45%以下である。
Bは、焼入れ性の向上に寄与する元素である。0.0004%未満では、添加による効果が得られないので、Bは0.0004%以上とすることが好ましい。より好ましくは0.0010%以上である。一方、0.01%を超えると、粗大なB化物が生成し、冷間成形性が低下するので、Bは0.01%以下とする。好ましくは0.008%以下である。
Nbは、炭化物の形態制御に有効な元素であり、また、組織を微細化して延性の向上に寄与する元素である。0.001%未満では、添加による効果が得られないので、Nbは0.001%以上とすることが好ましい。より好ましくは0.002%以上である。一方、0.10%を超えると、微細なNb炭化物が多数生成して、強度が上昇しすぎるとともに、フェライト粒界の炭化物の個数が低下し、冷間成形性が低下するので、Nbは0.10%以下とする。好ましくは0.09%以下である。
Vも、Nbと同様に、炭化物の形態制御に有効な元素であり、また、組織を微細化して延性の向上に寄与する元素である。0.001%未満では、添加による効果が得られないので、Vは0.001%以上とすることが好ましい。より好ましくは0.004%以上である。一方、0.10%を超えると、微細なV炭化物が多数生成して、強度が上昇しすぎるとともに、フェライト粒界の炭化物の個数が低下し、冷間成形性が低下するので、Vは0.10%以下とする。好ましくは0.09%以下である。
Cuは、フェライト粒界に偏析する元素であり、また、微細な析出物を形成して強度の向上に寄与する元素である。0.001%未満では、強度向上の効果が得られないので、Cuは0.001%以上とすることが好ましい。より好ましくは0.004%以上である。一方、0.10%を超えると、フェライト粒界への偏析が赤熱脆性を招き、熱間圧延での生産性が低下するので、0.10%以下とする。好ましくは0.09%以下である。
Wも、Nb、Vと同様に、炭化物の形態制御に有効な元素である。0.001%未満では、添加による効果が得られないので、Wは0.001%以上とすることが好ましい。より好ましくは0.003%以上である。一方、0.10%を超えると、微細なW炭化物が多数生成して強度が上昇しすぎるとともに、フェライト粒界の炭化物の個数が減少し、冷間成形性が低下するので、Wは0.10%以下とする。好ましくは0.08%以下である。
Taも、Nb、V、Wと同様に、炭化物の形態制御に有効な元素である。0.001%未満では、添加による効果が得られないので、Taは0.001%以上とすることが好ましい。より好ましくは0.007%以上である。一方、0.10%を超えると、微細なTa炭化物が多数生成し、強度が上昇しすぎるとともに、フェライト粒界の炭化物の個数が減少し、冷間成形性が低下するので、Taは0.10%以下とする。好ましくは、0.09%以下である。
Niは、延性の向上に有効な元素である。0.001%未満では、添加による効果が得られないので、Niは0.001%以上とすることが好ましい。より好ましくは0.002%以上である。一方、0.10%を超えると、フェライト粒界の炭化物の個数が減少し、冷間成形性が低下するので、Niは0.10%以下とする。好ましくは0.09%以下である。
Snは、鋼原料から不可避的に混入する元素である。それ故、Snは、少ないほど好ましいので、0%であっても良いが、0.001%未満に低減すると、精錬コストが大幅に増加するので、Snは0.001%以上としても良い。Snの含有量は、0.002%以上としても良い。一方、0.05%を超えると、フェライトが脆化して、冷間成形性が低下するので、Snは0.05%以下とする。好ましくは、0.04%以下である。
Sbは、Snと同様に、鋼原料から不可避的に混入して、フェライト粒界に偏析し、フェライト粒界の炭化物の個数を低減する元素である。それ故、Sbは、少ないほど好ましいので、0%であっても良い。但し、0.001%未満に低減すると、精錬コストが大幅に増加するので、Sbは0.001%以上としても良い。Sbの含有量は0.002%以上としても良い。一方、0.05%を超えると、Sbがフェライト粒界に偏析し、フェライト粒界の炭化物の個数が減少し、冷間成形性が低下するので、Sbは0.05%以下とする。好ましくは0.04%以下である。
Asは、Sn、Sbと同様に、鋼原料から不可避的に混入し、フェライト粒界に偏析する元素である。それ故、Asは、少ないほど好ましいので、0%であっても良い。但し、0.001%未満に低減すると、精錬コストが大幅に増加するので、Asは0.001%以上としても良い。好ましくは0.002%以上としても良い。一方、0.05%を超えると、Asがフェライト粒界に偏析し、フェライト粒界の炭化物の個数が減少し、冷間成形性が低下するので、Asは0.05%以下とする。好ましくは0.04%以下である。
Mgは、微量の添加で硫化物の形態を制御できる元素である。0.0001%未満では、添加による効果が得られないので、Mgは0.0001%以上とすることが好ましい。より好ましくは0.0008%以上である。一方、0.05%を超えると、フェライトが脆化し、冷間成形性が低下するので、Mgは0.05%以下とする。好ましくは0.04%以下である。
Caは、Mgと同様に、微量の添加で硫化物の形態を制御できる元素である。0.001%未満では、添加による効果が得られないので、Caは0.001%以上とすることが好ましい。より好ましくは0.003%以上である。一方、0.05%を超えると、粗大なCa酸化物が生成し、冷間成形時に割れの起点となるので、Caは0.05%以下とする。好ましくは0.04%以下である。
Yは、Mg、Caと同様に、微量の添加で硫化物の形態を制御できる元素である。0.001%未満では、添加による効果が得られないので、Yは0.001%以上とすることが好ましい。より好ましくは0.003%以上である。一方、0.05%を超えると、粗大なY酸化物が生成し、冷間成形時に割れの起点となるので、Yは0.05%以下とする。好ましくは0.03%以下である。
Zrは、Mg、Ca、Yと同様に、微量の添加で硫化物の形態を制御できる元素である。0.001%未満では、添加による効果が得られないので、Zrは0.001%以上とすることが好ましい。より好ましくは0.004%以上である。一方、0.05%を超えると、粗大なZr酸化物が生成し、冷間成形時に割れの起点となるので、Zrは0.05%以下とする。好ましくは0.04%以下である。
Laは、微量の添加で硫化物の形態を制御できる元素であるが、フェライト粒界に偏析し、フェライト粒界の炭化物の個数を低減する元素でもある。0.001%未満では、硫化物の形態制御効果が得られないので、Laは0.001%以上とすることが好ましい。より好ましくは0.003%以上である。一方、0.05%を超えると、フェライト粒界に偏析し、フェライト粒界の炭化物の個数が減少し、冷間成形性が低下するので、Laは0.05%以下とする。好ましくは0.04%以下である。
Ceは、Laと同様に、微量の添加で硫化物の形態を制御できる元素であるが、フェライト粒界に偏析し、フェライト粒界の炭化物の個数を低減する元素でもある。0.001%未満では、硫化物の形態制御効果が得られないので、Ceは0.001%以上とすることが好ましい。より好ましくは0.003%以上である。一方、0.05%を超えると、フェライト粒界に偏析し、フェライト粒界の炭化物の個数が減少し、冷間成形性が低下するので、Ceは0.05%以下とする。好ましくは0.04%以下である。
本発明鋼板の組織は、実質的に、フェライトと炭化物で構成される組織である。そして、フェライト粒内の炭化物の個数(A)に対するフェライト粒界の炭化物の個数(B)の比率(B/A)が1を超える組織とする。
焼鈍後の鋼板組織において、フェライト粒径を5μm以上とすることで、冷間成形性を改善することができる。フェライト粒径が5μm未満であると、硬さが増加して、冷間成形時に亀裂やクラックが発生し易くなるので、フェライト粒径は5μm以上とする。好ましくは7μm以上である。一方、フェライト粒径が50μmを超えると、すべりの伝播を抑制する結晶粒界の炭化物の個数が減少し、冷間成形性が低下するので、フェライト粒径は50μm以下とする。好ましくは38μm以下である。
本発明鋼板の組織に含有される炭化物の平均粒子径が0.4μm未満であると、鋼板の硬さが著しく増加し、冷間成形性が低下するので、前記炭化物の平均粒子径は0.4μm以上とする。好ましくは0.6μm以上である。一方、本発明鋼板の組織に含有される炭化物の平均粒子径が2.0μmを超えると、冷間成形時に炭化物が亀裂の起点となるので、前記炭化物の平均粒子径は2.0μm以下とする。好ましくは1.95μm以下である。
パーライト面積率が6%を超えると、鋼板の硬さが著しく増加し、冷間成形性が低下するので、パーライト面積率は6%以下とする。好ましくは5%以下である。
鋼板のビッカース硬さを120HV以上170HV以下とすることで、冷間成形性を向上させることができる。ビッカース硬さが120HV未満であると、冷間成形時に座屈が発生し易くなるので、ビッカース硬さは120HV以上とする。好ましくは130HV以上である。一方、ビッカース硬さが170HVを超えると、延性が低下し、冷間成形時に内部割れが起き易くなるので、ビッカース硬さは170HV以下とする。好ましくは160HV以下である。
鋼片を一旦冷却後加熱して熱間圧延に供する場合、加熱温度は1000℃以上1250℃以下が好ましく、加熱時間は0.5時間以上3時間以下が好ましい。鋼片を、直接、熱間圧延に供する場合、鋼片温度は1000℃以上1250℃以下が好ましい。
熱間圧延の仕上げ圧延は、800℃以上900℃以下の温度域で完了する。仕上げ温度が800℃未満であると、鋼板の変形抵抗が増加して、圧延負荷が著しく上昇し、また、ロール磨耗量が増大して、生産性が低下する。そのため、本発明において仕上げ温度は800℃以上とする。好ましくは830℃以上である。
仕上げ圧延後の熱延鋼板をROTで冷却する際、冷却速度は10℃/秒以上100℃/秒以下が好ましい。冷却速度が10℃/秒未満であると、冷却途中に分厚いスケールが生成し、それに起因する疵の発生を抑制できないので、冷却速度は10℃/秒以上が好ましい。より好ましくは15℃/秒以上である。
捲取温度は400℃以上550℃以下とする。捲取温度が400℃未満であると、捲取り前に未変態であったオーステナイトが硬いマルテンサイトに変態し、熱延鋼板コイルの払い出し時に、熱延鋼板の表層にクラックが発生し、冷間成形性が低下する。上記変態を抑制するため、捲取温度は400℃以上とする。好ましくは430℃以上である。
1段目の焼鈍は、AC1点以下の温度域で行なう。この焼鈍により、炭化物を粗大化させるとともに、合金元素を濃化させ、炭化物の熱的安定性を高める。その後、AC1点以上A3点以下の温度域に昇温し、オーステナイトを組織中に生成させる。その後、徐冷して、オーステナイトをフェライトに変態させ、オーステナイト中の炭素濃度を高める。
2段目の焼鈍における焼鈍温度(2段目焼鈍温度)は725℃以上790℃以下とする。2段目焼鈍温度が725℃未満であると、オーステナイトの生成量が少なく、フェライト粒界における炭化物の個数(B)が低下する。このため、2段目焼鈍温度は725℃以上とする。好ましくは715℃以下である。一方、2段目焼鈍温度が790℃を超えると、炭化物をオーステナイトに残存させることが困難となり、前述の組織変化の制御が難しくなるので、2段目焼鈍温度は790℃以下とする。好ましくは770℃以下である。
成分組成の影響を調べるため、表1-1、表1-2(本発明鋼板の成分組成)及び表2-1、表2-2(比較鋼板の成分組成)に示す成分組成の連続鋳造鋳片(鋼片)に対して、以下の条件で熱間圧延工程から2段焼鈍工程までの工程を実施して、表3に示される特性評価用の試料(発明鋼A-1~Z-1及び比較鋼AA-1~AZ-1)を作製した。尚、表1-1、表1-2のNo.A~Zの鋼片は、いずれも本発明鋼板の成分組成を有して。一方、表2-1、表2-2のNo.AA~AZの鋼片の成分組成は、いずれも本発明鋼板の成分組成の範囲外である。
熱間圧延の仕上げ圧延、鋼板の捲取工程及び2段焼鈍工程のそれぞれの条件の影響を調べるため、以下のようにNo.A-2~Z-2の試験用鋼板を作製した。すなわち、まず、表1-1及び表1-2に示す成分組成の鋼片No.A~Zのそれぞれを、1240℃で1.8時間加熱した後、熱間圧延に供し、表4に示す条件で、熱間圧延の仕上げ圧延を完了し、その後、ROT上で45℃/秒の冷却速度で冷却し、表4に示す捲取温度で捲き取り、板厚3.0mmの熱延鋼板コイルを製造した。
Claims (5)
- 成分組成が、質量%で、
C :0.10~0.40%、
Si:0.30~1.00%、
Mn:0.30~1.00%、
Al:0.001~0.10%、
P :0.02%以下、
S :0.01%以下
を含有し、残部がFe及び不純物からなる鋼板において、
フェライト粒内の炭化物の個数(A)に対するフェライト粒界の炭化物の個数(B)の比率(B/A)が1を超え、
フェライト粒径が5μm以上50μm以下であり、
炭化物の平均粒子径が0.4μm以上2.0μm以下であり、
パーライト面積率が6%以下であり、
ビッカース硬さが120HV以上170HV以下であることを特徴とする鋼板。 - 前記鋼板が、さらに、質量%で、
N :0.01%以下、
O :0.02%以下
の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に記載の鋼板。 - 前記鋼板が、さらに、質量%で、
Ti:0.10%、
Cr:0.50%、
Mo:0.50%、
B :0.01%、
Nb:0.10%、
V :0.10%、
Cu:0.10%、
W :0.10%、
Ta:0.10%、
Ni:0.10%、
Sn:0.05%、
Sb:0.05%、
As:0.05%、
Mg:0.05%、
Ca:0.05%、
Y :0.05%、
Zr:0.05%、
La:0.05%、
Ce:0.05%
の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又は2に記載の鋼板。 - 請求項1乃至3のいずれか1項に記載の鋼板を製造する製造方法であって、
(i)請求項1乃至3のいずれか1項に記載の成分組成の鋼片を、直接、又は、一旦冷却後加熱して熱間圧延に供し、800℃以上900℃以下の温度域で仕上げ圧延を完了した熱延鋼板を400℃以上550℃以下で捲き取り、
(ii)巻き取った熱延鋼板を払い出し、酸洗を施した後、650℃以上720℃以下の温度域で3時間以上60時間以下保持する1段目の焼鈍を施し、さらに、725℃以上790℃以下の温度域で3時間以上50時間以下保持する2段目の焼鈍を施す、2段ステップ型の焼鈍を施し、
(iii)上記焼鈍後の熱延鋼板を、1℃/時間以上30℃/時間以下に制御した冷却速度で650℃まで冷却し、次いで、室温まで冷却する
ことを特徴とする鋼板の製造方法。 - 前記熱間圧延に供する鋼片の温度が1000~1250℃であることを特徴とする請求項4に記載の鋼板の製造方法。
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Publication number | Publication date |
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CN107614728B (zh) | 2020-04-21 |
EP3305931A4 (en) | 2018-12-12 |
PL3305931T3 (pl) | 2020-06-01 |
ES2769275T3 (es) | 2020-06-25 |
US10837077B2 (en) | 2020-11-17 |
US20180127848A1 (en) | 2018-05-10 |
KR101988153B1 (ko) | 2019-06-12 |
TWI605133B (zh) | 2017-11-11 |
KR20170138509A (ko) | 2017-12-15 |
MX2017015085A (es) | 2018-05-07 |
TW201708558A (zh) | 2017-03-01 |
CN107614728A (zh) | 2018-01-19 |
JPWO2016190397A1 (ja) | 2017-06-15 |
JP6160783B2 (ja) | 2017-07-12 |
EP3305931A1 (en) | 2018-04-11 |
EP3305931B1 (en) | 2019-12-11 |
WO2016190397A9 (ja) | 2017-08-10 |
BR112017025030A2 (ja) | 2018-08-07 |
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