WO1995004838A1 - Acier a resistance a la traction elevee, a resistance a la fatigue et a aptitude au soudage superieures et procede de fabrication - Google Patents
Acier a resistance a la traction elevee, a resistance a la fatigue et a aptitude au soudage superieures et procede de fabrication Download PDFInfo
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- WO1995004838A1 WO1995004838A1 PCT/JP1994/001297 JP9401297W WO9504838A1 WO 1995004838 A1 WO1995004838 A1 WO 1995004838A1 JP 9401297 W JP9401297 W JP 9401297W WO 9504838 A1 WO9504838 A1 WO 9504838A1
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- strength
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Classifications
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0226—Hot rolling
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/002—Bainite
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/021—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips involving a particular fabrication or treatment of ingot or slab
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0231—Warm rolling
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
- 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
Definitions
- the present invention relates to a high-strength steel having excellent fatigue strength and weldability of a weld portion used for shipbuilding, offshore structures, bridges, and the like, and a method for producing the same.
- Si is used to favor the formation of clean polygonal graphite
- B is used to strengthen the steel, and by improving the hardenability, it is possible to obtain good elongation flangeability, fatigue properties
- C 0.01 to 0.2%
- Mn 0.6 to 2.5%
- Si 0.02 to 1.5%
- B 0.0005 to 0.1%
- a high-strength thin steel sheet excellent in quality is disclosed.
- An ultra-low carbon steel sheet comprising 0.001 to 0.100% and having good spot weldability is disclosed.
- JP-A-59-110490 and JP-A-1-1301823 require special work after welding, and the fatigue strength cannot be improved without welding.
- the method using heat treatment after welding is also not preferable because the number of processes increases and the welding work becomes complicated. The effect is also limited.
- Thin steel sheets disclosed in JP-A-62-10239 or JP-A-3-264645 are mainly used for automobile wheels and disk base materials. Since the purpose, thickness, and method of use are completely different from those of steel plates used in shipbuilding and marine structures, which are the subject of the present invention, the findings here are applied to steel plates as they are. It is not possible. Looking at the steel composition, the thin steel sheet disclosed in Japanese Patent Application Laid-Open No. 62-10239 particularly shows that the relationship between the amounts of C and P is C: less than 0.22% and P: 0.16%.
- the aim is to improve the fatigue strength of spot welds by specifying the range of C + 0.6 P31 with C 0.22 to 0.3%, and to improve the weld strength by arc welding. No disclosure is made regarding solid solution strengthening of the flight structure.
- spot welding is a type of resistance welding method, and is mainly used for welding thin steel sheets with a thickness of about 0.5 to 3.5 mra and after forming, for example, thin steel sheets for automotive parts. This is done by sandwiching the welded part of a thin steel plate by pressing it with an electrode and applying a large current in a short time.
- spot welding is the arc welding method used for welding high-tensile steel plates that are used as materials for shipbuilding, marine structures, bridges, etc. with a thickness of 6 mm or more.
- welding methods such as welding conditions, welding conditions, etc.
- shape of the welded part and welding residual stress also differ, the two factors governing the fatigue strength differ between the two. It is not possible to directly apply the knowledge of welding to arc welding.
- the steel sheet disclosed in Japanese Patent Application Laid-Open No. 264645 is a steel sheet to which B has been added to improve the strength and hardenability of the steel and to obtain a desired structure. Not touched. Furthermore, there is no description on the improvement of the fatigue strength of welds other than the base metal.
- the steel sheet disclosed in Japanese Patent Publication No. 56301/1996 relates to spot welds of ultra-low carbon steel sheets and is intended to control the hardness distribution of the spot welds. And grain growth.
- the upper limit of the amount added is set to suppress deterioration of the material, and no study has been made on weldability.
- An object of the present invention is to improve the fatigue strength of a weld of a structural member, particularly, a weld welded by an arc welding method.
- Another object of the present invention is to improve the fatigue strength of the structure of a welded portion of a structural member, particularly the structure of a weld heat affected zone (hereinafter, referred to as HAZ) by controlling the structure of the HAZ up to welding. .
- HAZ weld heat affected zone
- Another object of the present invention is to provide a high-tensile steel plate having good weldability in which weld cracks do not occur immediately after welding.
- Another object of the present invention is to provide a method for producing a high-strength steel plate that achieves the above object. Disclosure of the invention
- the present invention provides the following high-strength steel plate for achieving the above object.
- the inventors of the present invention have observed microscopically the state of crack initiation and propagation in a fatigue test piece of a welded joint. As a result, it was found that fatigue cracks often occur at the boundary between the weld metal and the HAZ where repeated load stresses are concentrated, propagate through the HAZ, and further propagate to the base metal, causing the specimen to fracture. did.
- the HAZ structure in which this fatigue crack is generated and propagated is greatly related to the fatigue strength. Fatigue is caused by the repeated movement of dislocations.To improve the fatigue strength of the weld, fatigue cracks are generated.
- the HAZ structure is strengthened so that it is difficult to propagate, and dislocation movement is suppressed. I came to think I needed to.
- strengthening methods such as solid solution strengthening, precipitation strengthening, and dislocation strengthening. Since the welds are rapidly heated and cooled, the precipitates are also dissolved, so it is not possible to strengthen the HAZ structure up to the weld by precipitation strengthening. Even if the base metal is strengthened by working dislocation, dislocation density is reduced by welding, so dislocation strengthening is not an appropriate strengthening method.
- solid solution strengthening is an effective means to strengthen the HAZ structure.
- Elements effective for solid solution strengthening are C, N, P, Si, Cu, and Mo in the order of their effect.
- C and N which are interstitial elements, have a large effect of solid solution strengthening, but have a greater effect on properties such as hardenability, weldability, and toughness other than solid solution strengthening.
- P has a great effect of solid solution strengthening, but embrittles grain boundaries, so its content must be reduced.
- substitutional Si, Cu, and Mo have a smaller ratio of solid solution strengthening to the added amount than C, N, and P, but are effective for solid solution strengthening because they can be added more than these.
- Si reduces stacking fault energy and reduces cross slip, thereby suppressing localization of deformation during repeated plastic deformation and increasing reversibility of plastic deformation. Has the effect of suppressing the generation of cracks.
- B has the highest cold cracking susceptibility compared to other elements (the larger the coefficient, the higher the cracking susceptibility).
- B has the function of suppressing grain boundary fluoride, which is a source of fatigue cracks. Therefore, when considering the susceptibility to low-temperature cracking, the effect must be suppressed to 0.0020% or less, at which the effect of saturation is saturated. In addition, when P cm is high due to the combination of elements, it is preferable to suppress the addition amount to less than 0.0005%, which is an addition amount that does not substantially affect the cold cracking susceptibility.
- the inventors of the present invention observed microscopically the appearance of crack initiation and propagation in fatigue test specimens of welded joints, and obtained knowledge on the relationship between HAZ structure and fatigue strength.
- the HAZ structure is classified into ferrite structure, bainite structure, and martensite structure according to the hardenability of steel.
- the HAZ structure of commercially available high-strength steel is often the veneer structure.
- the payinite organization was defined as both the upper bainite organization and the lower payinite organization, and the ratio of the payinite organization to the total organization was determined as the bainite organization fraction by microscopic observation.
- High hardenability of HAZ structure Higher fraction of ferrite structure than 20%
- the payinite microstructure fraction is less than 80%
- fatigue cracks are likely to occur from soft lite structures such as grain boundary ferrite ⁇ ite 'side plates, resulting in lower fatigue strength. Does not improve.
- the hardenability is high and the martensite microstructure fraction is higher than 20% and the payneite microstructure fraction is lower than 80%
- fatigue cracks occur from the grain boundaries at the interface of the hard martensite microstructure. Again, the fatigue strength does not improve.
- the present invention provides a high-strength steel sheet having improved fatigue strength and weldability by the effects of the above (1) and (2). Further, by combining (3), a higher strength steel sheet can be obtained. Achieved high-strength steel sheets can be provided.
- FIG. 1A is a plan view showing a fatigue test piece of a T-shaped fillet welded joint.
- FIG. 1B is a side view of the fatigue test piece shown in FIG. 1A.
- C is an element that increases the strength of the base material, and it is desirable to add a large amount of C to increase the strength of the base material.
- the addition of more than 0.20% of C lowers the toughness of the base metal and the weld, and deteriorates the weldability. Therefore, the upper limit of C was set to 0.20%.
- C is too low, it becomes difficult to secure the strength of the base metal, and the hardenability of the weld decreases, resulting in the formation of grain boundary pro-eutectites that are harmful to the fatigue strength.
- the lower limit of C was set to 0.03%.
- Si is a solid solution strengthening element that does not significantly enhance hardenability, and solid solution strengthens the structure. It suppresses the movement of dislocations and the generation of fatigue cracks. Also, Si is known to reduce the eyebrow defect energy of the steel sheet structure and reduce cross slip. As a result, plastic deformation It has the effect of suppressing the occurrence of cracks by suppressing cross-localization of dislocation slip lines and increasing the reversibility of plastic deformation when the shape is repeatedly loaded. Therefore, Si is an essential element for improving fatigue strength.
- the lower limit was set to 0.6%.
- the upper limit was set to 2.0%.
- Mn is an element that increases the strength of the base material without significantly reducing toughness. If Mn is less than 0.6%, sufficient base metal strength cannot be obtained, so the lower limit was set to 0.6%. When Mn is added in excess of 2.0%, not only the toughness of the weld is reduced, but also the weldability and ductility are deteriorated, so the upper limit was set to 2.0%.
- A1 is required as a deoxidizing element, and unless added at 0.01% or more, deoxidizing action cannot be expected. On the other hand, if added in excess of 0.08%, large amounts of A1 oxides and nitrides are generated, deteriorating the toughness of the weld. Therefore, the upper limit was set to 0.08%.
- N When Ti is added, N combines with Ti and suppresses austenite grain growth of HAZ. Since this effect cannot be expected if N is less than 0.002%, the lower limit of N is set to 0.002%. Conversely, if a large amount is added, the amount of dissolved N increases and the HAZ toughness decreases, so the upper limit is set to 0.008%.
- B has the effect of improving the hardenability of the HAZ structure and also has the function of suppressing grain boundary fluoride, which is the source of fatigue cracks, but greatly deteriorates the susceptibility to weld cracking and reduces weldability. It is an element that, when added, causes weld cracks such as root cracks and toe cracks.
- the above effects As the fruits are saturated at 0.0020%, the upper limit of the amount of B added is set to 0.0020% .When the amount of alloying elements other than B is large and P cm is high, the effect on cold cracking susceptibility is substantially negligible. The upper limit was set to less than 0.0005%.
- P and S are the more preferable impurity elements as they are lower.
- P should take into account the toughness of the base metal and the weld
- S should also take into account the toughness of the base metal and the weld as well as the ductility in the thickness direction, and the upper limit should be 0.020%. Is desirable.
- Cu and Mo improve the hardenability of the base metal and HAZ, but these elements are rather effective in strengthening the fiber matrix by solid solution strengthening like Si.
- stacking fault energy does not decrease as much as Si. The effect is not remarkable unless 0.1% and 0.05% or more are added, respectively. Also, if the addition exceeds 1.5% or 0.5%, the hardenability is too high, and the fatigue strength is adversely reduced due to the formation of martensite.
- Ni, Cr, and V are all elements that improve the hardenability of the base metal and HAZ.
- the lower limits of 0.1%, 0.1%, and 0.01%, respectively, were set as the additive amounts at which the effect was exhibited for each element.
- excessive addition facilitates the formation of a lower bainite-martensite structure and rather lowers the fatigue strength of the welded portion. Therefore, the upper limits of the respective contents are set to 3.0%, 1.0% and 0.10%.
- Nb is an element that has the effect of increasing base metal strength and also has an effect on hardenability.
- the non-recrystallization temperature range increases. Therefore, it is desirable to add 0.005% or more in order to control recrystallization during rolling and to enable controlled rolling in a wide temperature range.
- high Nb content lowers HAZ toughness. Therefore, the upper limit of Nb was set to 0.06%.
- Ti combines with N to form TiN, which improves the toughness of HAZ by refining the structure of HAZ. For that purpose, 0.005% or more is necessary, but if it exceeds 0.05%, no further effect is seen, so the lower limit was set to 0.005% and the upper limit to 0.05%.
- Ca has the effect of fixing sulfide, which is the source of fatigue cracks, and improving ductility. Also, the occurrence of fatigue fracture originating from sulfides can be suppressed. If the amount is less than 0.0005%, the effect cannot be expected.
- the lower limit was set to 0.0005% and the upper limit to 0.0050%.
- REM has the same effect as Ca in fixing sulfides that cause fatigue cracks and improving ductility. Also, the occurrence of fatigue fracture originating from sulfides can be suppressed. REM is considered to have the same effect as any other rare earth element. Among them, La, Ce and Y are mentioned as typical examples. In order for the effect of adding REM to be exerted, it is necessary to add a total of 0.0005% or more. Even if 0.0050% or more is added, the effect saturates and is not economical. Therefore, the lower limit was 0.0005% and the upper limit was 0.0050%.
- the present invention is mainly intended for high-tensile steel having a tensile strength of 490 MPa or more. By applying the following manufacturing method, it is possible to obtain thick steel plates having various strengths.
- the ingot before hot rolling, the ingot must first be 100% austenitized. Heating to austenite may be achieved by heating to Ac 3 or higher.However, when heating exceeds 1250 ° C, austenite grains become coarse and the crystal grain size after rolling increases, resulting in a base material such as strength and toughness. Since the characteristics deteriorate, the heating temperature was set to Ar 3 or higher and 1250 ° C or lower. In order to obtain good base metal properties, austenite grain size Need to be smaller. Since the austenite grain size is very large by heating the ingot, hot rolling is performed in the recrystallization temperature range where the austenite grain size can be reduced (normal rolling: about 900 to 1250 ° C) At a temperature of 10 to 95%.
- high-strength steel can be stably obtained at low cost.
- hot rolling is completed in the recrystallization temperature range, and natural cooling is performed.
- the strength may be insufficient when the plate thickness is large or when the added elements are small.
- Controlled rolling (rolling in the non-recrystallization temperature range, approximately 750 to 900 ° C for high-strength steel) can produce high-strength steel with high strength and toughness.
- it is effective to introduce a deformation zone by rolling into the austenite grains to increase the number of ferrite-forming nuclei, and then to perform natural cooling.
- hot rolling with a cumulative reduction of 40% or more in the non-recrystallization temperature region is required.However, if the cumulative reduction exceeds 90%, the base material toughness will decrease. Cumulative rolling reduction was set to 40 to 90%.
- a high-tensile steel having a higher strength than a manufacturing method using only controlled rolling can be obtained.
- it is effective to accelerate the cooling to a temperature at which the transformation ends while keeping the C concentration in the fly high.
- the cooling rate was 1-60 ° C / sec.
- the temperature at which the transformation is completed is 600 ° C or lower, but the cooling stop temperature is usually set at 600 ° C to room temperature because the liquid above room temperature is usually used as the cooling medium.
- the production method using controlled rolling, accelerated cooling and tempering heat treatment is even higher than the production method using a combination of controlled rolling and accelerated cooling.
- High strength steel having strength and toughness can be obtained.
- it is effective to recover the processed structure by dissipating dislocations or reducing the density of lattice defects due to coalescence.
- If the tempering temperature is lower than 300 ° C, these effects cannot be expected.At temperatures above the Ad point, transformation rather than recovery starts, so the tempering temperature and time are set to SOiTC Ac, point, 10 ⁇ 120 minutes.
- Table 2 shows the manufacturing conditions of each steel (heating temperature, cumulative reduction rate in the recrystallization area, cumulative reduction rate in the non-recrystallization area, finishing temperature, cooling start temperature, cooling rate, cooling stop temperature, and tempering temperature). .
- the cumulative reduction in the recrystallization region is (h 0 — h 1) Zh 0, and the cumulative reduction in the non-recrystallization region is the reduction ratio defined by (h 1 — h 2) / h 1 .
- h0 is the slab thickness (mm)
- hi is the thickness after rolling in the recrystallization temperature range or the thickness before rolling in the non-recrystallization temperature range (mm)
- h2 is the rolling in the non-recrystallization temperature range. It is the rear plate thickness (mm).
- Each slab is heated to 3 points or more of Ac and 1250 ° C or less, maintained for 60 minutes, hot-rolled in the recrystallization temperature range, and then cooled naturally or unrecrystallized without natural cooling After hot rolling with a cumulative rolling reduction of 40% to 90% in the temperature range, naturally cool or not cool, and cool at a cooling rate of 1 to SiTCZsec. Cool or temper by heating to the SOiTC Ad point With this, it was manufactured to a finished plate thickness of 15 mm.
- a T-shaped fillet weld fatigue test piece 1 shown in Fig. 1 was prepared.
- 2 is a flat plate
- 3 is a rib plate
- a corner 4 is formed by both plates, and this corner is welded.
- 5 is a weld metal.
- the welding method was sheathed arc welding and the heat input was 18 kJZcm.
- Table 4 shows the fraction of bainite in the HAZ structure of each steel and the crack arresting temperature by oblique y-shaped cracking test (JIS Z3158).
- Steels 1, 2, and 3 of the present invention are examples in which the amount of added Si is three levels.
- the steel 3 of the present invention which has been subjected to controlled rolling at an unrecrystallized region cumulative rolling reduction of 40%, has a higher yield stress and tensile strength.
- the fatigue strength increases, but the Charpy transition temperature also increases, indicating that there is an optimum amount of Si for practical use.
- the steels 4 to 16 of the present invention to which at least one of the groups Cu, Mo, Ni, Cr, Nb, V, Ti, B, Ca, and REM were added also exhibited a solid solution with Cu and Mo, in addition to the effect of Si.
- the fatigue strength increased further than the steels 1 to 3 of the present invention due to the synergistic effect due to the sulfide suppression effect due to Ca and REM, and the sulfide suppression.
- each manufacturing method of normal rolling, controlled rolling, controlled rolling + accelerated cooling, controlled rolling + accelerated cooling + tempering heat treatment is used, but compared to normal rolling, rolling by combining controlled rolling is performed.
- a high strength steel having higher strength was obtained even with the same carbon equivalent.
- the fatigue strength of a welded joint does not depend on the yield stress and tensile strength of the base metal.
- the above-mentioned effects including solid solution strengthening of Si described in the present invention are considered. Is indispensable.
- Comparative Steel 1 is an example in which the amount of Si added is smaller than the composition range of the steel of the present invention. Fatigue strength is improved when the amount of Si added is within the composition range of the steel of the present invention.
- Comparative steels 2 to 8 with excessive addition of Cu, Mo, Ni, Cr, Nb, V, and B have fatigue strengths higher than those of comparative steel 1 because the amount of Si added is within an appropriate range. Although it is a high value, as can be seen from the payite structure fraction in Table 4, the comparative steels 2 to 8 have too high hardenability to form a martensite structure, and , The fatigue strength was lower than that of the steel of the present invention.
- the steel of the present invention with regard to high tensile strength steel used in shipbuilding, offshore structures, bridges, etc., by controlling the structure of the heat-affected zone by adding a specific element while ensuring the weldability of the steel sheet. It is possible to improve the fatigue strength of the welded structure by using the steel of the present invention. It has become possible to improve reliability against fatigue failure.
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Description
Claims
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP94923079A EP0666332A4 (en) | 1993-08-04 | 1994-08-04 | HIGH TENSILE STRENGTH, FATIGUE RESISTANCE AND HIGHER WELDING ABILITY AND METHOD OF MANUFACTURE. |
KR1019950701263A KR0157540B1 (ko) | 1993-08-04 | 1994-08-04 | 용접부의 피로강도와 용접성이 뛰어난 고장력강 및 그 제조방법 |
JP50633695A JP3526576B2 (ja) | 1993-08-04 | 1994-08-04 | 溶接部の疲労強度と溶接性に優れた高張力鋼の製造方法 |
US08/411,738 US5634988A (en) | 1993-03-25 | 1994-08-04 | High tensile steel having excellent fatigue strength at its weld and weldability and process for producing the same |
NO951288A NO951288L (no) | 1993-08-04 | 1995-04-03 | Stål med höy strekkstyrke og god utmattingsstyrke ved dets sveis og sveisbarhet og fremgangsmåte for fremstilling av dette |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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JP5/193350 | 1993-08-04 | ||
JP19335093 | 1993-08-04 |
Publications (1)
Publication Number | Publication Date |
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WO1995004838A1 true WO1995004838A1 (fr) | 1995-02-16 |
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Application Number | Title | Priority Date | Filing Date |
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PCT/JP1994/001297 WO1995004838A1 (fr) | 1993-03-25 | 1994-08-04 | Acier a resistance a la traction elevee, a resistance a la fatigue et a aptitude au soudage superieures et procede de fabrication |
Country Status (6)
Country | Link |
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EP (1) | EP0666332A4 (ja) |
JP (1) | JP3526576B2 (ja) |
KR (1) | KR0157540B1 (ja) |
CN (1) | CN1040555C (ja) |
NO (1) | NO951288L (ja) |
WO (1) | WO1995004838A1 (ja) |
Cited By (6)
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WO1996041024A1 (en) * | 1995-06-07 | 1996-12-19 | Ipsco Inc. | Steckel mill/on-line accelerated cooling combination |
JP2007239042A (ja) * | 2006-03-09 | 2007-09-20 | Kobe Steel Ltd | 疲労亀裂進展抑制および溶接熱影響部の靭性に優れた高降伏比高張力鋼板 |
CN101838768A (zh) * | 2010-04-09 | 2010-09-22 | 武汉钢铁(集团)公司 | 耐低温冲击的热轧u型钢板桩用钢及其生产方法 |
JP2019505672A (ja) * | 2015-12-22 | 2019-02-28 | ポスコPosco | Pwht抵抗性に優れた低温圧力容器用鋼板及びその製造方法 |
CN115058656A (zh) * | 2022-06-30 | 2022-09-16 | 马鞍山钢铁股份有限公司 | 一种寒冷环境下服役的弹性车轮用轮箍及其热处理工艺 |
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Families Citing this family (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6264767B1 (en) | 1995-06-07 | 2001-07-24 | Ipsco Enterprises Inc. | Method of producing martensite-or bainite-rich steel using steckel mill and controlled cooling |
US6309482B1 (en) | 1996-01-31 | 2001-10-30 | Jonathan Dorricott | Steckel mill/on-line controlled cooling combination |
DE19632370C2 (de) * | 1996-08-10 | 1998-07-02 | Thyssen Stahl Ag | Hochleistungsschweißgeeigneter weichmagnetischer Stahl und seine Verwendung für Teile von Magnetschwebebahnen |
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- 1994-08-04 CN CN94190577A patent/CN1040555C/zh not_active Expired - Fee Related
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Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1996041024A1 (en) * | 1995-06-07 | 1996-12-19 | Ipsco Inc. | Steckel mill/on-line accelerated cooling combination |
JP2007239042A (ja) * | 2006-03-09 | 2007-09-20 | Kobe Steel Ltd | 疲労亀裂進展抑制および溶接熱影響部の靭性に優れた高降伏比高張力鋼板 |
CN101838768A (zh) * | 2010-04-09 | 2010-09-22 | 武汉钢铁(集团)公司 | 耐低温冲击的热轧u型钢板桩用钢及其生产方法 |
JP2019505672A (ja) * | 2015-12-22 | 2019-02-28 | ポスコPosco | Pwht抵抗性に優れた低温圧力容器用鋼板及びその製造方法 |
CN115058656A (zh) * | 2022-06-30 | 2022-09-16 | 马鞍山钢铁股份有限公司 | 一种寒冷环境下服役的弹性车轮用轮箍及其热处理工艺 |
CN115058656B (zh) * | 2022-06-30 | 2023-08-11 | 马鞍山钢铁股份有限公司 | 一种寒冷环境下服役的弹性车轮用轮箍及其热处理工艺 |
CN116482139A (zh) * | 2023-06-21 | 2023-07-25 | 宁德时代新能源科技股份有限公司 | 电池疲劳强度确定方法、装置、计算机设备和存储介质 |
CN116482139B (zh) * | 2023-06-21 | 2023-09-19 | 宁德时代新能源科技股份有限公司 | 电池疲劳强度确定方法、装置、计算机设备和存储介质 |
Also Published As
Publication number | Publication date |
---|---|
CN1113391A (zh) | 1995-12-13 |
NO951288L (no) | 1995-06-06 |
NO951288D0 (no) | 1995-04-03 |
EP0666332A4 (en) | 1995-12-13 |
CN1040555C (zh) | 1998-11-04 |
JP3526576B2 (ja) | 2004-05-17 |
KR950703661A (ko) | 1995-09-20 |
KR0157540B1 (ko) | 1998-11-16 |
EP0666332A1 (en) | 1995-08-09 |
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