HIGH TENSILE STRENGTH STEEL HAVING FAVORABLE DELAYED FRACTURE RESISTANCE AND METHOD FOR MANUFACTURING THE SAME

Information

  • Patent Application
  • 20100024926
  • Publication Number
    20100024926
  • Date Filed
    January 31, 2008
    16 years ago
  • Date Published
    February 04, 2010
    14 years ago
Abstract
High tensile strength steels that have both favorable delayed fracture resistance and a tensile strength of 600 MPa or higher and are suitably used in construction machinery, tanks, penstocks, and pipelines, as well as methods for manufacturing such steels are provided. The safety index of delayed fracture resistance (%) is 100×(X1/X0), where X0: reduction of area of a specimen substantially free from diffusible hydrogen, and X1: reduction of area of a specimen containing diffusible hydrogen.
Description
TECHNICAL FIELD

This disclosure relates to high tensile strength steels having favorable delayed fracture resistance and those having favorable delayed fracture resistance with the tensile strength thereof being 600 MPa or higher, in particular, 900 MPa or higher, as well as methods for manufacturing such steels.


BACKGROUND

Recently, in the fields involving the use of steels, such as construction machinery (e.g., moves and chassis for cranes), tanks, penstocks, and pipelines, the increasing size of structures urges steels to be stronger and also the use environment of such steels has been becoming progressively harsher.


However, strengthening of steels and a harsher use environment are generally known to increase the susceptibility of steels to delayed fractures. For example, in the field of high tensile bolts, JIS (Japanese Industrial Standards) B 1186 stipulates that the use of F11T bolts (tensile strength: 1100 to 1300 N/mm2) should be avoided whenever possible, indicating that the use of high strength steels is limited.


In response to this, methods for manufacturing steels with favorable delayed fracture resistance have been proposed in publications including Japanese Unexamined Patent Application Publication No. H3-243745, Japanese Unexamined Patent Application Publication No. 2003-73737, Japanese Unexamined Patent Application Publication No. 2003-239041, Japanese Unexamined Patent Application Publication No. 2003-253376, and Japanese Unexamined Patent Application Publication No. 2003-321743. These methods are based on various techniques, such as optimization of components, strengthening of grain boundaries, decreasing the size of crystal grains, the use of hydrogen-trapping sites, control of structural morphology, and fine dispersion of carbides.


However, the methods described in the publications listed above, including Japanese Unexamined Patent Application Publication No. H3-243745, Japanese Unexamined Patent Application Publication No. 2003-73737, Japanese Unexamined Patent Application Publication No. 2003-239041, Japanese Unexamined Patent Application Publication No. 2003-253376, and Japanese Unexamined Patent Application Publication No. 2003-321743, do not produce sufficiently strong steels achieving a delayed fracture resistance level that is required in applications where they are exposed to a severely corrosive environment. Thus, steels having both better delayed fracture resistance and a high level of tensile strength, in particular, a tensile strength of 900 MPa or higher, and methods for manufacturing such steels are demanded.


Delayed fractures reportedly occur when hydrogen able to diffuse in steel at room temperature, namely so-called “diffusible hydrogen,” gathers at a stress concentration zone and reaches the threshold limit value of the material. This threshold limit value depends on material strength, its structure, and other parameters.


In general, a delayed fracture of high strength steels starts from non-metallic inclusions, such as MnS, and grows along grain boundaries, such as prior austenite grain boundaries.


Thus, ways of improving delayed fracture resistance include reduction of the amount of non-metallic inclusions, such as MnS, and strengthening of prior austenite grain boundaries.


It could therefore be helpful to provide a high tensile strength steel having delayed fracture resistance better than that of known steels with the tensile strength thereof being 600 MPa or higher, in particular, 900 MPa or higher, as well as a method for manufacturing such a steel.


SUMMARY

We discovered that high tensile strength steels having delayed fracture resistance better than those of known steels can be obtained by the following principles: reduction of the amount of P and S that are impurity elements as well as extension of crystal grains and introduction of deformation bands via rolling of non-recrystallization regions can prevent the formation of MnS, non-metallic inclusions; a decrease in the covering density of grain boundaries of P, which is an impurity element, segregated in prior austenite grain boundaries, which may be followed by reduction of the amount of cementite precipitations formed in the boundaries of laths, can prevent a decrease in the strength of the prior austenite grain boundaries.


We thus provide:

    • 1. A high tensile strength steel having favorable delayed fracture resistance, containing elements C: 0.02 to 0.25%, Si: 0.01 to 0.8%, Mn: 0.5 to 2.0%, Al: 0.005 to 0.1%, N: 0.0005 to 0.008%, P: 0.02% or lower, and S: 0.004% or lower, all in percent by mass, and Fe and unavoidable impurities as the balance, wherein the average aspect ratio of prior austenite grains calculated over the entire thickness is at least three;
    • 2. The high tensile strength steel according to 1, wherein S: 0.003% or lower and the cementite covering ratio measured at boundaries of laths is 50% or lower;
    • 3. The high tensile strength steel having favorable delayed fracture resistance according to 1 or 2, further containing one or more of Mo: 1% or lower, Nb: 0.1% or lower, V: 0.5% or lower, Ti: 0.1% or lower, Cu: 2% or lower, Ni: 4% or lower, Cr: 2% or lower, and W: 2% or lower, all in percent by mass;
    • 4. The high tensile strength steel having favorable delayed fracture resistance according to 1 to 3, further containing one or more of B: 0.003% or lower, Ca: 0.01% or lower, REM: 0.02% or lower, and Mg: 0.01% or lower;
    • 5. The high tensile strength steel having. favorable delayed fracture resistance according to any one of 1 to 4, wherein, hydrogen is charged into the steel and the hydrogen contained in the steel is sealed by zinc galvanizing, the safety index of delayed fracture resistance calculated using the formula described below being at least 75% when a slow strain rate test is performed with the strain rate set to 1×10−3/s or lower:





Safety index of delayed fracture resistance (%)=100×(X1/X0)

    • where X0: reduction of area of a specimen substantially free from diffusible hydrogen, and
    • X1: reduction of area of a specimen containing diffusible hydrogen;
    • 6. The high tensile strength steel according to 5, wherein the safety index of delayed fracture resistance is at least 80%;
    • 7. A method for manufacturing the high tensile strength steel having favorable delayed fracture resistance according to 5, including a step of casting steel having the composition according to any one of 1 to 4, a step of protecting the steel from cooling to the Ar3 transformation temperature or lower or heating the steel to a temperature equal to or higher than the Ac3 transformation temperature once again, a step of hot rolling to achieve a predetermined steel thickness including rolling conducted with the rolling reduction for non-recrystallization regions set to 30% or higher, a step of cooling the steel from a temperature equal to or higher than the Ar3 transformation temperature to a temperature equal to or lower than 350° C. at a cooling rate of 1° C./s or higher, and a step of tempering the steel at a temperature equal to or lower than the Ac1 transformation temperature;
    • 8. The method according to 7, in which the steel is tempered at a temperature equal to or lower than the Ac1 transformation temperature, for manufacturing the high tensile strength steel having favorable delayed fracture resistance according to 6, wherein a heating apparatus installed in a manufacturing line having a rolling mill and a cooling apparatus is used to heat the steel from 370° C. to a predetermined tempering temperature equal to or lower than the Ac1 transformation while maintaining the average heating rate for heating the middle of the steel thickness at 1° C./s or higher so that the maximum tempering temperature at the middle of the steel thickness is 400° C. or higher; and
    • 9. The method according to 8, in which the steel is tempered at a temperature equal to or lower than the Ac1 transformation temperature, for manufacturing the high tensile strength steel having favorable delayed fracture resistance according to 6, wherein the steel is heated from a tempering initiation temperature to 370° C. with the average heating rate for heating the middle of the steel thickness maintained at 2° C./s or higher.


We enable manufacturing high tensile strength steels having excellent delayed fracture resistance with the tensile strength thereof being 600 MPa or higher, in particular, 900 MPa or higher, and thus has very high industrial applicability.





BRIEF DESCRIPTION OF THE DRAWINGS


FIG. 1: A schematic diagram of a martensite structure.



FIG. 2: Schematic diagrams and transmission electron microscope (TEM) images (extracted replicas) showing cementite precipitations formed in the boundaries of laths during slow-heating tempering and rapid-heating tempering.





DETAILED DESCRIPTION
Component Compositions

The following are reasons for selection of the components. The percentages representing the content ratios of chemical components are all in percent by mass. C: 0.02 to 0.25%


C ensures strength. C contained at a content ratio lower than 0.02% would have an insufficient effect, whereas C contained at a content ratio higher than 0.25% would result in reduced toughness of the base material and weld-heat-affected zones and significantly deteriorated weldability. Therefore, the content ratio of C should be in the range of 0.02 to 0.25% and is preferably in the range of 0.05 to 0.20%.


Si: 0.01 to 0.8%

Si is used as a deoxidizing material and a reinforcing element in a steel-making process. Si contained at a content ratio lower than 0.01% would have an insufficient effect, whereas Si contained at a content ratio higher than 0.8% would make grain boundaries brittle, thereby promoting the development of delayed fractures. Therefore, the content ratio of Si should be in the range of 0.01 to 0.8% and is preferably in the range of 0.1 to 0.5%.


Mn: 0.5 to 2.0%

Mn ensures strength and, during the tempering step, is concentrated in cementite to prevent coarsening thereof by diffusing as substitutional atoms to limit the cementite growth rate. Mn contained at a content ratio lower than 0.5% would have an insufficient effect, whereas Mn contained at a content ratio higher than 2.0% would result in reduced toughness of weld-heat-affected zones and significantly deteriorated weldability. Therefore, the content ratio of Mn should be in the range of 0.5 to 2.0% and is preferably in the range of 0.7 to 1.8%.


Al: 0.005 to 0.1%

Al is added as a deoxidizing material also having the effect of downsizing the diameters of crystal grains. Al contained at a content ratio lower than 0.005% would have an insufficient effect, whereas Al contained at a content ratio higher than 0.1% would increase the risk of surface flaws of resulting steels. Therefore, the content ratio of Al should be in the range of 0.005 to 0.1% and is preferably in the range of 0.01 to 0.05%.


N: 0.0005 to 0.008%

N binds to Ti or the like to form nitrides that reduce the size of resulting structures, thereby improving the toughness of the base material and weld-heat-affected zones. N contained at a content ratio lower than 0.0005% would result in insufficient downsizing of the resulting structures, whereas N contained at a content ratio higher than 0.008% would lead to an increased amount of a solid solution of N, thereby reducing the toughness of the base material and weld-heat-affected zones. Therefore, the content ratio of N should be in the range of 0.0005 to 0.008% and is preferably in the range of 0.001 to 0.005%.


P: 0.02% or Lower

P, which is an impurity element, is often segregated in crystal grain boundaries such as prior austenite grains during the tempering process. P contained at a content ratio higher than 0.02% would result in weakened bonds between adjacent crystal grains, thereby reducing low-temperature toughness and delayed fracture resistance. Therefore, the content ratio of P should be 0.02% or lower and is preferably 0.015% or lower.


S: 0.004% or Lower

S, which is an impurity element, often forms non-metallic inclusions, MnS. S contained at a content ratio higher than 0.004% would produce a vast amount of inclusions and thus reduce ductile fracture resistance, thereby deteriorating low-temperature toughness and delayed fracture resistance. Therefore, the content ratio of S should be 0.004% or lower and is preferably 0.003% or lower.


The following components may also be added if desired.


Mo: 1% or Lower

Mo has the effect of improving quenching properties and strength and forms carbides that trap diffusible hydrogen and enhance delayed fracture resistance. To achieve these effects, the content ratio of Mo is preferably 0.05% or higher. However, the addition of Mo at a content ratio higher than 1% would be uneconomic. Therefore, when Mo is added, the content ratio thereof should be 1% or lower and is preferably 0.8% or lower. It should be noted that Mo has the effect of improving temper softening resistance and thus, to ensure a strength of 900 MPa or higher, the content ratio thereof is preferably 0.2% or higher.


Nb: 0.1% or Lower

Nb is a microalloying element that improves strength, and forms carbides, nitrides, and carbonitrides that trap diffusible hydrogen and enhance delayed fracture resistance. To achieve these effects, the content ratio of Nb is preferably 0.01% or higher. However, the addition of Nb at a content ratio higher than 0.1% would result in reduced toughness of weld-heat-affected zones. Therefore, when Nb is added, the content ratio thereof should be 0.1% or lower and is preferably 0.05% or lower.


V: 0.5% or Lower

V is a microalloying element that improves strength, and forms carbides, nitrides, and carbonitrides that trap diffusible hydrogen and enhance delayed fracture resistance. To achieve these effects, the content ratio of V is preferably 0.02% or higher. However, the addition of V at a content ratio higher than 0.5% would result in reduced toughness of weld-heat-affected zones. Therefore, when V is added, the content ratio thereof should be 0.5% or lower and is preferably 0.1% or lower.


Ti: 0. 1% or Lower

When hot-rolled or welded, Ti forms TiN to prevent the growth of austenite grains, thereby improving the toughness of the base material and weld-heat-affected zones, and forms carbides, nitrides, and carbonitrides that trap diffusible hydrogen and enhance delayed fracture resistance. To achieve these effects, the content ratio of Ti is preferably 0.005% or higher. However, the addition of Ti at a content ratio higher than 0.1% would result in reduced toughness of weld-heat-affected zones. Therefore, when Ti is added, the content ratio thereof should be 0.1% or lower and is preferably 0.05% or lower.


Cu: 2% or Lower

Cu has the effect of improving strength through solid solution strengthening and precipitation strengthening. To achieve this effect, the content ratio of Cu is preferably 0.05% or higher. However, the addition of Cu at a content ratio higher than 2% would increase the risk of hot tearing that occurs during heating slabs or welding. Therefore, when Cu is added, the content ratio thereof should be 2% or lower and is preferably 1.5% or lower.


Ni: 4% or Lower

Ni has the effect of improving toughness and quenching properties. To achieve this effect, the content ratio of Ni is preferably 0.3% or higher. However, the addition of Ni at a content ratio higher than 4% would be uneconomic. Therefore, when Ni is added, the content ratio thereof should be 4% or lower and is preferably 3.8% or lower.


Cr: 2% or Lower

Cr has the effect of improving strength and toughness and is excellent in terms of high-temperature strength properties. Furthermore, during the tempering step, Cr is concentrated in cementite to prevent coarsening thereof by diffusing as substitutional atoms to limit the cementite growth rate. Thus, it is preferable to add Cr whenever possible for the purposes of improving strength, preventing coarsening of cementite, and, in particular, achieving a tensile strength of 900 MPa or higher, at a content ratio of 0.3% or higher. However, the addition of Cr at a content ratio higher than 2% would result in reduced weldability. Therefore, when Cr is added, the content ratio thereof should be 2% or lower and is preferably 1.5% or lower.


W: 2% or Lower

W has the effect of improving strength. To achieve this effect, the content ratio of W is preferably 0.05% or higher. However, the addition of W at a content ratio higher than 2% would result in reduced weldability. Therefore, when W is added, the content ratio thereof should be 2% or lower.


B: 0.003% or Lower

B has the effect of improving quenching properties. To achieve this effect, the content ratio of B is preferably 0.0003% or higher. However, the addition of B at a content ratio higher than 0.003% would result in reduced toughness. Therefore, when B is added, the content ratio thereof should be 0.003% or lower.


Ca: 0.01% or Lower

Ca is an element essential to control the morphology of sulfide inclusions. To achieve this effect, the content ratio of Ca is preferably 0.0004% or higher. However, the addition of Ca at a content ratio higher than 0.01% would result in reduced cleanliness and delayed fracture resistance. Therefore, when Ca is added, the content ratio thereof should be 0.01% or lower.


REM: 0.02% or Lower

REM (note: REM is an abbreviation representing Rare Earth Metal) forms REM (rare-earth metal) oxysulfides, namely REM (O, S), in steel to reduce the amount of solid solution S at crystal grain boundaries, thereby improving SR (stress relief) cracking resistance (in other words, PWHT (post welded heat treatment) cracking resistance). To achieve this effect, the content ratio of REM is preferably 0.001% or higher. However, the addition of REM at a content ratio higher than 0.02% would cause material deterioration due to significant deposition of REM oxysulfides on precipitated crystal bands. Therefore, when REM is added, the content ratio thereof should be 0.02% or lower.


Mg: 0.01% or Lower

Mg is used as a hot metal desulfurization agent in some cases. To achieve this effect, the content ratio of Mg is preferably 0.001% or higher. However, the addition of Mg at a content ratio higher than 0.01% would result in reduced cleanliness. Therefore, when Mg is added, the content ratio thereof should be 0.01% or lower.


Microstructure

The following are reasons for selection of the microstructure.


The representative structures of the high strength steel are martensite and bainite. In particular, a martensite structure has, as shown in the schematic structure diagram of FIG. 1, a fine and complex morphology in which a plurality of four kinds of characteristic structure units (prior austenite, packets, blocks, and laths) are layered. The packets described herein are defined as regions each consisting of a population of parallel laths having the same habit plane. The blocks consist of a population of parallel laths having the same orientation.


The average aspect ratio of prior austenite grains calculated over the entire steel thickness (in FIG. 1, the ratio a/b between the major axis a and the minor axis b of the prior austenite grain) is at least three and preferably at least four.


The aspect ratio of prior austenite grains being at least three reduces the grain boundary covering ratio of P segregated in prior austenite grain boundaries, packet boundaries, or the like, thereby improving low-temperature toughness and delayed fracture resistance, and such microstructures distributing over the entire steel thickness provide homogenous steel having the properties described above.


To measure the aspect ratio of prior austenite grains, prior austenite grains are developed using, for example, picric acid, and then image analysis is performed to simply average aspect ratios of, for example, 500 or more prior austenite grains.


The state in which the average aspect ratio of prior austenite grains calculated over the entire thickness is at least three means that the average aspect ratio calculated from values obtained at the following positions is at least three and preferably at least four: 1 mm in depth from the surface of steel, positions located at ¼, ½, and ¾ of the steel thickness, and 1 mm in depth from the back surface of the steel.


In addition to the findings described above, we found that reducing the ratio of cementite precipitating in the boundaries between many fine laths generated in the blocks illustrated in FIG. 1 (hereinafter, referred to as the cementite covering ratio of lath boundaries) to 50% or lower particularly prevents a decrease in the strength. of prior austenite grain boundaries and thus improves delayed fracture resistance. Preferably, the cementite covering ratio of lath boundaries is 30% or lower. FIG. 2 includes schematic diagrams and TEM images showing cementite precipitations formed in the boundaries of laths.


The cementite covering ratio of lath boundaries is determined by imaging a structure developed using nital (a solution of nitric acid and an alcohol) with a scanning electron microscope as shown in FIG. 2; analyzing, for example, 50 or more laths in the obtained image in terms of the lengths of formed cementite precipitations along the lath boundaries (LCementite) and the lengths of the lath boundaries (LLath); dividing the sum of the lengths of cementite along the lath boundaries by the sum of the lengths of the lath boundaries; and then multiplying the quotient by 100.


Safety Index of Delayed Fracture Resistance

Hydrogen is charged into the steel and the hydrogen contained in the steel is sealed by zinc galvanizing, the safety index of delayed fracture resistance calculated using the formula described below being at least 75% and preferably at least 80% when a slow strain rate test is performed with the strain rate set to 1×10−3/s or lower:





Safety index of delayed fracture resistance (%)=100×(X1/X0)

    • where X0: reduction of the area of a specimen substantially free from diffusible hydrogen, and
    • X1: reduction of the area of a specimen containing diffusible hydrogen.


The safety index of delayed fracture resistance is a quantitative measure of delayed fracture resistance of steel, and the higher this index is, the better the delayed fracture resistance is. In the practical use of steel under normal atmospheric conditions, the safety index of delayed fracture resistance for sufficiently high delayed fracture resistance is 75% or higher and preferably 80% or higher. In some cases, however, steels having a tensile strength less than 1200 MPa would be used under harsh conditions such as a corrosive environment and lower temperatures or be difficult to process. Therefore, it is desirable that the safety index of delayed fracture resistance is 80% or higher and more preferably 85% or higher.


Manufacturing Conditions

We provide various forms of steels such as steel plates, steel shapes, and steel bars. The temperature specifications described in the manufacturing conditions are applicable to temperatures measured at the center of steel. As for steel plates, the center of the steel is taken as the middle of the steel thickness. As for steel shapes, it is taken as the middle of the steel thickness measured at a site to which selected properties are given. As for steel bars, it is taken as the middle of diameter. It should be noted that the surroundings of the center of steel experience temperature changes similar to those at the center, and thus the scope of the temperature specifications is not limited to the center itself


Cast Conditions

Our steels are effective regardless of casting conditions used to manufacture steels, and thus particular limitations on cast conditions are unnecessary. Any method can be used in manufacturing of cast slabs from liquid steel and rolling of the cast slabs to produce billets. Examples of methods that can be used to melt steel include converter processes and electric furnace processes, and examples of methods that can be used to produce slabs include continuous casting and ingot-based methods.


Hot-Rolling Conditions

In rolling of cast slabs to produce billets, the cast slabs may be protected from cooling to the Ar3 transformation temperature or lower or allowed to cool and then heated to a temperature equal to or higher than the Ac3 transformation temperature once again before the start of hot rolling. This is because effectiveness is ensured whenever rolling is started as long as the temperature at that time is in the range described above.


The rolling reduction for non-recrystallization regions is 30% or higher and preferably 40% or higher, and rolling is finished at a temperature equal to or higher than the Ar3 transformation temperature. The reason why non-recrystallization regions are rolled with the rolling reduction being 30% or higher is because hot rolling performed in this way leads to extension of austenite grains and, at the same time, introduces deformation bands, thereby reducing the grain boundary covering ratio of P segregated in the grain boundaries during the tempering process. Higher aspect ratios of prior austenite grains would reduce effective grain sizes (sizes of grains that are fracture appearance units or, more specifically, packets) and the grain boundary covering ratios of P covering the prior austenite grains, packet boundaries, or the like, thereby improving delayed fracture resistance.


No particular limitation is imposed on formulae used to calculate the Ar3 transformation temperature (° C.) and the Ac3 transformation temperature (° C.). For example, Ar3=910−310C−80Mn−20Cu−15Cr−55Ni−80Mo, and Ac3=854−180C+44Si−14Mn−17.8Ni−1.7Cr. In these formulae, each of the elements represents the content ratio (percent by mass) thereof in the steel.


Post-Hot-Rolling Cooling Conditions

After the completion of hot rolling, the steel is forcedly cooled from a temperature equal to or higher than the Ar3 transformation temperature to a temperature of 350° C. or lower at a cooling rate of 1° C./s or higher to ensure the strength and toughness of the base material. The reason why the forced-cooling initiation temperature is equal to or higher than the Ar3 transformation temperature is because steel plates should consist of austenite phases only in the start of cooling. Cooling started when the temperature is lower than the Ar3 transformation temperature would result in unevenly tempered structures and reduced toughness and delayed fracture resistance. The reason why steel plates are cooled to a temperature of 350° C. or lower is because such a low temperature is required to complete transformation from austenite to martensite or bainite, thereby improving the toughness and delayed fracture resistance of the base material. The cooling rate used in this process is 1° C./s or higher and preferably 2° C./s or higher. It should be noted that the cooling rate is defined as the average cooling rate obtained by dividing the temperature difference required in cooling the steel after hot rolling it from a temperature equal to or higher than the Ar3 transformation temperature to a temperature of 350° C. or lower by the time required in this cooling process.


Tempering Conditions

The tempering process is performed at a certain temperature that makes the maximum temperature at the middle of the steel thickness equal to or lower than the Ac1 transformation temperature. The reason why the maximum temperature should be equal to or lower than the Ac1 transformation temperature is because, when it exceeds the Ac1 transformation temperature, austenite transformation significantly reduces strength. Meanwhile, in this tempering process, an on-line heating apparatus installed in a manufacturing line having a rolling mill and a cooling apparatus and after the cooling apparatus is preferably used. This shortens the time required in the process including rolling, quenching, and tempering, thereby improving the productivity.


In this tempering process, the heating rate is preferably 0.05° C./s or higher. A heating rate lower than 0.05° C./s would increase the amount of P segregated in prior austenite grains, packet boundaries, or the like during tempering, thereby deteriorating low-temperature toughness and delayed fracture resistance. In addition, in slow heating where the heating rate for tempering is 2° C./s or lower, the time for which the tempering temperature is maintained is preferably 30 min or shorter because such a tempering time would prevent the growth of precipitations such as cementite and improve the productivity.


More preferred tempering conditions are rapid-heating conditions where the average heating rate for heating the middle of the steel thickness from 370° C. to a certain temperature equal to or lower than the Ac1 transformation temperature is 1° C./s or higher and the maximum temperature at the middle of the steel thickness is 400° C. or higher.


The reason why the average heating rate is 1° C./s or higher is because such a heating rate would reduce the grain boundary covering density of P, an impurity element segregated in prior austenite grain boundaries, packet boundaries, or the like, and achieve lath boundaries with a reduced amount of cementite precipitations, which are shown in FIG. 2 providing the comparison between the slow-heating tempering and the rapid-heating tempering in terms of the schematic diagram and the TEM image showing cementite precipitations formed in the boundaries of laths.


More effective prevention of grain boundary segregation of P in prior austenite grain boundaries, packet boundaries, or the like would be preferably achieved by performing rapid heating where the average heating rate at the middle of the steel thickness for heating from the tempering initiation temperature to 370° C. is 2° C./s or higher in addition to the above-described rapid heating process, where the average heating rate at the middle of the steel thickness for heating from 370° C. to a certain tempering temperature equal to or lower than the Ac1 transformation temperature is 1° C./s or higher.


The reason why the average heating rate at the middle of the steel thickness for heating from the tempering initiation temperature to 370° C. is 2° C./s or higher is because segregation of P in prior austenite grain boundaries, packet boundaries, or the like is particularly promoted in this temperature range.


Meanwhile, when the average heating rate at the middle of the steel thickness for heating from 370° C. to a certain tempering temperature equal to or lower than the Ac1 transformation temperature is 1° C./s or higher and the average heating rate at the middle of the steel thickness for heating from the tempering initiation temperature to 370° C. is 2° C./s or higher, the time for which the tempering temperature is maintained is preferably 60 s or shorter because such a tempering time would prevent a decrease in productivity and deterioration of delayed fracture resistance due to coarsening of precipitations such as cementite. In addition, the heating rate is defined as the average heating rate obtained by dividing the temperature difference required in reheating the steel to a certain temperature so that the maximum temperature at the middle of the steel thickness is equal to or lower than the Ac1 transformation temperature after cooling it by the time required in this reheating process.


The average cooling rate for cooling the tempered steel from the tempering temperature to 200° C. is preferably 0.05° C./s or higher to prevent coarsening of precipitations during this cooling process.


Meanwhile, the heating method for tempering may be induction heating, energization heating, infra-red radiant heating, furnace heating, or any other heating method.


The tempering apparatus may be a heating apparatus installed in a manufacturing line that is different from one having a rolling mill and a direct quenching apparatus or that installed in a manufacturing line having a rolling mill and a direct quenching apparatus so as to be directly connected to them. None of these heating apparatuses spoils the advantageous effect.


Example 1

Tables 1 and 2 show the chemical compositions of the steels used in this example, whereas Tables 3 and 4 show the steel manufacturing conditions and aspect ratios of prior austenite grains.


Steels A to Z and AA to II whose chemical compositions are shown in Tables 1 and 2 were melted and cast into slabs (slab dimensions: 100 mm in height×150 mm in width×150 mm in length). The obtained slabs were heated in a furnace to the heating temperatures shown in Tables 3 and 4 and then hot-rolled with the rolling reduction for non-recrystallization regions set to the values shown in Tables 3 and 4 to produce steel plates. After the hot-rolling process, the steel plates were directly quenched with the direct quenching initiation temperatures, direct quenching termination temperatures, and cooling rates set to the values shown in Tables 3 and 4 and then tempered using solenoid type induction heating apparatus with the tempering initiation temperatures, tempering temperatures, and tempering times set to the values shown in Tables 3 and 4. The direct quenching was completed by forcedly cooling (cooling in water) the individual steel plates to a temperature of 350° C. or lower at a cooling rate of 1° C./s or higher.


The average heating rates at the middle of the steel thickness were achieved by controlling the threading rates of the steel plates. In addition, each steel plate was moved back and forth in the solenoid type induction heating apparatus while being heated so that its temperature was maintained in the range ±5° C. of the target heating temperature.


The cooling process after heating for tempering was completed by performing air cooling under the conditions shown in Tables 3 and 4. The temperatures, such as tempering temperatures and quenching temperatures, at the middle of the thickness of each steel plate were determined by heat transfer calculation based on temperatures dynamically measured on the surface thereof using an emission pyrometer.


Tables 5 and 6 show the yield strength, tensile strength, fracture appearance transition temperatures (vTrs), and safety indices of delayed fracture resistance of the obtained steel plates.


Each cooling rate was the average cooling rate for cooling from the direct quenching initiation temperature to the direct quenching termination temperature measured at the middle of the thickness of the steel plate.


For the tests described later, three specimens were sampled from the midpoint of the longitudinal axis of each steel plate, and additional three specimens were sampled from the position located at ¼ of the width of each steel plate.


The aspect ratios of prior austenite grains were determined by etching the structures of the specimens with picric acid, imaging each specimen using an optical microscope at 1 mm in depth from the surface thereof, positions located at ¼, ½, and ¾ of the thickness thereof, and 1 mm in depth from the back surface thereof, measuring the aspect ratios of approximately 500 prior austenite grains, and then averaging the aspect ratio measurements.


The yield strength and tensile strength were measured using specimens for the overall thickness tensile test according to JIS Z2241. The toughness was evaluated using the Charpy pendulum impact test according to JIS Z2242, in which vTrs of specimens sampled from the middle of the thickness of each steel plate was measured.


The safety indices of delayed fracture resistance were evaluated using rod-like specimens in the following way: hydrogen was charged into the specimens by cathodic hydrogen charging so that the amount of diffusible hydrogen contained in each specimen was approximately 0.5 mass ppm; the hydrogen was sealed by zinc galvanizing of the surface of each specimen; tensile tests of the specimens were performed with the strain rate set to 1×10−6/s and the reductions of area of the fractured specimens were measured; and then the same tensile tests were performed using other specimens, into which no hydrogen was charged. The obtained results were used to evaluate the safety indices of delayed fracture resistance in accordance with the following formula:





Safety index of delayed fracture resistance (%)=100×(X1/X0)

    • where X0: reduction of area of a specimen substantially free from diffusible hydrogen, and
    • X1: reduction of area of a specimen containing diffusible hydrogen.


The target vTrs was set to −40° C. or lower for steels having a tensile strength less than 1200 MPa and −30° C. or lower for steels having a tensile strength of 1200 MPa or higher. On the other hand, the target safety index of delayed fracture resistance was set to 80% or higher for steels having a tensile strength less than 1200 MPa and 75% or higher for steels having a tensile strength of 1200 MPa or higher.


As is clear in Tables 3 and 4, the steel plates 18 to 20, in which the rolling reduction for non-recrystallization regions deviated from our range, had the aspect ratios of prior austenite grains deviating from our range.


Furthermore, as is clear in Tables 5 and 6, the steel plates 1 to 17 and 33 to 39 (our examples) were produced under manufacturing conditions falling within our range to have a chemical component and the aspect ratio of prior austenite grains falling within our ranges, and showed favorable vTrs and a high safety index of delayed fracture resistance.


However, in the comparative steel plates 18 to 32 and 40 to 44 (comparative examples), at least one of vTrs and the safety index of delayed fracture resistance deviated from the target range thereof described above. The following are specific explanations of these comparative examples.


The steel plates 29 to 32 and 40 to 44 produced with the composition deviating from our range showed vTrs and/or the safety index of delayed fracture resistance being short of the target value.


The steel plates 18 to 20 produced with the rolling reduction for non-crystallization regions deviating from our range showed the safety index of delayed fracture resistance being short of the target value.


The steel plates 21 to 23 produced with the direct quenching initiation temperature deviating from our range showed vTrs and the safety index of delayed fracture resistance being short of the target value.


The steel plate 24 produced with the direct quenching termination temperature deviating from our range showed vTrs and the safety index of delayed fracture resistance being short of the target value.


The steel plate 25 produced with the cooling rate and direct quenching termination temperature deviating from our ranges showed vTrs and the safety index of delayed fracture resistance being short of the target value.


The steel plates 26 to 28 produced with the tempering temperature deviating from our range showed vTrs and the safety index of delayed fracture resistance being short of the target value.


Example 2

As with those produced in Example 1, steel plates were produced. More specifically, Steels A to Z and AA to II whose chemical compositions are shown in Tables 7 and 8 were melted and cast into slabs, and the obtained slabs were heated in a furnace and then hot-rolled to produce the steel plates. After the hot-rolling process, the steel plates were directly quenched and then tempered using solenoid type induction heating apparatus. The direct quenching was completed by forcedly cooling (cooling in water) the individual steel plates to a temperature of 350° C. or lower at a cooling rate of 1° C./s or higher.


The aspect ratios of prior austenite grains were determined in the same manner as Example 1, except that approximately 550 prior austenite grains were used to calculate the average aspect ratio.


The cementite covering ratios of lath boundaries were determined by imaging structures etched using nital with a scanning electron microscope at the position located at ¼ of the thickness of each specimen; analyzing the boundaries of approximately 60 laths in terms of the lengths of formed cementite precipitations along the lath boundaries (LCementite) and the lengths of the lath boundaries (LLath); dividing the sum of the lengths of cementite along the lath boundaries by the sum of the lengths of the lath boundaries; and then multiplying the quotient by 100.


Additionally, the yield strength, tensile strength, and safety indices of delayed fracture resistance were determined in the same manner as Example 1.


The target vTrs was set to −40° C. or lower for steels having a tensile strength less than 1200 MPa and −30° C. or lower for steels having a tensile strength of 1200 MPa or higher. On the other hand, the target safety index of delayed fracture resistance was set to 85% or higher for steels having a tensile strength less than 1200 MPa and 80% or higher for steels having a tensile strength of 1200 MPa or higher.


Tables 9 and 10 show the manufacturing conditions, aspect ratios of prior austenite grains, and cementite covering ratios of laths of the individual steel plates, and Tables 11 and 12 show the yield strength, tensile strength, fracture appearance transition temperatures (vTrs), and safety indices of delayed fracture resistance of the obtained steel plates.


It should be noted that, in Tables 9 to 12, our examples consist of steel plates meeting our requirements, whereas the comparative examples consist of those deviating from those requirements. The steel plates 1 to 17 and 41 to 47 are our examples in which the heating rate for heating from the tempering initiation temperature to 370° C. was 2° C./s or higher.


The steel plates 35 and 36 are close to our requirements, namely the requirement that the heating rate for heating from the tempering initiation temperature to 370° C. should be 2° C./s or higher and they meet others of our requirements and thus are classified into our examples.


As is clear in Tables 9 and 10, the steel plates 18 to 20, in which the rolling reduction for non-recrystallization regions deviated from our range, had the aspect ratio of prior austenite grains and cementite covering ratios of laths deviating from our ranges.


The steel plates 26 to 28 produced with the tempering temperature deviating from our range showed the cementite covering ratio of laths deviating from our range.


Furthermore, the steel plates 30 and 32 to 34 produced with the average heating rate for heating the middle of the steel thickness from the tempering initiation temperature to 370° C. and/or the average heating rate for heating the middle of the steel thickness from 370° C. to the tempering temperature deviating from our ranges showed the cementite covering ratio of laths deviating from our range.


Meanwhile, as is clear in Tables 11 and 12, the steel plates 1 to 17, 35, and 36 (our examples) were produced under manufacturing conditions falling within our range to have a chemical composition, the aspect ratio of prior austenite grains, and the cementite covering ratio of laths falling within our ranges, and showed favorable vTrs and a high safety index of delayed fracture resistance.


The comparison between the steel plates 4 and 35, both of which fall within our scope and are identical to each other except for the difference in the average heating rate for heating the middle of the steel thickness from the tempering initiation temperature to 370° C., revealed that the steel plate 4 produced with the average heating rate for heating the middle of the steel thickness from the tempering initiation temperature to 370° C. being higher than 2° C./s was better in terms of vTrs and the safety index of delayed fracture resistance than the steel plate 35. This is the case also for the comparison between the steel plates 12 and 36.


However, in the comparative steel plates 18 to 34, 37 to 46, and 48 to 52 (comparative examples), at least one of vTrs and the safety index of delayed fracture resistance deviated from the target range thereof described above. The following are specific explanations of these comparative examples.


The steel plates 37 to 40 and 48 to 52 produced with the composition deviating from our range showed vTrs and the safety index of delayed fracture resistance being short of the target value.


The steel plates 18 to 20 produced with the rolling reduction for non-crystallization regions deviating from our range showed the safety index of delayed fracture resistance being short of the target value.


The steel plates 21 to 23 produced with the direct quenching initiation temperature deviating from our range showed vTrs and/or the safety index of delayed fracture resistance being short of the target value.


The steel plates 24 and 25 produced with the direct quenching termination temperature deviating from our range showed vTrs being short of the target value.


The steel plates 26 to 28 produced with the tempering temperature deviating from our range showed vTrs and/or the safety index of delayed fracture resistance being short of the target value.


The steel plates 29 to 34 produced with the average heating rate for heating the middle of the steel thickness from 370° C. to the tempering temperature deviating from our range showed vTrs and/or the safety index of delayed fracture resistance being short of the target value.


INDUSTRIAL APPLICABILITY

The steels disclosed herein are high tensile strength steels having excellent delayed fracture resistance with the tensile strength thereof being 600 MPa or higher, in particular, 900 MPa or higher, and thus has very high industrial applicability.









TABLE 1





(mass %)



























Steels
C
Si
Mn
P
S
Cu
Ni
Cr
Mo
Nb
V
Ti





A
0.05
0.19
1.34
0.011
0.0019
0.00
0.00
0.03
0.05
0.020
0.034
0.000


B
0.08
0.26
1.43
0.018
0.0022
0.00
0.00
0.03
0.19
0.021
0.035
0.000


C
0.10
0.31
1.08
0.014
0.0038
0.00
0.00
0.06
0.09
0.019
0.008
0.010


D
0.12
0.38
1.48
0.014
0.0018
0.02
0.01
0.49
0.38
0.017
0.041
0.012


E
0.12
0.40
1.51
0.012
0.0019
0.02
0.01
0.26
0.40
0.020
0.000
0.010


F
0.13
0.41
1.51
0.014
0.0023
0.00
0.00
0.51
0.41
0.020
0.042
0.013


G
0.14
0.41
1.55
0.014
0.0022
0.00
1.09
0.50
0.43
0.020
0.000
0.011


H
0.15
0.41
1.52
0.014
0.0019
0.30
0.30
0.51
0.21
0.020
0.042
0.013


I
0.15
0.41
1.21
0.014
0.0037
0.00
0.00
0.51
0.69
0.020
0.000
0.013


J
0.16
0.42
1.19
0.005
0.0019
0.26
0.28
0.34
0.65
0.019
0.044
0.012


K
0.16
0.27
1.35
0.002
0.0009
0.26
0.24
0.53
0.52
0.022
0.052
0.013


L
0.17
0.37
1.12
0.009
0.0010
0.05
0.06
0.51
0.69
0.022
0.041
0.012


M
0.17
0.20
1.35
0.005
0.0018
0.00
0.40
0.35
0.25
0.022
0.050
0.000


N
0.17
0.22
1.45
0.015
0.0009
0.00
1.32
0.35
0.21
0.015
0.035
0.000


O
0.18
0.35
1.75
0.004
0.0007
0.20
0.20
0.45
0.30
0.019
0.008
0.010


P
0.21
0.33
1.09
0.014
0.0012
0.02
0.01
0.55
0.69
0.020
0.041
0.012












Remarks

























Ar3
Ac1



Steels
B
W
Ca
REM
Mg
Al
T.N
(° C.)
(° C.)
Remarks





A
0.0000




0.031
0.0032
783
709
Example


B
0.0000




0.028
0.0029
755
709
Example


C
0.0010




0.022
0.0037
785
716
Example


D
0.0012

0.0017


0.030
0.0030
716
722
Example


E
0.0013




0.027
0.0031
715
717
Example


F
0.0010




0.032
0.0037
708
723
Example


G
0.0015




0.024
0.0024
641
706
Example


H
0.0010




0.032
0.0030
695
718
Example


I
0.0010


0.0025

0.032
0.0030
704
727
Example


J
0.0012



0.0015
0.028
0.0046
688
719
Example


K
0.0015

0.0032


0.052
0.0035
684
719
Example


L
0.0013

0.0019


0.027
0.0037
701
726
Example


M
0.0000


0.0019

0.031
0.0032
702
711
Example


N
0.0000




0.028
0.0029
647
697
Example


O
0.0010
0.20



0.022
0.0037
668
714
Example


P
0.0012

0.0015


0.030
0.0030
693
728
Example





Note 1:


The symbol * means that the parameter deviates from the range specified in the present invention.


Note 2:


Ar3 = 91-310C—80Mn—20Cu—15Cr—55Ni—80Mo (the elements represent content ratios in mass percent)


Note 3:


Ac1 = 723-14Mn + 22Si—14.4Ni + 23.3Cr (the elements represent content ratios in mass percent)













TABLE 2





(mass %)




























Steels
C
Si
Mn
P
S
Cu
Ni
Cr
Mo
Nb
V
Ti
B





Q
0.23
0.45
1.52
0.018
0.0015
0.02
1.34
0.45
0.45
0.020
0.000
0.010
0.0013


R
0.12
0.38
1.48
0.025*
0.0018
0.02
0.01
0.49
0.38
0.017
0.041
0.012
0.0012


S
0.14
0.41
1.55
0.014
0.0043*
0.00
1.09
0.50
0.43
0.020
0.000
0.011
0.0015


T
0.15
0.41
1.52
0.031*
0.0019
0.30
0.30
0.51
0.21
0.020
0.042
0.013
0.0010


U
0.17
0.37
1.12
0.032*
0.0042*
0.05
0.06
0.51
0.69
0.022
0.041
0.012
0.0013


X
0.03
0.26
1.31
0.010
0.0009
0.01
0.03
0.56
0.05
0.012
0.031
0.001
0.0003


Y
0.17
0.67
1.81
0.006
0.0008
1.98
3.91
0.63
0.72
0.018
0.043
0.012
0.0015


Z
0.24
0.32
1.92
0.003
0.0006
1.95
3.95
0.51
0.95
0.016
0.042
0.015
0.0013


AA
0.18
0.02
1.12
0.005
0.0003
1.66
3.81
0.36
0.86
0.022
0.045
0.012
0.0010


BB
0.20
0.75
1.08
0.006
0.0004
1.82
3.56
0.48
0.89
0.019
0.046
0.012
0.0011


CC
0.23
0.41
0.60
0.004
0.0003
1.91
3.78
0.39
0.88
0.021
0.045
0.010
0.0013


DD
0.15
0.42
1.20
0.006
0.0006
0.00
0.01
0.51
0.41
0.019
0.042
0.012
0.0012


EE
0.27*
0.53
1.12
0.006
0.0004
1.61
3.23
0.68
0.78
0.021
0.043
0.011
0.0012


FF
0.22
0.85*
1.08
0.005
0.0005
1.55
3.16
0.51
0.77
0.022
0.041
0.009
0.0011


GG
0.18
0.42
2.11*
0.003
0.0003
1.51
2.84
0.53
0.63
0.021
0.038
0.011
0.0012


HH
0.21
0.51
1.32
0.004
0.0005
0.13
0.26
0.36
0.64
0.022
0.041
0.009
0.0011


II
0.22
0.48
1.16
0.005
0.0004
0.16
0.28
0.38
0.65
0.019
0.043
0.008
0.0012












Remarks

























Ar3
Ac1




Steels
W
Ca
REM
Mg
Al
T.N
(° C.)
(° C.)
Remarks







Q
0.15



0.027
0.0031
600
703
Example



R

0.0017


0.030
0.0030
716
722
Comparative Example



S




0.024
0.0024
641
706
Comparative Example



T




0.032
0.0030
695
718
Comparative Example



U

0.0019


0.027
0.0037
701
726
Comparative Example



X




0.035
0.0034
782
723
Example



Y

0.0005


0.031
0.0032
391
671
Example



Z

0.0012

0.0012
0.028
0.0035
342
658
Example



AA

0.0016


0.031
0.0034
448
661
Example



BB

0.0017


0.032
0.0035
451
684
Example



CC

0.0018


0.028
0.0033
468
678
Example



DD

0.0093


0.026
0.0038
727
727
Example



EE

0.0014


0.025
0.0034
454
688
Comparative Example



FF

0.0012


0.028
0.0033
481
693
Comparative Example



GG

0.0013


0.031
0.0034
441
674
Comparative Example



HH

0.0003*


0.033
0.0032
666
720
Comparative Example



II

0.0108*


0.031
0.0028
673
722
Comparative Example







Note 1:



The symbol * means that the parameter deviates from the range specified in the present invention.



Note 2:



Ar3 = 910-310C—80Mn—20Cu—15Cr—55Ni—80Mo (the elements represent content ratios in mass percent)



Note 3:



Ac1 = 723-14Mn + 22Si—14.4Ni + 23.3Cr (the elements represent content ratios in mass percent)





















TABLE 3











Rolling
Direct
Direct








reduction for
quenching
quenching





Heating
non-
initiation
termination




Thickness
temperature
recrystallization
temperature
temperature
Cooling rate
Tempering initiation


No.
Steels
(mm)
(° C.)
regions (%)
(° C.)
(° C.)
(° C./s)
temperature (° C.)


















1
A
25
1170
35
840
180
30
160


2
B
12
1150
30
820
350
80
330


3
C
25
1130
55
840
320
30
300


4
D
12
1100
60
830
230
80
210


5
E
25
1050
60
820
170
30
150


6
F
12
1200
70
830
230
80
210


7
G
25
1100
60
830
130
30
110


8
H
50
1130
60
820
180
10
160


9
I
12
1150
80
830
190
80
170


10
J
25
1150
60
830
200
30
180


11
K
50
1130
60
850
90
10
 70


12
L
60
1150
60
850
150
8
130


13
M
6
1100
60
730
140
150
120


14
N
12
1100
60
750
240
80
Room temperature


15
O
25
1100
60
760
130
30
110


16
P
60
1110
60
710
110
8
Room temperature


17
Q
6
1090
60
810
210
150
190


18
A
25
1170
 25*
840
180
30
160


19
B
12
1150
 20*
820
350
80
330


20
C
25
1130
 25*
840
320
30
300


21
D
12
1100
60
 705*
230
75
210


22
E
25
1050
60
 700*
170
25
150




















Average









heating rate





for heating





the middle





of the steel





thickness





from the

Average





tempering
Time for
cooling rate





initiation
which the
for cooling





temperature
tempering
from the





to the
temperature
maintained
Aspect ratio




Tempering
tempering
is
tempering
of prior




temperature
temperature
maintained
temperature
austenite



No.
(° C.)
(° C./s)
(s)
to 200° C. (° C./s)
grains
Remarks







1
540
0.5
600
0.3
3.5
Example



2
610
1.0
600
0.6
3.3
Example



3
570
0.5
600
0.3
13.2
Example



4
550
1.0
600
0.6
9.8
Example



5
590
0.5
1200
0.3
7.5
Example



6
640
1.0
2400
0.6
12.3
Example



7
680
0.5
3600
0.3
17.3
Example



8
600
0.2
300
0.2
6.5
Example



9
630
1.0
600
0.6
17.3
Example



10
600
0.5
600
0.3
15.3
Example



11
580
0.2
600
0.2
10.9
Example



12
550
0.2
600
0.1
5.3
Example



13
410
2.0
600
1.3
16.9
Example



14
460
1.0
60
0.6
11.9
Example



15
480
0.5
600
0.3
12.3
Example



16
510
0.2
600
0.1
5.4
Example



17
430
2.0
600
1.3
17.9
Example



18
540
0.5
600
0.3
2.5*
Comparative Example



19
610
1.0
600
0.6
2.3*
Comparative Example



20
570
0.5
600
0.3
1.7*
Comparative Example



21
550
1.0
600
0.6
9.8
Comparative Example



22
590
0.5
1200
0.3
7.5
Comparative Example







Note 1:



The symbol * means that the parameter deviates from the range specified in the present invention.



Note 2:



Ranges specified in the present invention are as follows: rolling reduction for non-recrystallization regions: 30% or higher; direct quenching initiation temperature: Ar3 transformation temperature or higher; direct quenching termination temperature: 350° C. or lower; cooling rate: 1° C./s or higher; tempering temperature: Ac1 transformation temperature or lower





















TABLE 4











Rolling










reduction for
Direct
Direct






non-
quenching
quenching

Tempering





Heating
recrystallization
initiation
termination

initiation




Thickness
temperature
regions
temperature
temperature
Cooling rate
temperature


No.
Steels
(mm)
(° C.)
(%)
(° C.)
(° C.)
(° C./s)
(° C.)





23
F
12
1200
70
 690*
230
75
210


24
G
25
1100
60
830
 400*
35
110


25
H
50
1130
60
820
 450*
0.8*
160


26
I
12
1150
80
830
190
80
170


27
J
25
1150
60
830
200
30
180


28
K
50
1130
60
850
 90
10
70


29
R*
35
1100
60
830
200
15
180


30
S*
50
1050
60
850
150
10
130


31
T*
50
1050
60
850
150
10
130


32
U*
60
1200
60
850
150
8
130


33
X
25
1160
30
830
230
30
210


34
Y
6
1120
65
670
 80
150
60


35
Z
25
1110
75
640
100
30
80


36
AA
12
1120
70
650
120
80
100


37
BB
32
1130
75
720
100
18
80


38
CC
20
1150
70
680
100
50
80


39
DD
32
1100
60
830
230
18
210


40
EE*
16
1100
75
700
100
60
80


41
FF*
8
1110
70
680
100
120
80


42
GG*
12
1120
60
670
100
80
80


43
HH*
12
1120
60
830
200
80
180


44
II*
12
1120
60
830
200
80
180


















Average heating rate








for heating the

Average cooling




middle of the steel
Time
rate for cooling




thickness from the
for which
from the




tempering initiation
the tempering
maintained
Aspect ratio



Tempering
temperature to the
temperature
tempering
of prior



temperature
tempering
is maintained
temperature to
austenite


No.
(° C.)
temperature (° C./s)
(s)
200° C. (° C./s)
grains
Remarks





23
640
1.0
2400
0.6
12.3
Comparative Example


24
680
0.5
3600
0.3
17.3
Comparative Example


25
600
0.2
300
0.2
6.5
Comparative Example


26
 740*
1.0
600
0.6
17.3
Comparative Example


27
 730*
0.5
600
0.3
15.3
Comparative Example


28
 730*
0.2
600
0.2
10.9
Comparative Example


29
490
0.3
600
0.2
10.7
Comparative Example


30
520
0.2
600
0.2
4.9
Comparative Example


31
520
0.2
600
0.2
5.5
Comparative Example


32
500
0.2
600
0.1
6.3
Comparative Example


33
520
0.5
10
0.3
3.5
Example


34
500
2.0
10
1.3
12.5
Example


35
500
0.5
10
0.3
16.1
Example


36
520
1.0
10
0.6
14.1
Example


37
500
0.4
10
0.2
16.3
Example


38
520
0.6
60
0.4
14.5
Example


39
560
0.4
600
0.2
8.3
Example


40
520
0.8
10
0.5
16.7
Comparative Example


41
520
1.5
10
0.9
17.6
Comparative Example


42
500
1.0
10
0.6
6.5
Comparative Example


43
500
1.0
10
0.6
6.3
Comparative Example


44
500
1.0
10
0.6
6.5
Comparative Example





Note 1:


The symbol * means that the parameter deviates from the range specified in the present invention.


Note 2:


Ranges specified in the present invention are as follows: rolling reduction for non-recrystallization regions: 30% or higher; direct quenching initiation temperature: Ar3 transformation temperature or higher; direct quenching termination temperature: 350° C. or lower; cooling rate: 1° C./s or higher; tempering temperature: Ac1 transformation temperature or lower




















TABLE 5










vTrs at the middle of
Safety index of





Thickness
Yield strength
Tensile strength
the steel thickness
delayed fracture


No.
Steels
(mm)
(MPa)
(MPa)
(° C.)
resistance (%)
Remarks






















1
A
25
573
648
−105 
93
Example


2
B
12
601
678
−116 
89
Example


3
C
25
801
868
−78
91
Example


4
D
12
1023
1048
−68
89
Example


5
E
25
1006
1027
−69
85
Example


6
F
12
1056
1061
−59
83
Example


7
G
25
1013
1052
−59
85
Example


8
H
50
1014
1019
−52
84
Example


9
I
12
1083
1197
−42
81
Example


10
J
25
1197
1247
−42
85
Example


11
K
50
1232
1267
−41
79
Example


12
L
60
1017
1057
−48
86
Example


13
M
6
1257
1263
−49
80
Example


14
N
12
1357
1376
−41
79
Example


15
O
25
1327
1387
−39
78
Example


16
P
60
1287
1298
−36
79
Example


17
Q
6
1356
1387
−35
78
Example


18
A
25
476
553
−42
 46*
Comparative Example


19
B
12
529
607
−58
 42*
Comparative Example


20
C
25
815
823
−59
 38*
Comparative Example


21
D
12
831
867
 −29*
 66*
Comparative Example


22
E
25
923
941
 −31*
 59*
Comparative Example





Note 1:


The symbol * means that the parameter deviates from the range specified in the present invention.


Note 2:


Ranges specified in the present invention are as follows: 1. vTrs at the middle of the steel thickness (° C.): −40° C. or lower for steel plates with a tensile strength lower than 1200 MPa; −30° C. or lower for steel plates with a tensile strength of 1200 MPa or higher: 2. Safety index of delayed fracture resistance: 80% or higher for steel plates with a tensile strength lower than 1200 MPa; 75% or higher for steel plates with a tensile strength of 1200 MPa or higher




















TABLE 6










vTrs at the middle of






Thickness
Yield strength
Tensile strength
the steel thickness
Safety index of delayed


No.
Steels
(mm)
(MPa)
(MPa)
(° C.)
fracture resistance (%)
Remarks






















23
F
12
982
991
−38*
52*
Comparative Example


24
G
25
923
956
−31*
78*
Comparative Example


25
H
50
937
952
−27*
76*
Comparative Example


26
I
12
983
1063
−27*
68*
Comparative Example


27
J
25
1101
1157
−29*
62*
Comparative Example


28
K
50
1127
1151
−27*
53*
Comparative Example


29
R*
35
1017
1041
−31*
43*
Comparative Example


30
S*
50
1007
1047
−27*
42*
Comparative Example


31
T*
50
1009
1012
−23*
36*
Comparative Example


32
U*
60
1021
1061
−15*
39*
Comparative Example


33
X
25
562
627
−102 
96 
Example


34
Y
6
1380
1457
−42 
78 
Example


35
Z
25
1421
1512
−46 
77 
Example


36
AA
12
1358
1583
−48 
80 
Example


37
BB
32
1391
1623
−42 
79 
Example


38
CC
20
1413
1678
−43 
81 
Example


39
DD
32
1071
1112
−63 
88 
Example


40
EE*
16
1378
1563
−26*
56*
Comparative Example


41
FF*
8
1341
1532
−25*
63*
Comparative Example


42
GG*
12
1328
1419
−23*
65*
Comparative Example


43
HH*
12
1151
1238
−41 
68*
Comparative Example


44
II*
12
1168
1241
−28*
53*
Comparative Example





Note 1:


The symbol * means that the parameter deviates from the range specified in the present invention.


Note 2:


Ranges specified in the present invention are as follows: 1. vTrs at the middle of the steel thickness (° C.): −40° C. or lower for steel plates with a tensile strength lower than 1200 MPa; −30° C. or lower for steel plates with a tensile strength of 1200 MPa or higher: 2. Safety index of delayed fracture resistance: 80% or higher for steel plates with a tensile strength lower than 1200 MPa; 75% or higher for steel plates with a tensile strength of 1200 MPa or higher













TABLE 7





(mass %)



























Steels
C
Si
Mn
P
S
Cu
Ni
Cr
Mo
Nb
V
Ti





A
0.05
0.19
1.34
0.011
0.0019
0.00
0.00
0.03
0.05
0.020
0.034
0.000


B
0.08
0.26
1.43
0.018
0.0022
0.00
0.00
0.03
0.19
0.021
0.035
0.000


C
0.10
0.31
1.08
0.014
0.0029
0.00
0.00
0.06
0.09
0.019
0.008
0.010


D
0.12
0.38
1.48
0.014
0.0018
0.02
0.01
0.49
0.38
0.017
0.041
0.012


E
0.12
0.40
1.51
0.012
0.0019
0.02
0.01
0.26
0.40
0.020
0.000
0.010


F
0.13
0.41
1.51
0.014
0.0023
0.00
0.00
0.51
0.41
0.020
0.042
0.013


G
0.14
0.41
1.55
0.014
0.0022
0.00
1.09
0.50
0.43
0.020
0.000
0.011


H
0.15
0.41
1.52
0.014
0.0019
0.30
0.30
0.51
0.21
0.020
0.042
0.013


I
0.15
0.41
1.21
0.014
0.0027
0.00
0.00
0.51
0.69
0.020
0.000
0.013


J
0.16
0.42
1.19
0.005
0.0019
0.26
0.28
0.34
0.65
0.019
0.044
0.012


K
0.16
0.27
1.35
0.002
0.0009
0.26
0.24
0.53
0.52
0.022
0.052
0.013


L
0.17
0.37
1.12
0.009
0.0010
0.05
0.06
0.51
0.69
0.022
0.041
0.012


M
0.17
0.20
1.35
0.005
0.0018
0.00
0.40
0.35
0.25
0.022
0.050
0.000


N
0.17
0.22
1.45
0.015
0.0009
0.00
1.32
0.35
0.21
0.015
0.035
0.000


O
0.18
0.35
1.75
0.004
0.0007
0.20
0.20
0.45
0.30
0.019
0.008
0.010


P
0.21
0.33
1.09
0.014
0.0012
0.02
0.01
0.55
0.69
0.020
0.041
0.012



























Remarks











Ar3
Remarks Ac1


Steels
B
W
Ca
REM
Mg
Al
T.N
(° C.)
(° C.)





A
0.0000




0.031
0.0032
783
709


B
0.0000




0.028
0.0029
755
709


C
0.0010




0.022
0.0037
785
716


D
0.0012

0.0017


0.030
0.0030
716
722


E
0.0013




0.027
0.0031
715
717


F
0.0010




0.032
0.0037
708
723


G
0.0015




0.024
0.0024
641
706


H
0.0010




0.032
0.0030
695
718


I
0.0010


0.0025

0.032
0.0030
704
727


J
0.0012



0.0015
0.028
0.0046
688
719


K
0.0015

0.0032


0.052
0.0035
684
719


L
0.0013

0.0019


0.027
0.0037
701
726


M
0.0000


0.0019

0.031
0.0032
702
711


N
0.0000




0.028
0.0029
647
697


O
0.0010
0.20



0.022
0.0037
668
714


P
0.0012

0.0015


0.030
0.0030
693
728





Note 1:


The symbol * means that the parameter deviates from the range specified in the present invention.


Note 2:


Ar3 (° C.) = 910-310C—80Mn—20Cu—15Cr—55Ni—80Mo


Note 3:


Ac1 (° C.) = 723-14Mn + 22Si—14.4Ni + 23.3Cr















TABLE 8







(mass %)




























Steels
C
Si
Mn
P
S
Cu
Ni
Cr
Mo
Nb
V
Ti





Q
0.23
0.45
1.52
0.018
0.0015
0.02
1.34
0.45
0.45
0.020
0.000
0.010


R
0.12
0.38
1.48
0.025*
0.0018
0.02
0.01
0.49
0.38
0.017
0.041
0.012


S
0.14
0.41
1.55
0.014
0.0043*
0.00
1.09
0.50
0.43
0.020
0.000
0.011


T
0.15
0.41
1.52
0.031*
0.0019
0.30
0.30
0.51
0.21
0.020
0.042
0.013


U
0.17
0.37
1.12
0.032*
0.0042*
0.05
0.06
0.51
0.69
0.022
0.041
0.012


X
0.03
0.26
1.31
0.010
0.0009
0.01
0.03
0.56
0.05
0.012
0.031
0.001


Y
0.17
0.67
1.81
0.006
0.0008
1.98
3.91
0.63
0.72
0.018
0.043
0.012


Z
0.24
0.32
1.92
0.003
0.0006
1.95
3.95
0.51
0.95
0.016
0.042
0.015


AA
0.18
0.02
1.12
0.005
0.0003
1.66
3.81
0.36
0.86
0.022
0.045
0.012


BB
0.20
0.75
1.08
0.006
0.0004
1.82
3.56
0.48
0.89
0.019
0.046
0.012


CC
0.23
0.41
0.60
0.004
0.0003
1.91
3.78
0.39
0.88
0.021
0.045
0.010


DD
0.15
0.42
1.20
0.006
0.0006
0.00
0.01
0.51
0.41
0.019
0.042
0.012


EE
0.27*
0.53
1.12
0.006
0.0004
1.61
3.23
0.68
0.78
0.021
0.043
0.011


FF
0.22
0.85*
1.08
0.005
0.0005
1.55
3.16
0.51
0.77
0.022
0.041
0.009


GG
0.18
0.42
2.11*
0.003
0.0003
1.51
2.84
0.53
0.63
0.021
0.038
0.011


HH
0.21
0.51
1.32
0.004
0.0005
0.13
0.26
0.36
0.64
0.022
0.041
0.009


II
0.22
0.48
1.16
0.005
0.0004
0.16
0.28
0.38
0.65
0.019
0.043
0.008





























Remarks
Remarks











Ar3
Ac1



Steels
B
W
Ca
REM
Mg
Al
T.N
(° C.)
(° C.)







Q
0.0013
0.15



0.027
0.0031
600
703



R
0.0012

0.0017


0.030
0.0030
716
722



S
0.0015




0.024
0.0024
641
706



T
0.0010




0.032
0.0030
695
718



U
0.0013

0.0019


0.027
0.0037
701
726



X
0.0003




0.035
0.0034
782
723



Y
0.0015

0.0005


0.031
0.0032
391
671



Z
0.0013

0.0012

0.0012
0.028
0.0035
342
658



AA
0.0010

0.0016


0.031
0.0034
448
661



BB
0.0011

0.0017


0.032
0.0035
451
684



CC
0.0013

0.0018


0.028
0.0033
468
678



DD
0.0012

0.0093


0.026
0.0038
727
727



EE
0.0012

0.0014


0.025
0.0034
454
688



FF
0.0011

0.0012


0.028
0.0033
481
693



GG
0.0012

0.0013


0.031
0.0034
441
674



HH
0.0011

0.0003*


0.033
0.0032
666
720



II
0.0012

0.0108*


0.031
0.0028
673
722







Note 1:



The symbol * means that the parameter deviates from the range specified in the present invention.



Note 2:



Ar3 (° C.) = 910-310C—80Mn—20Cu—15Cr—55Ni—80Mo



Note 3:



Ac1 (° C.) = 723-14Mn + 22Si—14.4Ni + 23.3Cr





















TABLE 9












Direct
Direct








Rolling reduction
quenching
quenching





Heating
for non-
initiation
termination

Tempering




Thickness
temperature
recrystallization
temperature
temperature
Tempering initiation
temperature


No.
Steels
(mm)
(° C.)
regions (%)
(° C.)
(° C.)
temperature (° C.)
(° C.)





1
A
25
1170
35
840
180
160
540


2
B
12
1150
30
820
350
330
610


3
C
25
1130
55
840
320
300
570


4
D
12
1100
60
830
230
210
550


5
E
25
1050
60
820
170
150
590


6
F
12
1200
70
830
230
210
640


7
G
25
1100
60
830
130
110
680


8
H
50
1130
60
820
180
160
600


9
I
12
1150
80
830
190
170
630


10
J
25
1150
60
830
200
180
600


11
K
50
1130
60
850
 90
 70
580


12
L
60
1150
60
850
150
130
550


13
M
6
1100
60
730
140
120
410


14
N
12
1100
60
750
240
Room temperature
460


15
O
25
1100
60
760
130
110
480


16
P
60
1110
60
710
110
Room temperature
510


17
Q
6
1090
60
810
210
190
430


18
A
25
1170
 25*
840
180
160
540


19
B
12
1150
 20*
820
350
330
610


20
C
25
1130
 25*
840
320
300
570


21
D
12
1100
60
 705*
230
210
550


22
E
25
1050
60
 700*
170
150
590


23
F
12
1200
70
 690*
230
210
640


24
G
25
1100
60
830
 400*
110
680


25
H
50
1130
60
820
 450*
160
600


26
I
12
1150
80
830
190
170
 740*



















Average








Average
heating rate

Average



heating rate
for heating

cooling rate



for heating
the middle

for cooling



the middle of
of the steel

from the



the steel thickness
thickness from

maintained
Aspect



from the tempering
370° C. to the
Time for which
tempering
ratio of
Cementite



initiation
tempering
the tempering
temperature
prior
covering



temperature
temperature
temperature is
to 200° C.
austenite
rate of


No.
to 370° C. (° C./s)
(° C./s)
maintained (s)
(° C./s)
grains
laths
Classification





1
6.0
8.0
0
0.3
3.5
 5
Example


2
12.5
14.5
0
0.6
3.3
 7
Example


3
6.0
8.0
0
0.3
13.2
12
Example


4
12.5
14.5
0
0.6
9.8
15
Example


5
6.0
8.0
0
0.3
7.5
24
Example


6
12.5
14.5
0
0.6
12.3
34
Example


7
6.0
8.0
0
0.3
17.3
40
Example


8
3.0
5.0
60
0.2
6.5
26
Example


9
12.5
14.5
0
0.6
17.3
25
Example


10
6.0
8.0
0
0.3
15.3
30
Example


11
3.0
5.0
60
0.2
10.9
26
Example


12
2.5
4.5
0
0.1
5.3
19
Example


13
25.0
27.0
0
1.3
16.9
11
Example


14
12.5
14.5
0
0.6
11.9
23
Example


15
6.0
8.0
0
0.3
12.3
37
Example


16
2.5
4.5
0
0.1
5.4
40
Example


17
25.0
27.0
0
1.3
17.9
35
Example


18
6.0
8.0
0
0.3
2.5*
 55*
Comparative Example


19
12.5
14.5
0
0.6
2.3*
 52*
Comparative Example


20
6.0
8.0
0
0.3
1.7*
 53*
Comparative Example


21
12.5
14.5
0
0.6
8.8
14
Comparative Example


22
6.0
8.0
0
0.3
7.1
23
Comparative Example


23
12.5
14.5
0
0.6
11.2
32
Comparative Example


24
6.0
8.0
0
0.3
16.6
38
Comparative Example


25
3.0
5.0
60
0.2
6.2
24
Comparative Example


26
12.5
14.5
0
0.6
17.0
 56*
Comparative Example





Note:


The symbol * means that the parameter deviates from the range specified in the present invention.





















TABLE 10











Rolling
Direct
Direct








reduction for
quenching
quenching





Heating
non-
initiation
termination

Tempering




Thickness
temperature
recrystallization
temperature
temperature
Tempering initiation
temperature


No.
Steels
(mm)
(° C.)
regions (%)
(° C.)
(° C.)
temperature (° C.)
(° C.)


















27
J
25
1150
60
830
200
180
 730*


28
K
50
1130
60
850
 90
 70
 730*


29
L
60
1150
60
850
150
130
550


30
M
6
1100
60
730
140
120
410


31
N
12
1100
60
750
240
Room temperature
460


32
O
25
1100
60
760
130
110
480


33
P
60
1110
60
710
110
Room temperature
510


34
Q
6
1090
60
810
210
190
430


35
D
12
1100
60
830
230
210
550


36
L
60
1150
60
850
150
130
550


37
R
35
1100
60
830
200
180
490


38
S
50
1050
60
850
150
130
520


39
T
50
1050
60
850
150
130
520


40
U
60
1200
60
850
150
130
500


41
X
25
1160
30
830
230
810
520


42
Y
6
1120
65
670
80
850
500


43
Z
25
1110
75
640
100
620
500


44
AA
12
1120
70
650
120
630
520


45
BB
32
1130
75
720
100
700
500


46
CC
20
1150
70
680
100
660
520


47
DD
32
1100
60
830
230
810
560


48
EE
16
1100
75
700
100
680
520


49
FF
8
1110
70
680
100
660
520


50
GG
12
1120
60
670
100
650
500


51
HH
12
1120
60
830
200
810
500


52
II
12
1120
60
830
200
810
500


















Average









heating rate



for heating


Average



the middle


cooling rate



of the steel


for cooling



thickness from
Average heating rate
Time for
from the



the tempering
for heating the middle
which the
maintained
Aspect



initiation
of the steel thickness
tempering
tempering
ratio of
Cementite



temperature
from 370° C. to the
temperature
temperature
prior
covering



to 370° C.
tempering
is maintained
to 200° C.
austenite
rate of


No.
(° C./s)
temperature (° C./s)
(s)
(° C./s)
grains
laths
Classification





27
6.0
8.0
0
0.3
15.1
 61*
Comparative Example


28
3.0
5.0
60
0.2
10.2
 63*
Comparative Example


29
2.5
0.8*
0
0.1
5.3
39
Comparative Example


30
25.0
0.9*
0
1.3
16.9
 52*
Comparative Example


31
12.5
0.7*
0
0.6
11.9
42
Comparative Example


32
1.5
0.6*
0
0.3
12.3
 55*
Comparative Example


33
1.1
0.6*
0
0.1
5.4
 61*
Comparative Example


34
1.2
0.8*
0
1.3
17.9
 53*
Comparative Example


35
1.5
14.5
0
0.6
9.8
23
Example


36
1.0
4.5
0
0.1
5.3
32
Example


37
4.3
6.3
0
0.2
10.7
41
Comparative Example


38
3.0
5.0
0
0.2
4.9
45
Comparative Example


39
3.0
5.0
0
0.2
5.5
23
Comparative Example


40
2.5
4.5
0
0.1
6.3
 56*
Comparative Example


41
5.0
7.0
10
0.3
3.5
25
Example


42
20.0
22.0
0
1.3
12.5
21
Example


43
5.0
7.0
10
0.3
16.1
25
Example


44
10.0
12.0
10
0.6
14.1
21
Example


45
3.0
5.0
0
0.2
16.3
32
Example


46
5.0
7.0
0
0.4
14.5
26
Example


47
3.0
5.0
0
0.2
8.3
31
Example


48
8.0
10.0
0
0.5
16.7
34
Comparative Example


49
15.0
17.0
0
0.9
17.6
19
Comparative Example


50
10.0
12.0
0
0.6
6.5
32
Comparative Example


51
10.0
12.0
0
0.6
6.3
23
Comparative Example


52
10.0
12.0
10
0.6
6.5
26
Comparative Example





Note:


The symbol * means that the parameter deviates from the range specified in the present invention.




















TABLE 11










vTrs at the
Safety index of






Yield
Tensile
middle of the
delayed




Thickness
strength
strength
steel thickness
fracture


No.
Steels
(mm)
(MPa)
(MPa)
(° C.)
resistance (%)
Classification






















1
A
25
596
667
−121 
100 
Example


2
B
12
611
695
−131 
99
Example


3
C
25
812
888
−93
100 
Example


4
D
12
1037
1061
−81
98
Example


5
E
25
1015
1041
−83
99
Example


6
F
12
1112
1115
−73
97
Example


7
G
25
1069
1100
−76
97
Example


8
H
50
1025
1034
−63
96
Example


9
I
12
1151
1253
−53
95
Example


10
J
25
1251
1314
−51
90
Example


11
K
50
1296
1312
−49
91
Example


12
L
60
1051
1097
−56
98
Example


13
M
6
1315
1317
−66
89
Example


14
N
12
1410
1426
−56
88
Example


15
O
25
1399
1415
−49
89
Example


16
P
60
1333
1348
−41
85
Example


17
Q
6
1410
1451
−66
82
Example


18
A
25
523
601
−59
 53*
Comparative Example


19
B
12
538
623
−63
 49*
Comparative Example


20
C
25
783
852
−67
 41*
Comparative Example


21
D
12
927
953
 −39*
 73*
Comparative Example


22
E
25
936
951
 −36*
 75*
Comparative Example


23
F
12
1037
1039
−41
 67*
Comparative Example


24
G
25
986
1012
 −38*
97
Comparative Example


25
H
50
953
967
 −34*
96
Comparative Example


26
I
12
1053
1149
 −32*
95
Comparative Example





Note:


The symbol * means that the parameter deviates from the range specified in the present invention.


Note 2:


Ranges specified in the present invention are as follows: 1. vTrs at the middle of the steel thickness (° C.): −40° C. or lower for steel plates with a tensile strength lower than 1200 MPa: −30° C. or lower for steel plates with a tensile strength of 1200 MPa or higher: 2. Safety index of delayed fracture resistance: 85% or higher for steel plates with a tensile strength lower than 1200 MPa; 80% or higher for steel plates with a tensile strength of 1200 MPa or higher




















TABLE 12










vTrs at









the middle







of the





Yield
Tensile
steel
Safety index of





Thickness
strength
strength
thickness
delayed fracture


No.
Steels
(mm)
(MPa)
(MPa)
(° C.)
resistance (%)
Classification






















27
J
25
1153
1213
−33
67*
Comparative Example


28
K
50
1183
1203
−35
69*
Comparative Example


29
L
60
1012
1053
 −23*
83*
Comparative Example


30
M
6
1213
1216
 −28*
81 
Comparative Example


31
N
12
1308
1327
 −25*
78*
Comparative Example


32
O
25
1297
1323
 −24*
72*
Comparative Example


33
P
60
1216
1218
 −26*
68*
Comparative Example


34
Q
6
1309
1311
−35
73*
Comparative Example


35
D
12
1039
1058
−75
95 
Example


36
L
60
1048
1093
−47
93 
Example


37
R
35
1031
1063
 −38*
64*
Comparative Example


38
S
50
1061
1105
 −34*
61*
Comparative Example


39
T
50
1015
1023
 −29*
53*
Comparative Example


40
U
60
1049
1099
 −23*
55*
Comparative Example


41
X
25
589
661
−112 
98 
Example


42
Y
6
1411
1473
−51
88 
Example


43
Z
25
1459
1539
−53
82 
Example


44
AA
12
1371
1606
−55
86 
Example


45
BB
32
1403
1641
−47
86 
Example


46
CC
20
1451
1712
−51
90 
Example


47
DD
32
1115
1143
−70
92 
Example


48
EE
16
1405
1589
−32
62*
Comparative Example


49
FF
8
1369
1551
−34
72*
Comparative Example


50
GG
12
1351
1441
−32
71*
Comparative Example


51
HH
12
1179
1251
−52
72*
Comparative Example


52
II
12
1181
1269
−39
62*
Comparative Example


27
J
25
1153
1213
−33
67*
Comparative









Example


28
K
50
1183
1203
−35
69*
Comparative









Example


29
L
60
1012
1053
 −23*
83*
Comparative









Example


30
M
6
1213
1216
 −28*
81 
Comparative









Example


31
N
12
1308
1327
 −25*
78*
Comparative









Example


32
O
25
1297
1323
 −24*
72*
Comparative









Example


33
P
60
1216
1218
 −26*
68*
Comparative









Example


34
Q
6
1309
1311
−35
73*
Comparative









Example


35
D
12
1039
1058
−75
95 
Example


36
L
60
1048
1093
−47
93 
Example


37
R
35
1031
1063
 −38*
64*
Comparative









Example


38
S
50
1061
1105
 −34*
61*
Comparative









Example


39
T
50
1015
1023
 −29*
53*
Comparative









Example


40
U
60
1049
1099
 −23*
55*
Comparative









Example


41
X
25
589
661
−112 
98 
Example


42
Y
6
1411
1473
−51
88 
Example


43
Z
25
1459
1539
−53
82 
Example


44
AA
12
1371
1606
−55
86 
Example


45
BB
32
1403
1641
−47
86 
Example


46
CC
20
1451
1712
−51
90 
Example


47
DD
32
1115
1143
−70
92 
Example


48
EE
16
1405
1589
−32
62*
Comparative









Example


49
FF
8
1369
1551
−34
72*
Comparative









Example


50
GG
12
1351
1441
−32
71*
Comparative









Example


51
HH
12
1179
1251
−52
72*
Comparative









Example


52
II
12
1181
1269
−39
62*
Comparative









Example





Note:


The symbol * means that the parameter deviates from the range specified in the present invention.


Note 2:


Ranges specified in the present invention are as follows: 1. vTrs at the middle of the steel thickness (° C.): −40° C. or lower for steel plates with a tensile strength lower than 1200 MPa; −30° C. or lower for steel plates with a tensile strength of 1200 MPa or higher: 2. Safety index of delayed fracture resistance: 85% or higher for steel plates with a tensile strength lower than 1200 MPa; 80% or higher for steel plates with a tensile strength of 1200 MPa or higher





Claims
  • 1. A high tensile strength steel comprising elements C: 0.02 to 0.25%, Si: 0.01 to 0.8%, Mn: 0.5 to 2.0%, Al: 0.005 to 0.1%, N: 0.0005 to 0.008%, P: 0.02% or lower, and S: 0.004% or lower, all in percent by mass, and Fe and an unavoidable impurity as a balance, wherein an average aspect ratio of a prior austenite grain calculated over entire thickness is at least three.
  • 2. The high tensile strength steel according to claim 1, wherein S: 0.003% or lower and a cementite covering ratio measured at a boundary of a lath is 50% or lower.
  • 3. The high tensile strength steel according to claim 1, further comprising one or more of Mo: 1% or lower, Nb: 0.1% or lower, V: 0.5% or lower, Ti: 0.1% or lower, Cu: 2% or lower, Ni: 4% or lower, Cr: 2% or lower, and W: 2% or lower, all in percent by mass.
  • 4. The high tensile strength steel according to claim 1, further comprising one or more of B: 0.003% or lower, Ca: 0.01% or lower, REM: 0.02% or lower, and Mg: 0.01% or lower, all in percent by mass.
  • 5. The high tensile strength steel according to claim 1, wherein hydrogen is charged into the steel and the hydrogen contained in the steel is sealed by zinc galvanizing, a safety index of delayed fracture resistance calculated using the formula described below being at least 75% when a slow strain rate test is performed with a strain rate set to 1×10−3/s or lower: Safety index of delayed fracture resistance (%)=100×(X1/X0)where X0: reduction of area of a specimen substantially free from diffusible hydrogen, andX1: reduction of area of a specimen containing diffusible hydrogen.
  • 6. The high tensile strength steel according to claim 5, wherein the safety index of delayed fracture resistance is at least 80%.
  • 7. A method for manufacturing the high tensile strength steel comprising casting steel having a composition according to claim 1 and a safety index of delayed fracture resistance calculated using the formula described below being at least 75% when a slow strain rate test is performed with a strain rate set to 1×10−3/s or lower: Safety index of delayed fracture resistance (%)=100×(X1/X0)where X0: reduction of area of a specimen substantially free from diffusible hydrogen, andX1: reduction of area of a specimen containing diffusible hydrogen, comprising: protecting the steel from cooling to an Ar3 transformation temperature or lower or heating the steel to a temperature equal to or higher than an Ac3 transformation temperature once again,hot rolling to achieve a predetermined steel thickness including rolling conducted with a rolling reduction for a non-recrystallization region set to 30% or higher,cooling the steel from a temperature equal to or higher than the Ar3 transformation temperature to a temperature equal to or lower than 350° C. at a cooling rate of 1° C./s or higher, andtempering the steel at a temperature equal to or lower than an Ac1 transformation temperature.
  • 8. The method according to claim 7, in which the steel is tempered at a temperature equal to or lower than the Ac1 transformation temperature, for manufacturing the high tensile strength steel having a safety index of delayed fracture resistance of at least 80%, wherein a heating apparatus installed in a manufacturing line having a rolling mill and a cooling apparatus is used to heat the steel from 370° C. to a predetermined tempering temperature equal to or lower than the Ac1 transformation temperature while maintaining an average heating rate for heating a middle of a steel thickness at 1° C./s or higher so that a maximum temperature at the middle of the steel thickness is 400° C. or higher.
  • 9. The method according to claim 8, in which the steel is tempered at a temperature equal to or lower than the Ac1 transformation temperature, for manufacturing the high tensile strength steel having a safety index of delayed fracture resistance of at least 80%, wherein the steel is heated from a tempering initiation temperature to 370° C. with an average heating rate for heating the middle of the steel thickness maintained at 2° C./s or higher.
  • 10. A high tensile strength steel comprising elements C: 0.02 to 0.25%, Si: 0.01 to 0.8%, Mn: 0.5 to 2.0%, Al: 0.005 to 0.1%, N: 0.0005 to 0.008%, P: 0.02% or lower, and S: 0.004% or lower, all in percent by mass, and Fe and an unavoidable impurity as a balance, wherein an average aspect ratio of a prior austenite grain calculated over entire thickness is at least three.
  • 11. The high tensile strength steel according to claim 10, further comprising one or more of Mo: 1% or lower, Nb: 0.1% or lower, V: 0.5% or lower, Ti: 0.1% or lower, Cu: 2% or lower, Ni: 4% or lower, Cr: 2% or lower, and W: 2% or lower, all in percent by mass.
  • 12. The high tensile strength steel according to claim 10, further comprising one or more of B: 0.003% or lower, Ca: 0.01% or lower, REM: 0.02% or lower, and Mg: 0.01% or lower, all in percent by mass.
  • 13. The high tensile strength steel according to claim 10, wherein hydrogen is charged into the steel and the hydrogen contained in the steel is sealed by zinc galvanizing, a safety index of delayed fracture resistance calculated using the formula described below being at least 75% when a slow strain rate test is performed with a strain rate set to 1×10−3/s or lower: Safety index of delayed fracture resistance (%)=100×(X1/X0)where X0: reduction of area of a specimen substantially free from diffusible hydrogen, andX1: reduction of area of a specimen containing diffusible hydrogen.
  • 14. A method for manufacturing the high tensile strength steel comprising casting steel having a composition according to claim 10 and a safety index of delayed fracture resistance calculated using the formula described below being at least 75% when a slow strain rate test is performed with a strain rate set to 1×10−3/s or lower: Safety index of delayed fracture resistance (%)=100×(X1/X0)where X0: reduction of area of a specimen substantially free from diffusible hydrogen, andX1: reduction of area of a specimen containing diffusible hydrogen, comprising: protecting the steel from cooling to an Ar3 transformation temperature or lower or heating the steel to a temperature equal to or higher than an Ac3 transformation temperature once again,hot rolling to achieve a predetermined steel thickness including rolling conducted with a rolling reduction for a non-recrystallization region set to 30% or higher,cooling the steel from a temperature equal to or higher than the Ar3 transformation temperature to a temperature equal to or lower than 350° C. at a cooling rate of 1° C./s or higher, andtempering the steel at a temperature equal to or lower than an Ac1 transformation temperature.
  • 15. A high tensile strength steel comprising elements C: 0.02 to 0.25%, Si: 0.01 to 0.8%, Mn: 0.5 to 2.0%, Al: 0.005 to 0.1%, N: 0.0005 to 0.008%, P: 0.02% or lower, and S: 0.003% or lower, all in percent by mass, and Fe and an unavoidable impurity as a balance, wherein an average aspect ratio of a prior austenite grain calculated over entire thickness is at least three and a cementite covering ratio measured at a boundary of a lath is 50% or lower.
  • 16. The high tensile strength steel according to claim 15, further comprising one or more of Mo: 1% or lower, Nb: 0.1% or lower, V: 0.5% or lower, Ti: 0.1% or lower, Cu: 2% or lower, Ni: 4% or lower, Cr: 2% or lower, and W: 2% or lower, all in percent by mass.
  • 17. The high tensile strength steel according to claim 15, further comprising one or more of B: 0.003% or lower, Ca: 0.01% or lower, REM: 0.02% or lower, and Mg: 0.01% or lower, all in percent by mass.
  • 18. The high tensile strength steel according to claim 15, wherein hydrogen is charged into the steel and the hydrogen contained in the steel is sealed by zinc galvanizing, a safety index of delayed fracture resistance calculated using the formula described below being at least 80% when a slow strain rate test is performed with a strain rate set to 1×10−3/s or lower: Safety index of delayed fracture resistance (%)=100×(X1/X0)where X0: reduction of area of a specimen substantially free from diffusible hydrogen, andX1: reduction of area of a specimen containing diffusible hydrogen.
  • 19. A method for manufacturing the high tensile strength steel comprising casting steel having the composition according to claim 15 and a safety index of delayed fracture resistance calculated using the formula described below being at least 80% when a slow strain rate test is performed with a strain rate set to 1×10−3/s or lower: Safety index of delayed fracture resistance (%)=100×(X1/X0)where X0: reduction of area of a specimen substantially free from diffusible hydrogen, andX1: reduction of area of a specimen containing diffusible hydrogen comprising: protecting the steel from cooling to an Ar3 transformation temperature or lower or heating the steel to a temperature equal to or higher than an Ac3 transformation temperature once again,hot rolling to achieve a predetermined steel thickness including rolling conducted with a rolling reduction for a non-recrystallization region set to 30% or higher,cooling the steel from a temperature equal to or higher than the Ar3 transformation temperature to a temperature equal to or lower than 350° C. at a cooling rate of 1° C./s or higher, andtempering the steel using a heating apparatus installed in a manufacturing line having a rolling mill and a cooling apparatus with an average heating rate for heating a middle of a steel thickness from 370° C. to a predetermined tempering temperature equal to or lower than the Ac1 transformation temperature maintained at 1° C./s or higher so that a maximum temperature at the middle of the steel thickness is 400° C. or higher.
  • 20. A method for manufacturing the high tensile strength steel comprising casting steel having the composition according to claim 15 and a safety index of delayed fracture resistance calculated using the formula described below being at least 80% when a slow strain rate test is performed with a strain rate set to 1×10−3/s or lower: Safety index of delayed fracture resistance (%)=100×(X1/X0)where X0: reduction of area of a specimen substantially free from diffusible hydrogen, andX1: reduction of area of a specimen containing diffusible hydrogen comprising: protecting the steel from cooling to an Ar3 transformation temperature or lower or heating the steel to a temperature equal to or higher than an Ac3 transformation temperature once again,hot rolling to achieve a predetermined steel thickness including rolling conducted with a rolling reduction for a non-recrystallization region set to 30% or higher,cooling the steel from a temperature equal to or higher than the Ar3 transformation temperature to a temperature equal to or lower than 350° C. at a cooling rate of 1° C./s or higher, andtempering the steel using a heating apparatus installed in a manufacturing line having a rolling mill and a cooling apparatus with an average heating rate for heating a middle of a steel thickness from a tempering initiation temperature to 370° C. maintained at 2° C./s or higher and an average heating rate for heating the middle of the steel thickness from 370° C. to a predetermined tempering temperature equal to or lower than an Ac1 transformation temperature maintained at 1° C./s or higher so that a maximum temperature at the middle of the steel thickness is 400° C. or higher.
Priority Claims (2)
Number Date Country Kind
2007-021573 Jan 2007 JP national
2007-086296 Mar 2007 JP national
RELATED APPLICATIONS

This is a §371 of International Application No. PCT/JP2008/052002, with an international filing date of Jan. 31, 2008 (WO 2008/093897 A1, published Aug. 7, 2008), which is based on Japanese Patent Application Nos. 2007-021573, filed Jan. 31, 2007, and 2007-086296, filed Mar. 29, 2007.

PCT Information
Filing Document Filing Date Country Kind 371c Date
PCT/JP2008/052002 1/31/2008 WO 00 7/29/2009