WO2014141632A1 - 多層溶接継手ctod特性に優れた厚鋼板およびその製造方法 - Google Patents
多層溶接継手ctod特性に優れた厚鋼板およびその製造方法 Download PDFInfo
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- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/50—Ferrous alloys, e.g. steel alloys containing chromium with nickel with titanium or zirconium
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- C21D6/001—Heat treatment of ferrous alloys containing Ni
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- 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
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- C21D6/008—Heat treatment of ferrous alloys containing Si
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- 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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- 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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- 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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- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
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- 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
- C22C38/005—Ferrous alloys, e.g. steel alloys containing rare earths, i.e. Sc, Y, Lanthanides
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- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
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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
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- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/08—Ferrous alloys, e.g. steel alloys containing nickel
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- C—CHEMISTRY; METALLURGY
- 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
- C22C38/12—Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
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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
- C22C38/14—Ferrous alloys, e.g. steel alloys containing titanium or zirconium
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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- C22C38/16—Ferrous alloys, e.g. steel alloys containing copper
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- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
Definitions
- the present invention relates to a steel plate used for ships, offshore structures, line pipes, pressure vessels and the like, and is not only excellent in low-temperature toughness of a base material but also in a multi-layer welded joint with low to medium heat input and excellent in CTOD characteristics, and its It relates to a manufacturing method.
- Charpy test has been mainly used as an evaluation standard for toughness of steel.
- a crack opening displacement test Cracking Opening Displacement Test, hereinafter referred to as CTOD test
- CTOD test Cracking Opening Displacement Test
- This test evaluates the resistance to brittle fracture by performing a bending test at low temperature on a specimen with fatigue cracks introduced in the toughness evaluation section, and measuring the crack opening (plastic deformation) just before fracture. It is.
- multilayer welding HAZ weld heat affected zone of multilayer welding
- CGHAZ Coarse Grain Heat Affected Zone
- MA Martensite-Austenite Constituent
- the ICCGHAZ structure is included in the evaluation region in which fatigue precrack is introduced when multilayer welding HAZ is used.
- the joint CTOD characteristic obtained by the joint CTOD test is very small, it is governed by the toughness of the region that becomes the most brittle in the evaluation region. It also reflects the toughness of the tissue. For this reason, improvement of the toughness of the ICCGHAZ structure is also necessary for improving the joint CTOD characteristics of the multilayer welded HAZ.
- austenite grain growth suppression by dispersion of REM oxysulfide produced by adding REM austenite grain growth inhibition by dispersion of Ca oxysulfide produced by adding Ca, ferrite BN Techniques that combine productivity and oxide dispersion have also been used.
- Patent Literature 1 and Patent Literature 2 propose a technique for suppressing the coarsening of the austenite structure of HAZ using REM and TiN particles.
- Patent Document 3 proposes a HAZ toughness improving technique using CaS and a base metal toughness improving technique by hot rolling.
- Patent Document 4 proposes a technique that suppresses the formation of MA by reducing C and Si and further increases the strength of the base material by adding Cu.
- Patent Document 5 proposes a technique that uses BN as a ferrite transformation nucleus in a high heat input welding heat-affected zone, refines the HAZ structure, and improves the HAZ toughness.
- CTOD specification temperature of a standard for example, API standard RP-2Z
- API standard RP-2Z the CTOD specification temperature of a standard (for example, API standard RP-2Z) that prescribes joint CTOD characteristics
- CTOD specification temperature the CTOD specification temperature which API specification establishes
- these techniques have not been able to sufficiently satisfy the joint CTOD characteristics required for multi-layer welded joints for low-temperature specifications that have been demanded in recent years.
- REM oxysulfides and Ca oxysulfides are effective in suppressing austenite grain growth.
- the joint CTOD characteristic at the low temperature specification temperature cannot be satisfied only by the effect of improving the toughness by suppressing the austenite grain coarsening of HAZ.
- the ferrite nucleation ability of BN was effective in the case of a structure in which the cooling rate of the weld heat affected zone is slow in high heat input welding and HAZ is mainly composed of ferrite.
- HAZ structure is mainly bainite, and the effect cannot be obtained.
- Patent Document 3 the joint CTOD characteristic at the normal specification temperature ( ⁇ 10 ° C.) is satisfied.
- the joint CTOD characteristic at the low temperature specification temperature has not been studied.
- Patent Document 5 is effective in the case of a structure in which the cooling rate of the weld heat affected zone is slow and HAZ is mainly composed of ferrite, such as large heat input welding.
- HAZ is mainly composed of ferrite, such as large heat input welding.
- the amount of alloy components contained in the base metal is relatively high, and multilayer welding has a relatively small amount of heat input, so the HAZ structure is mainly bainite, and the effect cannot be obtained.
- an object of the present invention is to provide a thick steel plate having excellent multilayer weld joint CTOD characteristics and a method for producing the same.
- ACR (Ca ⁇ (0.18 + 130 ⁇ Ca) ⁇ O) / (1.25 ⁇ S) (2) Since the inclusion form is a composite inclusion composed of a sulfide containing Ca and Mn and an oxide containing Al, austenite can exist stably even in a region where the temperature is raised to a high temperature near the weld line. The effect of grain coarsening can be sufficiently exhibited. Further, since a Mn dilute layer is formed around the composite inclusion, it has a nucleation effect of bainite or acicular ferrite. (3) Nucleation sites during cooling of HAZ are mainly austenite grain boundaries.
- the presence of the above complex inclusions having a nucleation effect in the austenite grains nucleation starts from within the austenite grains in addition to the austenite grain boundaries, the HAZ structure finally obtained becomes fine, HAZ toughness and joint CTOD characteristics are improved.
- the nucleation effect of bainite, acicular ferrite, and ferrite by the composite inclusion is insufficient if the inclusion size is too small, and a circle equivalent diameter of 0.1 ⁇ m or more is required.
- the austenite grain size near the weld line is about 200 ⁇ m, so the density of inclusions needs to be 25 / mm 2 or more.
- the composite inclusions themselves have low toughness the HAZ toughness is rather lowered with an excessive amount of inclusions.
- inclusions tend to accumulate at 1/4 t (t: plate thickness) position by floating the unsolidified part in the slab due to the density difference between the inclusions and steel. It is necessary to prevent the number of objects from becoming excessive.
- the reduction ratio / pass is 5% or more.
- a large reduction per pass such as a cumulative reduction rate of 35% or more, the strain applied to the center of the plate thickness is increased, and the coarse inclusions are stretched and further divided to increase the density of fine inclusions.
- the present inventors have determined the transformation region / untransformed region of the base material during welding, which is required by BS standard EN10225 (2009) and API standard Recommended Practice 2Z (2005) in which joint CTOD test methods are defined.
- “multi-layer welded joint CTOD characteristics are excellent” means that the crack opening displacement is 0.4 mm or more at the test temperature of ⁇ 40 ° C. in each of the notch position bond and SC / ICHAZ.
- the present invention has been made based on the obtained knowledge and further studies, that is, the present invention, 1.
- the component composition is C: 0.03 to 0.10%, Si: 0.5% or less, Mn: 1.0 to 2.0%, P: 0.015% or less, S: 0.005% by mass.
- the effective crystal grain size of the base material at the center is 20 ⁇ m or less, and the equivalent circle diameter of 0 and 1/2 of the plate thickness (t: mm) is made of a sulfide containing Ca and Mn and an oxide containing Al. thick steel composite inclusions or .1 ⁇ m and excellent multilayer welded joint CTOD characteristics that exist 2 25-250 particles / mm .
- the thick steel plate having excellent CTOD characteristics according to 1 above, comprising one or more of 0.0060%.
- the steel slab having the component composition described in 3.1 or 2 is heated to 950 ° C. or more and 1200 ° C. or less, and the rolling reduction rate at a plate thickness center temperature of 950 ° C. or more / pass is 8% or more, and the cumulative rolling reduction rate is 30% or more.
- the cumulative reduction rate is 40% or more when the sheet thickness center temperature is less than 950 ° C.
- cooling is performed so that the average cooling rate between 700 and 500 ° C. at the sheet thickness center is 1 to 50 ° C./sec.
- the steel slab having the component composition described in 4.1 or 2 is heated to 950 ° C. or more and 1200 ° C. or less, and the rolling reduction ratio / pass when the sheet thickness center temperature is 950 ° C. or more is 5% or more is 35% or more.
- cooling is performed so that the average cooling rate between 700 and 500 ° C. at the sheet thickness center is 1 to 50 ° C./sec.
- C 0.03-0.10% C is an element that improves the strength of steel, and needs to be contained by 0.03% or more. However, if C exceeds 0.10% and excessively contains C, the joint CTOD characteristics deteriorate. Therefore, C is limited to the range of 0.03 to 0.10%. It is preferably 0.04 to 0.08%.
- Si 0.5% or less
- the joint CTOD characteristics deteriorate.
- Si was limited to the range of 0.5% or less.
- it is 0.4% or less, More preferably, it exceeds 0.1% and is 0.3% or less.
- Mn 1.0 to 2.0% Mn is an element that improves the strength through improving the hardenability of steel. However, when added in excess, the joint CTOD characteristics are significantly reduced. Therefore, Mn is limited to the range of 1.0 to 2.0%. The preferred range is 1.2 to 1.8%.
- P 0.015% or less
- P is an element that is inevitably contained in steel as an impurity, and is desirably reduced as much as possible in order to reduce the toughness of the steel.
- the content exceeds 0.015%, the joint CTOD characteristics are remarkably deteriorated, so the content is limited to 0.015% or less. Preferably it is 0.010% or less.
- S 0.0005 to 0.0050% S is an element necessary for inclusions for improving the toughness of the multilayer welded HAZ, and should be contained in an amount of 0.0005% or more. However, if the content exceeds 0.0050%, the joint CTOD characteristics are deteriorated, so the content is limited to 0.0050% or less. Preferably it is 0.0045% or less.
- Al 0.005 to 0.060%
- Al is an element necessary for inclusions for improving the toughness of the multilayer welded HAZ, and it is necessary to contain 0.005% or more.
- the content exceeding 0.060% is limited to 0.060% or less in order to reduce the joint CTOD characteristics.
- Ni 0.5 to 2.0%
- Ni is an element that can increase the strength without greatly degrading the toughness of both the base material and the joint. In order to acquire the effect, 0.5% or more of content is required. However, if it exceeds 2.0%, the effect of increasing the strength is saturated, so that an increase in cost becomes a problem. Therefore, the upper limit was made 2.0%. It is preferably 0.5 to 1.8%.
- Ti 0.005 to 0.030%
- Ti precipitates as TiN and is an element that suppresses HAZ austenite grain coarsening, refines the HAZ structure, and improves toughness. In order to acquire such an effect, 0.005% or more of content is required.
- the content exceeds 0.030%, the weld heat-affected zone toughness decreases due to precipitation of solute Ti and coarse TiC. Therefore, Ti is limited to the range of 0.005 to 0.030%.
- the content is 0.005 to 0.025%.
- N 0.0015 to 0.0065% N is an element effective for improving toughness by suppressing the coarsening of austenite grains of HAZ by being precipitated as TiN and by refining the HAZ structure. In order to acquire such an effect, 0.0015% or more of content is required. On the other hand, when it exceeds 0.0065% and it contains excessively, the heat-affected zone toughness will fall. Therefore, the content is limited to 0.0015 to 0.0065%. Preferably it is 0.0015 to 0.0055%.
- O 0.0010 to 0.0050%
- O is an element necessary for inclusions for improving the toughness of the multilayer welded HAZ, and should be contained in an amount of 0.0010% or more.
- the content is limited to the range of 0.0010 to 0.0050%.
- the content is 0.0010 to 0.0045%.
- Ca 0.0005 to 0.0060%
- Ca is an element necessary for inclusions for improving the toughness of the multilayer welded HAZ, and it is necessary to contain 0.0005% or more.
- the content is limited to the range of 0.0005 to 0.0060%. Preferably it is 0.0007 to 0.0050%.
- Ti / N controls the amount of solid solution N in HAZ and the precipitation state of TiC. If Ti / N is less than 1.5, the HAZ toughness deteriorates due to the presence of solid solution N not fixed as TiN. On the other hand, if Ti / N exceeds 5.0, the HAZ toughness deteriorates due to precipitation of coarse TiC. Therefore, Ti / N was limited to the range of 1.5 to 5.0. Preferably, it is 1.8 or more and 4.5 or less. In said formula (1), each alloy element shall be content (mass%).
- Ceq 0.45% or less
- the HAZ toughness deteriorates due to an increase in the amount of inferior toughness such as island martensite and bainite in the HAZ structure.
- Ceq is larger than 0.45%, the required joint CTOD characteristic cannot be satisfied even if the HAZ toughness improving technique by inclusions is used due to the toughness deterioration of the HAZ base structure itself, so the upper limit was made 0.45%.
- Ceq [C] + [Mn] / 6 + ([Cu] + [Ni]) / 15 + ([Cr] + [Mo] + [V]) / 5 (2)
- Each alloy element has a content (mass%).
- Pcm 0.20% or less
- the structure of inferior toughness such as island martensite and bainite in the HAZ structure increases and HAZ toughness deteriorates. If the Pcm exceeds 0.20%, the toughness of the HAZ base structure itself deteriorates, and the required joint CTOD characteristics cannot be obtained even by using the HAZ toughness improvement technology by inclusions. It was.
- Pcm [C] + [Si] / 30 + ([Mn] + [Cu] + [Cr]) / 20+ [Ni] / 60 + [Mo] / 15 + [V] / 10 + 5 [B] (3)
- each alloy element has a content (mass%).
- each alloy element has a content (mass%).
- the thick steel plate according to the present invention has the above-mentioned component composition as a basic composition, with the remainder being Fe and inevitable impurities. Further, for the purpose of adjusting strength, toughness, and improving joint toughness, Cu: 0.05 to 2.0%, Cr: 0.05 to 0.30%, Mo: 0.05 to 0.30%, Nb: 0.0. 005 to 0.035%, V: 0.01 to 0.10%, W: 0.01 to 0.50%, B: 0.0005 to 0.0020%, REM: 0.0020 to 0.0200% Mg: One or more of 0.0002 to 0.0060% can be contained.
- Cu 0.05 to 2.0%
- Cu is an element that can be increased in strength without greatly degrading the base metal and joint toughness. In order to obtain the effect, it is necessary to contain 0.05% or more. However, if 2.0% or more is added, cracking of the steel sheet due to the Cu concentrated layer generated immediately below the scale becomes a problem, so when added, the content is made 0.05 to 2.0%. It is preferably 0.1 to 1.5%.
- Cr 0.05-0.30% Cr is an element that improves the strength by improving the hardenability of the steel. However, if added excessively, the joint CTOD characteristics are deteriorated, so when added, the content is made 0.05 to 0.30%.
- Mo 0.05-0.30% Mo is an element that improves the strength through the improvement of the hardenability of steel, but if added in excess, the joint CTOD characteristics are lowered. Therefore, when added, the content is made 0.05 to 0.30%.
- Nb 0.005 to 0.035%
- Nb is an element that widens the non-recrystallization temperature region of the austenite phase, and is an effective element for efficiently performing non-recrystallization region rolling to obtain a fine structure.
- 0.005% or more of content is required. However, if it exceeds 0.035%, the joint CTOD characteristics are deteriorated. Therefore, when added, the content is made 0.005 to 0.035%.
- V 0.01 to 0.10%
- V is an element that improves the strength of the base material, and is effective when added in an amount of 0.01% or more. However, if it exceeds 0.10%, the HAZ toughness is lowered, so when added, the content is made 0.01 to 0.10%. It is preferably 0.02 to 0.05%.
- W 0.01 to 0.50% W is an element that improves the strength of the base material, and exhibits an effect when added in an amount of 0.01% or more. However, if it exceeds 0.50%, the HAZ toughness is lowered, so when added, the content is made 0.01 to 0.50%. It is preferably 0.05 to 0.35%.
- B 0.0005 to 0.0020%
- B is an element effective for improving the hardenability and thereby improving the strength of the steel sheet by containing a very small amount thereof. To obtain such an effect, B needs to be contained in an amount of 0.0005% or more. However, if the content exceeds 0.0020%, the HAZ toughness decreases, so when added, the content is made 0.0005 to 0.0020%.
- REM 0.0020 to 0.0200% REM suppresses HAZ austenite grain growth and improves HAZ toughness by forming oxysulfide inclusions. In order to acquire such an effect, 0.0020% or more needs to be contained. However, an excessive content exceeding 0.0200% lowers the base metal and HAZ toughness, so when added, the content is made 0.0020 to 0.0200%.
- Mg 0.0002 to 0.0060%
- Mg is an element effective in improving the weld heat affected zone toughness by suppressing the growth of austenite grains in the weld heat affected zone by forming oxide inclusions.
- the content 0.0002% or more is necessary.
- the content exceeds 0.0060%, the effect is saturated and an effect commensurate with the content cannot be expected, which is economically disadvantageous. Therefore, when added, the content is made 0.0002 to 0.0060%.
- the effective crystal grain size of the material microstructure is set to 20 ⁇ m or less.
- the phase of the base material microstructure is not particularly limited as long as a desired strength can be obtained.
- the effective crystal grain size in the present invention is a circle equivalent diameter of a crystal grain surrounded by a large-angle grain boundary whose orientation difference from an adjacent crystal grain is 15 ° or more.
- Inclusions Compound inclusions of sulfides containing Ca and Mn and oxides containing Al: 25-250 pieces / mm 2 when the equivalent circle diameter is 0.1 ⁇ m or more When a sulfide containing Mn is formed, a Mn-diluted region is formed around the inclusions, which is effective as a transformation nucleus. Further, since Ca is contained in the sulfide, it has a high melting point, and remains even at a temperature rise in the vicinity of the HAZ weld line, thereby exhibiting an austenite grain growth suppressing effect and a transformation nucleus effect.
- the composite inclusion has a circle-equivalent diameter of 0.1 ⁇ m or more, and 25 to 250 / mm 2 at each of the 1/4 and 1/2 positions of the plate thickness, preferably 35-170 pieces / mm 2 . 4).
- the reasons for limiting the conditions for the manufacturing method are described below. The following temperatures are the steel surface temperatures unless otherwise specified.
- Heating condition of steel slab The steel slab shall be continuously cast and heated to 950 ° C or higher and 1200 ° C or lower.
- the heating temperature is lower than 950 ° C., an untransformed region remains during heating and a coarse structure during solidification remains, so that a desired fine grain structure cannot be obtained.
- the heating temperature is higher than 1200 ° C., austenite grains become coarse, and a desired fine grain structure cannot be obtained after controlled rolling.
- heating temperature is limited to 950 degreeC or more and 1200 degrees C or less.
- it is 970 degreeC or more and 1170 degrees C or less.
- Hot rolling defines pass conditions in the recrystallization temperature range and pass conditions in the non-recrystallization temperature range.
- the rolling reduction / pass when the plate thickness center temperature is 950 ° C. or higher is 8% or higher so that the cumulative rolling reduction is 30% or higher.
- the reduction ratio / pass at a plate thickness center temperature of 950 ° C. or higher is reduced to 5% or more so that the cumulative reduction ratio is 35% or more.
- the rolling rate / pass is less than 8%, there is no grain refinement due to recrystallization. Even when the rolling reduction / pass is 8% or more, if the cumulative rolling amount is 30% or less, crystal grain refining is insufficient, so that the rolling reduction with a rolling reduction / pass of 8% or more is 30%. % Or more. Further, the present inventors have further studied that even when the rolling reduction / pass is 5% or more, the grain reduction by recrystallization occurs sufficiently by setting the cumulative rolling amount to 35% or more. It was. Therefore, when the rolling reduction / pass is 5% or higher, the cumulative rolling reduction is set to 35% or higher.
- the cumulative reduction ratio when the sheet thickness center temperature is less than 950 ° C. is 40% or more.
- recrystallization hardly occurs during rolling at less than 950 ° C., and the introduced strain is recrystallized. Accumulated without being consumed, the final structure is refined by acting as a transformation nucleus at the time of subsequent cooling.
- the cumulative rolling reduction is less than 40%, the effect of crystal grain refinement is insufficient, so the cumulative rolling reduction when the plate thickness center temperature is less than 950 ° C. is limited to 40% or more.
- Cooling conditions Cooling after hot rolling is performed so that the average cooling rate between 700 and 500 ° C. at the center of the plate thickness is 1 to 50 ° C./sec, and the cooling stop temperature is 600 ° C. or less.
- tempering is performed at 700 ° C. or lower after cooling is stopped.
- the tempering temperature is higher than 700 ° C., a coarse ferrite phase is generated and the toughness of SCHAZ is deteriorated.
- 650 degrees C or less is preferable.
- Table 1 shows the composition of the test steel. It should be noted that the casting speed was 0.2 to 0.4 m / min. The water density in the cooling zone is 1000 to 2000 l / min. A steel piece continuously cast under the condition of m 2 was used. Steel types A to K are invention examples whose component compositions satisfy the scope of the present invention, and steel types L to T are comparative examples whose component compositions are outside the scope of the present invention. Using these steel types, thick steel plates were produced under the production conditions shown in Table 2. Moreover, the multilayer pile-welded joint was created for every obtained thick steel plate. At the time of hot rolling, a thermocouple was attached to the plate length, width, and plate thickness center position, and the plate thickness center temperature was measured.
- the average effective crystal grain size in the microstructure of the base material and the distribution of inclusions in the thickness direction were investigated.
- the average effective grain size is measured by taking a sample from the longitudinal, width, and thickness direction center of the plate, performing mirror polishing and performing EBSP analysis under the following conditions, and being adjacent to the obtained crystal orientation map
- the equivalent circle diameter of a structure surrounded by large-angle grain boundaries whose orientation difference from the crystal grains was 15 ° or more was evaluated as the effective crystal grain size.
- EBSP conditions Analysis area 1 mm x 1 mm area at the center of plate thickness Step size: 0.4 ⁇ m
- the density of inclusions is measured by taking samples from 1/4 and 1/2 positions of the plate length, width and plate thickness direction, mirror polishing with diamond buff + alcohol, and then field emission type. Inclusions existing in an evaluation region of 1 mm ⁇ 1 mm were identified by EDX analysis using a scanning electron microscope (FE-SEM), and the inclusion density was evaluated together. In addition, in the evaluation of the inclusion type, when various elements were contained in an atomic fraction of 3% or more with respect to the chemical composition of the inclusion quantified by the ZAF method, it was determined that the inclusion was included.
- the welded joint used in the joint CTOD test was created using submerged arc welding (multilayer welding) with a K groove shape and a heat input of 5.0 kJ / mm.
- the test method was based on BS standard EN10225 (2009), and a CTOD value ( ⁇ ) was evaluated at a test temperature of ⁇ 40 ° C. using a test piece having a cross-sectional shape of t (plate thickness) ⁇ t (plate thickness).
- Three steels were tested at each notch position for each steel type, and a steel sheet having an average CTOD value of 0.40 mm or more was determined as a steel sheet excellent in joint CTOD characteristics.
- the notch position is CGHAZ (position of 0.25 mm from the weld line to the base metal side) directly on the K groove and the SC / ICHAZ boundary (corrosion HAZ boundary that appears when the joint CTOD specimen is etched with nitric acid). 0.25 mm position on the side).
- CGHAZ position of 0.25 mm from the weld line to the base metal side
- SC / ICHAZ boundary corrosion HAZ boundary that appears when the joint CTOD specimen is etched with nitric acid. 0.25 mm position on the side.
- Table 2 shows the test results.
- No. 1 to 11 are steel types that are within the scope of the invention in terms of chemical composition, average crystal grain size of the base material, inclusion density, and production conditions, and the notch position exhibits excellent joint CTOD characteristics at both the CGHAZ and SC / ICHAZ boundaries.
- No. 12 to 26 are comparative examples, and the joint CTOD characteristics at the CGHAZ and / or SC / ICHAZ boundary are inferior.
- No. No. 12 has a large amount of C, and the HAZ structure becomes a hard structure with poor toughness, so the joint CTOD value of CGHAZ is low.
- No. No. 13 has a small amount of Ti and Ti / N, and the amount of TiN necessary for suppressing the coarsening of the HAZ structure is small. Therefore, the joint CTOD value of CGHAZ is low.
- No. No. 14 has a large Ti / N, and has low HAZ toughness due to the precipitation of coarse TiC and the presence of solute Ti, so the joint CTOD value at the CGHAZ / SC / ICHAZ boundary is low.
- No. No. 15 has a high Ceq outside the range of the present invention, and the HAZ structure has become a hard structure with poor toughness, so the joint CTOD value of CGHAZ is low.
- the amount of B and Pcm are high outside the range of the present invention, and the HAZ structure becomes a hard structure with poor toughness, so the joint CTOD value of CGHAZ is low.
- No. No. 17 has a small ACR, the main component of sulfide inclusions is MnS, and the amount of Ca-based composite inclusions required for refining the HAZ structure is small, so the joint CTOD value of CGHAZ is low.
- No. No. 18 has a large ACR, the main component of sulfide inclusions is CaS, and the amount of Ca-based composite inclusions necessary for refining the HAZ structure is small, so the joint CTOD value of CGHAZ is low.
- No. No. 19 has a small amount of Ca and a small amount of Ca-based composite inclusions necessary for refining the HAZ structure, so that the joint CTOD value of CGHAZ is low.
- No. No. 20 has a large amount of S and Ca, and the joint CTOD value at the boundary of CGHAZ and SC / ICHAZ is low due to an increase in the amount of inclusions.
- No. No. 21 has a high heating temperature, and the average crystal grain size of the base material becomes coarse due to grain growth during high-temperature heating, so the joint CTOD value at the SC / ICHAZ boundary is low.
- No. No. 22 has a low heating temperature, the cast structure remains, and the average crystal grain size of the base material becomes coarse, so the joint CTOD value at the SC / ICHAZ boundary is low.
- No. No. 23 has a small reduction amount in the recrystallization region, and the average crystal grain size of the base material becomes coarse, so the joint CTOD value at the SC / ICHAZ boundary is low.
- No. No. 24 has a low rolling reduction in the non-recrystallized region and the average crystal grain size of the base material is coarse, so the joint CTOD value at the SC / ICHAZ boundary is low.
- No. No. 25 has a low cooling rate and the average crystal grain size of the base material becomes coarse due to the formation of coarse ferrite, so the joint CTOD value at the SC / ICHAZ boundary is low.
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Abstract
Description
(1)鋼中のCa、OおよびSを、下式で示される原子濃度比(ACR:Atomic Concentration Ratio)が0.2~1.4の範囲内となるように制御すると、硫化物の形態がMnの一部固溶したCa系硫化物とAl系酸化物の複合介在物となる。
(2)介在物形態をCaとMnを含む硫化物とAlを含む酸化物からなる複合介在物とすることで、溶接線近傍の高温まで昇温される領域においても安定的に存在できるためオーステナイト粒粗大化効果を十分に発揮できる。さらに、複合介在物周囲にMn希薄層が形成されるためベイナイトやアシキュラーフェライトの核生成効果を有する。
(3)HAZの冷却時の核生成サイトは主にオーステナイト粒界である。本発明では、オーステナイト粒内に核生成効果を有する上記複合介在物が存在することで、オーステナイト粒界に加えオーステナイト粒内からも核生成が開始し、最終的に得られるHAZ組織が微細となり、HAZの靭性および継手CTOD特性が向上する。
(4)上記複合介在物によるベイナイトやアシキュラーフェライト、フェライトの核生成効果は介在物サイズが微小すぎると不十分であり、円相当直径0.1μm以上必要である。
(5)上記複合介在物の変態核生成効果を十分に活用するためには、溶接昇温時にHAZのオーステナイト粒内中に少なくとも1個以上の介在物が存在する必要があり、入熱量が5kJ/mm程度では溶接線近傍のオーステナイト粒径は約200μmとなるため、介在物の密度は25個/mm2以上必要となる。
(6)一方、上記複合介在物自体の靭性は低いため、過剰な量の介在物ではかえってHAZ靭性が低下してしまう。特に連続鋳造によりスラブが製造される際、介在物と鋼の密度差によりスラブ中の未凝固部分を浮上することで1/4t(t:板厚)位置に介在物が集積し易いため、介在物個数が過剰とならないようにする必要がある。また、元素の偏析が存在し多層溶接HAZ靭性の劣る板厚中心部分においても介在物個数を適切にする必要があり、介在物個数を250個/mm2以下とすることで良好な多層溶接継手CTOD特性が確保できる。
(7)通常、スラブの板厚中心の元素偏析部には合金元素が濃化することで粗大な介在物が低密度で分散してしまう問題が生じる。しかしながら、板厚中心温度が950℃以上における圧下率/パスが8%以上のパスの累積圧下率が30%以上、もしくは、板厚中心温度が950℃以上における圧下率/パスが5%以上のパスの累積圧下率が35%以上といった1パス当たり大きな圧下を加えることで、板厚中心に加わる歪みを増加させ、粗大介在物を伸長、さらには分断させることで細かな介在物を高密度に分散させることができ、介在物によるHAZ靭性向上効果を確保することができるとともに、特別CTOD仕様にも対応可能な良好なCTOD特性を実現することができる。
1.質量%で、成分組成が、C:0.03~0.10%、Si:0.5%以下、Mn:1.0~2.0%、P:0.015%以下、S:0.0005~0.0050%、Al:0.005~0.060%、Ni:0.5~2.0%、Ti:0.005~0.030%、N:0.0015~0.0065%、O:0.0010~0.0050%、Ca:0.0005~0.0060%を含み、(1)~(4)の各式を満足し、残部Feおよび不可避的不純物からなり、板厚中心における母材の有効結晶粒径が20μm以下、板厚(t:mm)の1/4と1/2のそれぞれにおいてCaとMnを含む硫化物とAlを含む酸化物からなる円相当直径0.1μm以上の複合介在物が25~250個/mm2存在する多層溶接継手CTOD特性に優れた厚鋼板。
1.5≦Ti/N≦5.0 (1)
Ceq(=[C]+[Mn]/6+([Cu]+[Ni])/15+([Cr]+[Mo]+[V])/5)≦0.45 (2)
Pcm(=[C]+[Si]/30+([Mn]+[Cu]+[Cr])/20+[Ni]/60+[Mo]/15+[V]/10+5[B])≦0.20 (3)
0.2<(Ca-(0.18+130×Ca)×O)/(1.25×S)<1.4 (4)
(1)~(4)式において、各合金元素は含有量(質量%)とする。
2.更に、質量%で、Cu:0.05~2.0%、Cr:0.05~0.30%、Mo:0.05~0.30%、Nb:0.005~0.035%、V:0.01~0.10%、W:0.01~0.50%、B:0.0005~0.0020%、REM:0.0020~0.0200%、Mg:0.0002~0.0060%のうちの1種または2種以上を含むことを特徴とする1に記載の多層溶接継手CTOD特性に優れた厚鋼板。
3.1または2記載の成分組成の鋼片を950℃以上1200℃以下に加熱し、板厚中心温度が950℃以上における圧下率/パスが8%以上のパスの累積圧下率が30%以上、板厚中心温度が950℃未満での累積圧下率が40%以上となる熱間圧延後、板厚中心での700-500℃間の平均冷却速度が1~50℃/secとなる冷却を600℃以下まで行うことを特徴とする1または2記載の多層溶接継手CTOD特性に優れた厚鋼板の製造方法。
4.1または2記載の成分組成の鋼片を950℃以上1200℃以下に加熱し、板厚中心温度が950℃以上における圧下率/パスが5%以上のパスの累積圧下率が35%以上、板厚中心温度が950℃未満での累積圧下率が40%以上となる熱間圧延後、板厚中心での700-500℃間の平均冷却速度が1~50℃/secとなる冷却を600℃以下まで行うことを特徴とする請求項1または2記載の多層溶接継手CTOD特性に優れた厚鋼板の製造方法。
5.冷却後、700℃以下の温度で焼戻し処理を行うことを特徴とする3または4に記載の多層溶接継手CTOD特性に優れた厚鋼板の製造方法。
はじめに、本発明の鋼の化学成分を規定した理由を説明する。なお、%は全て質量%を意味する。
Cは、鋼の強度を向上させる元素であり、0.03%以上の含有を必要とする。しかし、0.10%を超えてCを過剰に含有すると継手CTOD特性が低下する。このため、Cは0.03~0.10%の範囲に限定した。なお好ましくは0.04~0.08%である。
0.5%を超えてSiを過剰に含有すると継手CTOD特性が低下する。このため、Siは0.5%以下の範囲に限定した。なお好ましくは0.4%以下であり、さらに好ましくは0.1%超え0.3%以下である。
Mnは、鋼の焼入れ性の向上を介して強度を向上させる元素である。しかしながら、過剰に添加すると継手CTOD特性を著しく低下させる。このため、Mnは1.0~2.0%の範囲に限定した。なお好ましくは1.2~1.8%の範囲である。
Pは、不純物として鋼中に不可避的に含有される元素であり、鋼の靭性を低下させるため、できるだけ低減することが望ましい。特に0.015%を超える含有は、著しく継手CTOD特性を低下させるため、0.015%以下に限定した。好ましくは0.010%以下である。
Sは、多層溶接HAZの靭性を向上させるための介在物に必要な元素であり、0.0005%以上の含有が必要である。しかしながら、0.0050%を超える含有は、継手CTOD特性を低下させるため、0.0050%以下に限定した。好ましくは0.0045%以下である。
Alは、多層溶接HAZの靭性を向上させるための介在物に必要な元素であり、0.005%以上の含有が必要である。一方、0.060%を超える含有は、継手CTOD特性を低下させるため、0.060%以下に限定した。
Niは、母材と継手の両方の靭性を大きく劣化させることなく高強度化が可能な元素である。その効果を得るためには、0.5%以上の含有を必要とする。しかし、2.0%を超えると強度上昇の効果が飽和するためコスト増加が問題となる。そのため、上限を2.0%とした。なお好ましくは0.5~1.8%である。
Tiは、TiNとして析出することでHAZのオーステナイト粒粗大化を抑制し、HAZ組織を微細化し、靭性向上に有効な元素である。このような効果を得るためには0.005%以上の含有を必要とする。一方、0.030%を超えて過剰に含有すると、固溶Tiや粗大TiCの析出により溶接熱影響部靭性が低下するようになる。このため、Tiは0.005~0.030%の範囲に限定した。好ましくは0.005~0.025%である。
Nは、TiNとして析出することでHAZのオーステナイト粒粗大化を抑制し、HAZ組織の微細化により、靭性向上に有効な元素である。このような効果を得るためには0.0015%以上の含有を必要とする。一方、0.0065%を超えて過剰に含有すると、溶接熱影響部靭性が低下するようになる。このため、0.0015~0.0065%の範囲に限定した。好ましくは0.0015~0.0055%である。
Oは、多層溶接HAZの靭性を向上させるための介在物に必要な元素であり、0.0010%以上の含有が必要である。一方、0.0050%を超える含有は、継手CTOD特性が低下するようになるため、本発明では0.0010~0.0050%の範囲に限定した。好ましくは0.0010~0.0045%である。
Caは、多層溶接HAZの靭性を向上させるための介在物に必要な元素であり、0.0005%以上の含有が必要である。一方、0.0060%を超える含有は、かえって継手CTOD特性が低下するため、本発明では0.0005~0.0060%の範囲に限定した。好ましくは0.0007~0.0050%である。
Ti/Nは、HAZにおける固溶N量とTiCの析出状態を制御する。Ti/Nが1.5未満では、TiNとして固定されていない固溶Nの存在によりHAZ靭性が劣化する、一方Ti/Nが5.0より大きいと粗大TiCの析出によりHAZ靭性が劣化する。そのためTi/Nを1.5以上5.0以内の範囲に限定した。なお好ましくは1.8以上4.5以下である。上記式(1)において、各合金元素は含有量(質量%)とする。
Ceqが増加すると、HAZ組織中の島状マルテンサイトやベイナイトといった靭性の劣る組織量の増加によりHAZ靭性が劣化する。Ceqが0.45%より大きくなると、HAZの基地組織自体の靭性劣化により介在物によるHAZ靭性向上技術を用いても必要な継手CTOD特性を満足できなくなるため上限を0.45%とした。なお、Ceq=[C]+[Mn]/6+([Cu]+[Ni])/15+([Cr]+[Mo]+[V])/5…(2)とし、式(2)において、各合金元素は含有量(質量%)とする。
Pcmが増加すると、HAZ組織中の島状マルテンサイトやベイナイトなど靭性の劣る組織が増加してHAZ靭性が劣化する。Pcmが0.20%を超えると、HAZの基地組織自体の靭性が劣化して、介在物によるHAZ靭性向上技術を用いても必要な継手CTOD特性が得られないため、上限を0.20%とした。Pcm=[C]+[Si]/30+([Mn]+[Cu]+[Cr])/20+[Ni]/60+[Mo]/15+[V]/10+5[B]…(3)とし、式(3)において、各合金元素は含有量(質量%)とする。
(Ca-(0.18+130×Ca)×O)/(1.25×S)は鋼中のCa、OおよびSの原子濃度比(ACR:Atomic Concentration Ratio)で、0.2未満では硫化物系介在物の主要形態がMnSとなる。MnSは融点が低く溶接時の溶接線近傍では溶解してしまうため、溶接線近傍でのオーステナイト粒粗大化抑制効果および溶接後の冷却時の変態核効果も得られない。一方、(Ca-(0.18+130×Ca)×O)/(1.25×S)が1.4を超えると硫化物系介在物の主要形態はCaSとなるため、CaS周囲に変態核となるために必要なMn希薄層が形成されないため変態核効果が得られない。従って、0.2以上1.4以下とする。なお好ましくは0.3以上1.2以下の範囲である。式(4)において、各合金元素は含有量(質量%)とする。
Cuは、母材、継手靭性を大きく劣化させることなく高強度化が可能な元素で、その効果を得るためには、0.05%以上の含有を必要する。しかし、2.0%以上の添加を行うとスケール直下に生成するCu濃化層起因の鋼板割れが問題となるため、添加する場合は、0.05~2.0%とする。なお好ましくは0.1~1.5%である。
Crは、鋼の焼入れ性の向上を介して強度を向上させる元素であるが、過剰に添加すると継手CTOD特性を低下させるため、添加する場合は、0.05~0.30%とする。
Moは、鋼の焼入れ性の向上を介して強度を向上させる元素であるが、過剰に添加すると継手CTOD特性を低下させる。このため、添加する場合は0.05~0.30%とする。
Nbは、オーステナイト相の未再結晶温度域を広げる元素であり、未再結晶域圧延を効率的に行い微細組織を得るために有効な元素である。その効果を得るためには0.005%以上の含有を必要とする。しかしながら、0.035%を超えると継手CTOD特性の低下を招くため、添加する場合は、0.005~0.035%とする。
Vは、母材の強度を向上させる元素であり、0.01%以上の添加で効果を発揮する。しかし、0.10%を超えるとHAZ靭性の低下を招くため、添加する場合は、0.01~0.10%とする。なお好ましくは0.02~0.05%である。
Wは、母材の強度を向上させる元素であり、0.01%以上の添加で効果を発揮する。しかし、0.50%を超えるとHAZ靭性の低下を招くため、添加する場合は、0.01~0.50%とする。なお好ましくは0.05~0.35%である。
Bは、極微量の含有で焼入れ性を向上させ、それにより鋼板の強度を向上させるのに有効な元素であり、このような効果を得るには0.0005%以上の含有を必要とする。しかし、0.0020%を超えて含有すると、HAZ靭性が低下するようになるため、添加する場合は、0.0005~0.0020%とする。
REMは、酸硫化物系介在物を形成することでHAZのオーステナイト粒成長を抑制しHAZ靭性を向上させる。このような効果を得るためには、0.0020%以上の含有を必要とする。しかし、0.0200%を超える過剰の含有は、母材、HAZ靭性を低下させるようになるため、添加する場合は0.0020~0.0200%とする。
Mgは、酸化物系介在物を形成することで溶接熱影響部においてオーステナイト粒の成長を抑制し、溶接熱影響部靭性の改善に有効な元素である。このような効果を得るには0.0002%以上の含有が必要である。しかし、0.0060%を超える含有は、効果が飽和して含有量に見合う効果が期待できずに経済的に不利となるため、添加する場合は0.0002~0.0060%とする。
SC/ICHAZ境界の継手CTOD特性を向上させるため、中心偏析が存在しやすい、板厚中心での結晶粒微細化により母材靭性が向上するように、板厚中心での母材ミクロ組織の有効結晶粒径を20μm以下とする。母材ミクロ組織の相は、所望する強度が得られれば良く、特に規定しない。なお、本発明における有効結晶粒径とは、隣接する結晶粒との方位差が15°以上の大角粒界で囲まれた結晶粒の円相当直径である。
CaとMnを含む硫化物とAlを含む酸化物の複合介在物:円相当直径が0.1μm以上で25~250個/mm2
Mnを含んだ硫化物が形成される際、介在物周囲にMn希薄域が形成されることで変態核として有効となる。さらに硫化物にCaも含有されることで高融点下し、HAZの溶接線近傍の昇温でも残存しオーステナイト粒成長抑制効果と変態核効果が発揮される。このような効果を得るため、複合介在物は円相当直径を0.1μm以上の大きさとし、板厚の1/4と1/2のそれぞれの位置において、25~250個/mm2、好ましくは35~170個/mm2とする。
4.製造方法について
製造方法について、各条件の限定理由を以下に述べる。なお以下の温度は特に断らない限り鋼材の表面温度とする。
鋼片は連続鋳造によるものとし、950℃以上1200℃以下に加熱する。加熱温度が950℃より低くなると加熱時に未変態領域が残存し、凝固時の粗大組織が残存してしまうため所望の細粒組織が得られなくなる。一方、加熱温度が1200℃よりも高くなると、オーステナイト粒が粗大になり制御圧延後に所望の細粒組織が得られなくなる。このため、加熱温度を950℃以上1200℃以下に限定する。なお好ましくは970℃以上1170℃以下である。
熱間圧延は再結晶温度域のパス条件と未再結晶温度域のパス条件を規定する。再結晶温度域では、板厚中心温度が950℃以上における圧下率/パスが8%以上の圧下を累積圧下率が30%以上となるように行う。もしくは、再結晶温度域では、板厚中心温度が950℃以上における圧下率/パスが5%以上の圧下を累積圧下率が35%以上となるように行う。
本発明鋼は950℃未満での圧延では再結晶が起こり難くなり、導入された歪みは再結晶に消費されずに蓄積され、後の冷却時の変態核として作用することで最終組織が微細化する。また、累積圧下率が40%未満では結晶粒微細化効果が不十分であるため、板厚中心温度が950℃未満での累積圧下率を40%以上に限定した。
熱間圧延後の冷却は、板厚中心位置における、700-500℃間での平均冷速が1~50℃/secとなるように行い、冷却停止温度は600℃以下とする。
解析領域:板厚中心の1mm×1mm領域
ステップサイズ:0.4μm
介在物の密度測定は、板の長手、幅、板厚方向の板厚の1/4、1/2位置よりサンプルを採取し、ダイヤモンドバフ+アルコールで鏡面研磨仕上げを行った後、電界放出型走査型電子顕微鏡(FE-SEM)を用いて1mm×1mmの評価領域に存在する介在物をEDX分析により同定し、合わせて介在物密度を評価した。なお介在物種類の評価は、ZAF法で定量化した介在物の化学組成に対し各種元素が原子分率で3%以上含まれる場合、その元素が含まれる介在物であると判断した。
Claims (5)
- 質量%で、成分組成がC:0.03~0.10%、Si:0.5%以下、Mn:1.0~2.0%、P:0.015%以下、S:0.0005~0.0050%、Al:0.005~0.060%、Ni:0.5~2.0%、Ti:0.005~0.030%、N:0.0015~0.0065%、O:0.0010~0.0050%、Ca:0.0005~0.0060%を含み、(1)~(4)の各式を満足し、残部Feおよび不可避的不純物からなり、板厚中心における母材の有効結晶粒径が20μm以下、板厚(t:mm)の1/4と1/2のそれぞれにおいてCaとMnを含む硫化物とAlを含む酸化物からなる円相当直径0.1μm以上の複合介在物が25~250個/mm2存在する多層溶接継手CTOD特性に優れた厚鋼板。
1.5≦Ti/N≦5.0 (1)
Ceq(=[C]+[Mn]/6+([Cu]+[Ni])/15+([Cr]+[Mo]+[V])/5)≦0.45 (2)
Pcm(=[C]+[Si]/30+([Mn]+[Cu]+[Cr])/20+[Ni]/60+[Mo]/15+[V]/10+5[B])≦0.20 (3)
0.2<(Ca-(0.18+130×Ca)×O)/(1.25×S)<1.4 (4)
(1)~(4)式において、各合金元素は含有量(質量%)とする。 - 更に、質量%で、Cu:0.05~2.0%、Cr:0.05~0.30%、Mo:0.05~0.30%、Nb:0.005~0.035%、V:0.01~0.10%、W:0.01~0.50%、B:0.0005~0.0020%、REM:0.0020~0.0200%、Mg:0.0002~0.0060%のうちの1種または2種以上を含むことを特徴とする請求項1に記載の多層溶接継手CTOD特性に優れた厚鋼板。
- 請求項1または2記載の成分組成の鋼片を950℃以上1200℃以下に加熱し、板厚中心温度が950℃以上における圧下率/パスが8%以上のパスの累積圧下率が30%以上、板厚中心温度が950℃未満での累積圧下率が40%以上となる熱間圧延後、板厚中心での700-500℃間の平均冷却速度が1~50℃/secとなる冷却を600℃以下まで行うことを特徴とする請求項1または2記載の多層溶接継手CTOD特性に優れた厚鋼板の製造方法。
- 請求項1または2記載の成分組成の鋼片を950℃以上1200℃以下に加熱し、板厚中心温度が950℃以上における圧下率/パスが5%以上のパスの累積圧下率が35%以上、板厚中心温度が950℃未満での累積圧下率が40%以上となる熱間圧延後、板厚中心での700-500℃間の平均冷却速度が1~50℃/secとなる冷却を600℃以下まで行うことを特徴とする請求項1または2記載の多層溶接継手CTOD特性に優れた厚鋼板の製造方法。
- 冷却後、700℃以下の温度で焼戻し処理を行うことを特徴とする請求項3または4に記載の多層溶接継手CTOD特性に優れた厚鋼板の製造方法。
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Citations (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS60184663A (ja) | 1984-02-29 | 1985-09-20 | Kawasaki Steel Corp | 大入熱溶接用低温用高張力鋼 |
JPS61253344A (ja) | 1985-05-01 | 1986-11-11 | Kawasaki Steel Corp | 大入熱溶接用鋼板とその製造方法 |
JPH0277521A (ja) * | 1988-09-13 | 1990-03-16 | Kawasaki Steel Corp | 板厚方向の均質性に優れた溶接用超高張力鋼板の製造方法 |
JPH0353367B2 (ja) | 1984-01-20 | 1991-08-14 | Kawasaki Steel Co | |
JPH05186823A (ja) | 1991-11-13 | 1993-07-27 | Kawasaki Steel Corp | 高靱性Cu含有高張力鋼の製造方法 |
JPH05271766A (ja) * | 1992-03-30 | 1993-10-19 | Nippon Steel Corp | 耐水素誘起割れ性の優れた高強度鋼板の製造方法 |
JPH1017982A (ja) * | 1996-06-28 | 1998-01-20 | Nippon Steel Corp | 耐破壊性能に優れた建築用低降伏比高張力鋼材及びその製造方法 |
JPH11140582A (ja) * | 1997-11-11 | 1999-05-25 | Kawasaki Steel Corp | 溶接熱影響部靱性に優れた高靱性厚鋼板およびその製造方法 |
WO2009072753A1 (en) * | 2007-12-04 | 2009-06-11 | Posco | High-strength steel sheet with excellent low temperature toughness and manufacturing method thereof |
JP2010202949A (ja) * | 2009-03-05 | 2010-09-16 | Sumitomo Metal Ind Ltd | ラインパイプ用鋼材の製造方法 |
JP2012162797A (ja) * | 2011-01-18 | 2012-08-30 | Kobe Steel Ltd | 溶接熱影響部の靱性に優れた鋼材およびその製造方法 |
JP2012184500A (ja) | 2011-02-15 | 2012-09-27 | Jfe Steel Corp | 溶接熱影響部の低温靭性に優れた高張力鋼板およびその製造方法 |
JP2013023713A (ja) * | 2011-07-19 | 2013-02-04 | Jfe Steel Corp | Sr後の溶接部靱性に優れた低降伏比耐hic溶接鋼管およびその製造方法 |
JP2013095927A (ja) * | 2011-10-28 | 2013-05-20 | Nippon Steel & Sumitomo Metal Corp | 靭性に優れた高張力鋼板およびその製造方法 |
JP2013095928A (ja) * | 2011-10-28 | 2013-05-20 | Nippon Steel & Sumitomo Metal Corp | 靭性に優れた高張力鋼板およびその製造方法 |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0353367A (ja) | 1989-07-20 | 1991-03-07 | Toshiba Corp | 分散型情報処理システム |
JP3218447B2 (ja) | 1994-04-22 | 2001-10-15 | 新日本製鐵株式会社 | 優れた低温靱性を有する耐サワー薄手高強度鋼板の製造方法 |
EP1262571B1 (en) * | 2000-02-10 | 2005-08-10 | Nippon Steel Corporation | Steel having weld heat-affected zone excellent in toughness |
JP3699657B2 (ja) * | 2000-05-09 | 2005-09-28 | 新日本製鐵株式会社 | 溶接熱影響部のCTOD特性に優れた460MPa以上の降伏強度を有する厚鋼板 |
JP2002235114A (ja) * | 2001-02-05 | 2002-08-23 | Kawasaki Steel Corp | 大入熱溶接部靱性に優れた厚肉高張力鋼の製造方法 |
JP4096839B2 (ja) | 2003-08-22 | 2008-06-04 | Jfeスチール株式会社 | 超大入熱溶接熱影響部靱性に優れた低降伏比高張力厚鋼板の製造方法 |
JP5435837B2 (ja) * | 2006-03-20 | 2014-03-05 | 新日鐵住金株式会社 | 高張力厚鋼板の溶接継手 |
JP4356950B2 (ja) * | 2006-12-15 | 2009-11-04 | 株式会社神戸製鋼所 | 耐応力除去焼鈍特性と溶接性に優れた高強度鋼板 |
JP4547037B2 (ja) * | 2007-12-07 | 2010-09-22 | 新日本製鐵株式会社 | 溶接熱影響部のctod特性が優れた鋼およびその製造方法 |
JP5439887B2 (ja) | 2008-03-31 | 2014-03-12 | Jfeスチール株式会社 | 高張力鋼およびその製造方法 |
EP2241646B1 (en) * | 2008-10-23 | 2012-09-05 | Nippon Steel Corporation | High tensile strength steel thick plate having excellent weldability and tensile strength of 780mpa or above, and process for manufacturing same |
WO2014141632A1 (ja) | 2013-03-12 | 2014-09-18 | Jfeスチール株式会社 | 多層溶接継手ctod特性に優れた厚鋼板およびその製造方法 |
-
2014
- 2014-03-05 WO PCT/JP2014/001218 patent/WO2014141632A1/ja active Application Filing
- 2014-03-05 JP JP2014530840A patent/JP5618036B1/ja active Active
- 2014-03-05 US US14/774,366 patent/US10023946B2/en active Active
- 2014-03-05 CN CN201480014302.2A patent/CN105008574B/zh active Active
- 2014-03-05 EP EP14762492.8A patent/EP2975148B1/en active Active
- 2014-03-05 KR KR1020157025141A patent/KR101719943B1/ko active IP Right Grant
Patent Citations (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0353367B2 (ja) | 1984-01-20 | 1991-08-14 | Kawasaki Steel Co | |
JPS60184663A (ja) | 1984-02-29 | 1985-09-20 | Kawasaki Steel Corp | 大入熱溶接用低温用高張力鋼 |
JPS61253344A (ja) | 1985-05-01 | 1986-11-11 | Kawasaki Steel Corp | 大入熱溶接用鋼板とその製造方法 |
JPH0277521A (ja) * | 1988-09-13 | 1990-03-16 | Kawasaki Steel Corp | 板厚方向の均質性に優れた溶接用超高張力鋼板の製造方法 |
JPH05186823A (ja) | 1991-11-13 | 1993-07-27 | Kawasaki Steel Corp | 高靱性Cu含有高張力鋼の製造方法 |
JPH05271766A (ja) * | 1992-03-30 | 1993-10-19 | Nippon Steel Corp | 耐水素誘起割れ性の優れた高強度鋼板の製造方法 |
JPH1017982A (ja) * | 1996-06-28 | 1998-01-20 | Nippon Steel Corp | 耐破壊性能に優れた建築用低降伏比高張力鋼材及びその製造方法 |
JPH11140582A (ja) * | 1997-11-11 | 1999-05-25 | Kawasaki Steel Corp | 溶接熱影響部靱性に優れた高靱性厚鋼板およびその製造方法 |
WO2009072753A1 (en) * | 2007-12-04 | 2009-06-11 | Posco | High-strength steel sheet with excellent low temperature toughness and manufacturing method thereof |
JP2010202949A (ja) * | 2009-03-05 | 2010-09-16 | Sumitomo Metal Ind Ltd | ラインパイプ用鋼材の製造方法 |
JP2012162797A (ja) * | 2011-01-18 | 2012-08-30 | Kobe Steel Ltd | 溶接熱影響部の靱性に優れた鋼材およびその製造方法 |
JP2012184500A (ja) | 2011-02-15 | 2012-09-27 | Jfe Steel Corp | 溶接熱影響部の低温靭性に優れた高張力鋼板およびその製造方法 |
JP2013023713A (ja) * | 2011-07-19 | 2013-02-04 | Jfe Steel Corp | Sr後の溶接部靱性に優れた低降伏比耐hic溶接鋼管およびその製造方法 |
JP2013095927A (ja) * | 2011-10-28 | 2013-05-20 | Nippon Steel & Sumitomo Metal Corp | 靭性に優れた高張力鋼板およびその製造方法 |
JP2013095928A (ja) * | 2011-10-28 | 2013-05-20 | Nippon Steel & Sumitomo Metal Corp | 靭性に優れた高張力鋼板およびその製造方法 |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3276026A4 (en) * | 2015-03-26 | 2018-04-18 | JFE Steel Corporation | Thick steel sheet for structural pipe, method for manufacturing thick steel sheet for structural pipe, and structural pipe |
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JP2017110249A (ja) * | 2015-12-15 | 2017-06-22 | 新日鐵住金株式会社 | 耐サワー鋼板 |
WO2018216665A1 (ja) * | 2017-05-22 | 2018-11-29 | Jfeスチール株式会社 | 厚鋼板およびその製造方法 |
JP6477993B1 (ja) * | 2017-05-22 | 2019-03-06 | Jfeスチール株式会社 | 厚鋼板およびその製造方法 |
US11299798B2 (en) | 2017-05-22 | 2022-04-12 | Jfe Steel Corporation | Steel plate and method of producing same |
JP2019183205A (ja) * | 2018-04-05 | 2019-10-24 | Jfeスチール株式会社 | 鋼板およびその製造方法 |
WO2023112634A1 (ja) * | 2021-12-14 | 2023-06-22 | Jfeスチール株式会社 | 鋼板およびその製造方法 |
JP7323086B1 (ja) * | 2021-12-14 | 2023-08-08 | Jfeスチール株式会社 | 鋼板およびその製造方法 |
WO2023219146A1 (ja) * | 2022-05-12 | 2023-11-16 | Jfeスチール株式会社 | 鋼板およびその製造方法 |
JP7468800B2 (ja) | 2022-05-12 | 2024-04-16 | Jfeスチール株式会社 | 鋼板およびその製造方法 |
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EP2975148A1 (en) | 2016-01-20 |
EP2975148B1 (en) | 2019-02-27 |
CN105008574B (zh) | 2018-05-18 |
KR101719943B1 (ko) | 2017-03-24 |
US10023946B2 (en) | 2018-07-17 |
CN105008574A (zh) | 2015-10-28 |
KR20150119285A (ko) | 2015-10-23 |
JPWO2014141632A1 (ja) | 2017-02-16 |
JP5618036B1 (ja) | 2014-11-05 |
EP2975148A4 (en) | 2016-04-27 |
US20160040274A1 (en) | 2016-02-11 |
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