STEEL MATERIAL EXCELLENT IN RESISTANCE OF DUCTILE CRACK INITIATION FROM WELDED HEAT AFFECTED ZONE AND BASE MATERIAL AND METHOD FOR MANUFACTURING THE SAME

- JFE STEEL CORPORATION

A steel material has a composition of C: 0.02 to 0.2%, Si: 0.01 to 0.5%, Mn: 0.5 to 2.5%, P: 0.05% or lower, S: 0.05% or lower, Al: 0.1% or lower, and N: 0.01% or lower and, as required, one or two or more elements selected from Cu: 0.01 to 2%, Ni: 0.01 to 5%, Cr: 0.01 to 3%, Mo: 0.01 to 2%, Nb: 0.1% or lower, V: 0.1% or lower, Ti: 0.1% or lower, B: 0.01% or lower, Ca: 0.01% or lower, and REM: 0.1% or lower in terms of % by mass, and the balance Fe with inevitable impurities, in which the microstructure at the ¼ position of the plate thickness contains ferrite and a hard phase, the area fraction of the hard phase is 50 to 90%, and the average aspect ratio of the ferrite is 1.5 or more.

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Description
RELATED APPLICATIONS

This is a §371 of International Application No. PCT/JP2009/071908, with an international filing date of Dec. 25, 2009 (WO 2010/074347 A1, published Jul. 1, 2010), which is based on Japanese Patent Application Nos. 2008-333204, filed Dec. 26, 2008, and 2008-333205, filed Dec. 26, 2008, the subject matter of which is incorporated by reference.

TECHNICAL FIELD

This disclosure relates to steel materials suitable for use in welded structures such as pipelines, bridges, and architectural structures, requiring structural safety and a method for manufacturing the same and particularly relates to one excellent in resistance of ductile crack initiation from welded heat affected zone and a base material. Specifically, the disclosure is targeted to steel materials for structures having excellent resistance of ductile crack initiation from welded heat affected zone and a base material and having strength of Tensile strength: 490 MPa or more in TS and high toughness of Ductile-brittle fracture transition temperature of Charpy impact test (according to the regulation of JIS Z 2242): vTrs of 0° C. or lower.

BACKGROUND

It is known that when the welded structures such as pipelines, bridges, and buildings, are exposed to large external force of an earthquake or the like, ductile crack initiates in a stress concentration zone, such as a weld toe, and the generated ductile crack serves as a trigger to cause brittle fracture, resulting in break and fracture of the structures in some cases.

It is important that steel materials constituting the same are excellent in resistance of ductile crack initiation to avoid such break and fracture of the welded structures.

Japanese Unexamined Patent Application Publication No. 2008-202119 discloses a high tensile-strength steel material excellent in resistance of ductile crack initiation in which, in the microstructure a steel material surface zone, the ferrite area fraction is 10 to 40%, the bainite area fraction is 50% or more, and the average grain size is 5 μm or lower.

Japanese Unexamined Patent Application Publication No. 2000-3281777 discloses a steel plate excellent in arrestrability and resistance of ductile fracture in which the microstructure is substantially constituted by a ferrite structure, a pearlite structure, and a bainite structure and, when divided into three layers of both surface zones and the central zone in the plate thickness direction of the steel plate, each zone has a specific microstructure.

Both the surface zones of the steel plate are constituted by a layer which has 50% or more of a ferrite structure containing ferrite grains in which the equivalent (circle) diameter is 7 μm or lower and the aspect ratio is 2 to 4 over 5% or more of the plate thickness of each of the structure zones and in which the bainite area fraction of the portion is 5 to 25% or lower. The central zone in the plate thickness direction of the steel plate is constituted by a layer which contains ferrite grains in which the equivalent (circle) diameter is 4 to 10 μm and the aspect ratio is 2 or lower over 50% or more of the plate thickness and in which the bainite area fraction of the zones is 10% or lower.

More specifically, the technique of JP '177 is directed to a steel plate in which three layers having a ferrite/pearlite structure containing ferrite grains different in the aspect ratio are present in the plate thickness direction from the plate surface of the steel plate and further in which a bainite structure which is a hard phase is appropriately dispersed in a soft phase which is the ferrite/pearlite structure. The technique increases the arrestrability by positively forming processed ferrite grains having a high aspect ratio and also appropriately dispersing a bainite structure on each of both the surface zones of the three zones of the steel plate and, in contrast, increases extension characteristics, which are important to ductile fracture at room temperature, by controlling the central zone of the steel plate to have a uniform equiaxed ferrite grain structure and also suppressing a bainite structure, and thus satisfies both opposite characteristics of “arrestrability” and “ductile fracture characteristics” by controlling both the surface zones and the central zone of the steel plate to the three-layer structure.

Also the technique of Japanese Unexamined Patent Application Publication No. 2003-221619 is directed to a technique of obtaining deformed ferrite grains on the steel plate surface zone of ferrite/pearlite steel and also controlling the microstructure of the central zone to a uniform equiaxed ferrite grain structure similarly as the technique of JP '177.

More specifically, JP '619 discloses a method for manufacturing a thick steel plate excellent in arrestrability and ductile fracture characteristics in which the rolling conditions are strictly controlled so that the steel plate surface zone has a specific microstructure.

Specifically, when the thickness during plate rolling is defined as t, an equivalent plastic strain ε of ε≧0.5 in a non-recrystallization temperature zone of Ar3 transformation point or more and 900° C. or lower is given to a surface layer zone of 0.05 t or more and 0.15 t or lower from both the surfaces in the plate thickness direction.

Thereafter, the surface layer zone is cooled to a temperature range of 450 to 650° C. at a cooling rate of 2 to 15° C./s while maintaining the temperature of the central zone defined as t/4 to 3t/4 of the plate thickness at the Ar3 transformation point or more within a period of time when the residual and cumulative equivalent plastic strain εr of the surface layer zone satisfies εr≧0.5, and subsequently rolling is restarted.

In the restarted rolling, the residual and cumulative equivalent plastic strain εr of 0.35≦εr<0.55 is given to the central zone to complete the rolling at the Ar3 transformation point or more and also the surface layer is recuperated to the Ar3 transformation point or lower by processing heat and internal sensible heat, and thereafter cooling is performed in such a manner that the average cooling rate is 1 to 10° C./s.

The techniques of JP '119, JP '177 and JP '619 all relate to techniques of forming fine subgrains in austenite to miniaturize the structure after transformation by performing rolling in a non recrystallization zone (fine grain temperature zone) of austenite or performing rolling at a rolling finish temperature Ar3 or more.

However, according to the techniques of JP '119, JP '177 and JP '619, when the surface layer structure changes to the welded heat affected zone by welding or the like, there is a concern that the effect of resistance of ductile crack initiation is lost.

Moreover, in all of a scale breaker for use in treatment of the surface of a slab extracted from a heating furnace described in Examples of JP '119, two-stage rolling of rolling in a pulverization temperature range and rolling in a set temperature zone described in Examples of JP '177, and various kinds of rolling or temperature control for separately creating the structure of a surface layer and the structure inside a steel plate described in JP '619, the manufacturing process is complicated.

Then, in view of the problems of such former techniques, it could be helpful to provide steel materials excellent in resistance of ductile crack initiation from the welded heat affected zone and a base material by a simple method and a method for manufacturing the same.

SUMMARY

We conducted extensive research on the microstructure of base material excellent in resistance of ductile crack initiation of welded heat affected zones and found that, when the microstructure of a base material has a ferrite and a hard phase in which the average aspect ratio of the ferrite and the area fraction of the hard phase are at the ¼ position of the plate thickness exhibiting an average structure in the plate thickness direction of a steel plate, the resistance of ductile crack initiation is excellent also in the welded heat affected zone and such a steel material is excellent also in the resistance of ductile crack initiation of the base material, and further manufacturing conditions of a steel plate having the microstructure.

We thus provide:

    • (1) A steel material excellent in resistance of ductile crack initiation from welded heat affected zone and a base material has a composition of C: 0.02 to 0.2%, Si: 0.01 to 0.5%, Mn: 0.5 to 2.5%, P: 0.05% or lower, S: 0.05% or lower, Al: 0.1% or lower, and N: 0.01% or lower in terms of % by mass, and the balance Fe with inevitable impurities, in which the microstructure at the ¼ position of the plate thickness contains ferrite and a hard phase, the area fraction of the hard phase is 50 to 90%, and the average aspect ratio of the ferrite is 1.5 or more.
    • (2) The steel material excellent in resistance of ductile crack initiation from welded heat affected zone and a base material according to (1), further contains, in the chemical composition, one or two or more elements selected from Cu: 0.01 to 2%, Ni: 0.01 to 5%, Cr: 0.01 to 3%, Mo: 0.01 to 2%, Nb: 0.1% or lower, V: 0.1% or lower, Ti: 0.1% or lower, B: 0.01% or lower, Ca: 0.01% or lower, and REM: 0.1% or lower in terms of % by mass.
    • (3) In the steel material excellent in resistance of ductile crack initiation from welded heat affected zone and a base material according to (1) or (2) above, the structure on the surface of a steel plate contains ferrite and a hard phase, the area fraction of the ferrite exceeds 40%, and the average aspect ratio of the ferrite grain size exceeds 2.
    • (4) A method for manufacturing a steel material excellent in resistance of ductile crack initiation from welded heat affected zone and a base material includes reheating a steel base material having the chemical compositions of (1) or (2) to 1000° C. or more, rolling the same in such a manner that the rolling reduction rate in a temperature range of 900° C. or more is 50% or more and the rolling finish temperature is Ar3 point to Ar3-50° C., starting water cooling at Ar3-10° C. to Ar3-70° C., and terminating the water cooling at 500° C. or lower.
    • (5) The method for manufacturing a steel material excellent in resistance of ductile crack initiation from welded heat affected zone and a base material according to (4) further includes, after the water cooling, performing tempering treatment at a temperature of lower than the highest heating temperature Ac1 point.

A steel material capable of suppressing ductile crack initiation from welded heat affected zone and a base material that can suppress ductile crack initiation from a stress concentration zone, such as a weld toe, and prevent collapse or break of steel structures even when the steel structures greatly deform due to an earthquake or the like, for example, can be easily and stably mass-produced and industrially remarkable effects are demonstrated.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a view illustrating a ductile crack initiation test method of a welded heat affected zone.

FIG. 2 is a view illustrating influence of the area fraction of a hard phase and the average aspect ratio of ferrite on ductile crack initiation of a 1400° C. simulated heat cycle material.

FIG. 3 is a view illustrating a ductile crack initiation test method of a base material.

FIG. 4 is a view illustrating influence of the area fraction of a hard phase and the average aspect ratio of ferrite on ductile crack initiation of a base material.

 DETAILED DESCRIPTION

The chemical composition and the microstructure are specified. In the description of the chemical composition, % by mass is simply represented by % unless otherwise specified.

Chemical Composition C: 0.02 to 0.2%

C is an element having an action of increasing the strength of steel and, particularly, contributes to the generation of a hard phase. A C content of 0.02% or more is required to obtain such an effect. In contrast, when the C content exceeds 0.2%, the ductility or the bending workability are reduced and also the weldability decreases. Therefore, the C content is limited in the range of 0.02 to 0.2%. More preferably, the C content is 0.02 to 0.18%.

Si: 0.01 to 0.5%

Si acts as a deoxidizing agent and has an action of forming a solid solution to increase the strength of steel. An Si content of 0.01% or more is required to obtain such an effect. In contrast, when the Si content exceeds 0.5%, the toughness is reduced and also the weldability is reduced. Therefor, Si is limited in the range of 0.01 to 0.5%. More preferably, the Si content is 0.01 to 0.4%.

Mn: 0.1 to 2.5%

Mn has an action of increasing the strength of steel and also increasing the toughness through an increase in hardenability. An Mn content of 0.1% or more is required to obtain such an effect. In contrast, when the Mn content exceeds 2.5%, the weldability is reduced. Therefore, Mn is limited in the range of 0.1 to 2.5%. More preferably, the content is 0.5 to 2.0%.

P: 0.05% or lower

Since P causes degradation of toughness, the P content is preferably reduced as much as possible, but the content up to 0.05% is permissible. Therefore, the P content is limited to 0.05% or lower. More preferably, the content is 0.04% or lower.

S: 0.05% or lower

Since S is present as an inclusion in steel and degrades the ductility and the toughness, the S content is preferably reduced as much as possible. However, the content up to 0.05% is permissible. Therefore, the S content is limited to 0.05% or lower. More preferably, the content is 0.04% or lower.

Al: 0.1% or lower

Al is an element that acts as a deoxidizing agent and also contributes to pulverization of crystal grains. However, an excessive content of Al in a proportion exceeding 0.1% causes a reduction in toughness. Therefore, the Al content is limited to 0.1% or lower. More preferably, the content is 0.05% or lower.

N: 0.01% or lower

N is an element that increases the strength of steel by solid solution strengthening similarly as C. However, an excessive content of N causes a reduction in toughness. Therefore, the N content is limited to 0.01% or lower. More preferably, the content is 0.005% or lower.

The chemical compositions described above are basic chemical compositions but one or two or more elements selected from Cu: 0.01 to 2%, Ni: 0.01 to 5%, Cr: 0.01 to 3%, Mo: 0.01 to 2%, Nb: 0.1% or lower, V: 0.1% or lower, Ti: 0.1% or lower, B: 0.01% or lower, Ca: 0.01% or lower, and REM: 0.1% or lower may be further contained according to the desired properties.

Cu: 0.01 to 2%

Cu is an element that has an action of increasing the strength of steel through an increase in hardenability or solid solution. The content of 0.01% or more is required to secure such an effect. In contrast, when the content exceeds 2%, the weldability decreases and also cracks are likely to generate during manufacturing of steel materials. Therefore, when Cu is added, the content is in the range of 0.01 to 2%. More preferably, the content is 0.01 to 1%.

Ni: 0.01 to 5%

Ni is added as required, because Ni contributes to an increase in low temperature toughness, an increase in hardenability, and prevention of hot ductility of Cu when Cu is contained. Such an effect is recognized when Ni is contained in the proportion of 0.01% or more. However, the addition of 5% or more causes a reduction in steel material cost and also a reduction in weldability. Therefore, when Ni is added, the content is in the range of 0.01 to 5%. More preferably, the content is 0.01 to 4.5%.

Cr: 0.01 to 3%

Cr is added as required to increase the strength of steel materials through improvement of hardenability or an increase in tempering softening resistance. Such an effect is recognized when Cr is contained in the proportion of 0.01% or more. In contrast, the addition exceeding 3% reduces weldability and toughness. Therefore, when Cr is added, the content is in the range of 0.01 to 3%. More preferably, the content is in the range of 0.01 to 2.5%.

Mo: 0.01 to 2%

Mo is added as required to increase the strength of steel materials through improvement of hardenability or an increase in tempering softening resistance. Such an effect is recognized when Mo is contained in the proportion of 0.01% or more. In contrast, the addition exceeding 2% reduces weldability or toughness. Therefore, when Mo is added, the content is in the range of 0.01 to 2%. More preferably, the content is in the range of 0.01 to 1%.

Nb: 0.1% or lower

Nb is an element that precipitates as a carbide or a carbonitride in tempering and increases the strength of steel through precipitation strengthening. Moreover, Nb also has an effect of pulverizing austenite grains during rolling to increase toughness. The content of 0.001% or more is preferable to obtain the effects. However, the content exceeding 0.1% reduces toughness. Therefore, when Nb is added, the content is 0.1% or lower. More preferably, the content is 0.05% or lower.

V: 0.1% or lower

V is an element that precipitates as a carbide or a carbonitride in tempering and increases the strength of steel through precipitation strengthening. Moreover, V also has an effect of pulverizing austenite grains during rolling to increase toughness. The content of 0.001% or more is preferable to obtain the effects. However, the content exceeding 0.1% reduces toughness. Therefore, when Nb is added, the content is 0.1% or lower. More preferably, the content is 0.05% or lower.

Ti: 0.1% or lower

Ti is added as required because Ti has an effect of pulverizing austenite in a welded heat affected zone to increase toughness. The content of 0.001% or more is preferable to obtain the effect. However, the addition exceeding 0.1% reduces toughness and also causes a sudden rise of steel material cost. Therefore, when Ti is added, the content is 0.1% or lower. More preferably, the content is 0.05% or lower.

B: 0.01% or lower

B is added as required because B has an effect of increasing hardenability and increasing the strength of steel with a small content thereof. The content is preferably 0.0001% or more to obtain the effect. However, the addition exceeding 0.01% reduces weldability. Therefore, when B is added, the content is 0.01% or lower. More preferably, the content is 0.005% or lower.

Ca: 0.01% or lower

Ca is added as required because Ca increases the base material toughness by controlling the shape of a CaS inclusion and further increase the toughness of a welded heat affected zone. The content of 0.0001% or more is preferable to obtain the effects. However, the addition exceeding 0.01% reduces toughness due to an increase in the amount of the CaS inclusion. Therefore, when Ca is added, the content is 0.01% or lower. More preferably, the content is 0.009% or lower.

REM: 0.1% or lower

REM is an element that increases the toughness of a welded heat affected zone and is added as required. The content is preferably 0.0001% or more to obtain the effect. However, the addition exceeding 0.1% causes a reduction in toughness. Therefore, when REM is added, the content is 0.1% or lower. More preferably, the content is 0.05% or lower.

REM is a general term of Y, Ce and the like that are rare earth elements and the addition amount as used herein refers to the total amount of these rare earth elements.

Microstructure

The steel material has a microstructure in which the structure at the ¼ position of the plate thickness contains ferrite and a hard phase, the area fraction of the hard phase is 50 to 90%, and the average aspect ratio of the ferrite grain size is 1.5 or more. When the area fraction of the hard phase is lower than 50% and exceeds 90% or the aspect ratio of the ferrite grain size is lower than 1.5, there is a possibility that ductile crack initiation occurs.

The upper limit of the average aspect ratio of the ferrite grain size does not need to particularly specify and is 5 or lower in view of the capability and the like of a rolling mill. The area fraction of the hard phase is more preferably 52 to 90% and the average aspect ratio of the ferrite grain size is more preferably 1.6 or more. The average aspect ratio is more preferably 1.7 or more.

In a two phase mixed structure containing ferrite and a hard phase, the yield ratio (or Y/T ratio) of a base material decreases, and the strain concentration in a stress concentration zone is eased even in the base material as it is or even after a simulated heat cycle of simulating the welded heat affected zone. Such an effect is not obtained in the case of a single phase of ferrite or a single phase of a hard phase.

In the steel material, the structure of the surface of a steel plate (1 mm position from the plate surface) contains ferrite and a hard phase, in which the area fraction of the ferrite exceeds 40% and is more preferably 50% or more. The average aspect ratio of the ferrite grain size exceeds 2. When the area fraction of the ferrite is lower than 40% or the average aspect ratio of the ferrite grain size is 2 or lower, the resistance of ductile crack initiation in a welded heat affected zone is poor.

The hard phase is bainite, martensite, or a bainite/martensite mixed structure and contains 5% or lower, in terms of area fraction, of an island martensite (M-A constituent) (MA).

FIG. 2 illustrates the results of examining the resistance of ductile crack initiation using a simulated heat cycle specimen of a welded zone (highest heating temperature of 1400° C.). As illustrated in FIG. 2, when the area fraction of the hard phase of the base material is 50 to 90% and the average aspect ratio of the ferrite thereof is 1.5 or more, ductile crack initiation is not observed also after the simulated heat cycle.

The results illustrated in FIG. 2 were obtained by specimens of 12 mm thickness (=plate thickness direction)×12 mm width×200 length from the ¼ center of the plate thickness (½ center of the plate thickness in the case of a plate thickness of 25 mm or lower) from the steel materials obtained by producing steel having a composition in our range by various manufacturing methods and changing the microstructure, and then giving a simulated heat cycle (time for reaching the highest heating temperature: 6 s, cooling rate from the highest heating temperature to room temperature: 40° C./s) of a welded zone thereto by a Gleeble tester to obtain sample materials.

FIG. 1 illustrates the specimen shape and the test conditions. The sample material (specimen 1), to which the simulated heat cycle was given, in which a single through-thickness edge notch is introduced with the length of 3 mm in the plate thickness direction into the center of a simulated heat cycle zone 2 of the sample material (specimen 1) was fixed with clamps 5, then a tensile load (arrow 6) was applied to 0.6 mm in terms of displacement of a clip gage 3 between knife-edges 4 that are screwed, the load was removed, and then the specimen was ground to the central zone and mirror polished. Then, the presence of crack initiation at the notch tip was evaluated. The case where the ductile crack from the notch bottom was 50 μm or more was defined as crack initiation.

It is considered that the results illustrated in FIG. 2 are obtained due to the fact that the yield ratio (or Y/T ratio) (0.2% proof stress/tensile strength) decreased also in the structure after the simulated heat cycle and the degree of distortion concentration at the notch tip zone decreased by the use of the base material having a complex structure of ferrite and a hard phase.

Such outstanding characteristics were observed in common also in a base material to which the simulated heat cycle was not given.

More specifically, FIG. 4 illustrates the results of examining the influence of the microstructure of the base material exerted on the resistance of ductile crack initiation. As illustrated in FIG. 4, when the area fraction of the hard phase of the base material is 50 to 90% and the average aspect ratio of the ferrite is 1.5 or more, ductile crack initiation is not accepted.

The results of the base material illustrated in FIG. 4 were obtained by specimens of 12 mm thickness (=plate thickness direction)×12 mm width×200 length from the ¼ center of the plate thickness (½ center of the plate thickness in the case of a plate thickness of 25 mm or lower) from steel materials obtained by producing steel having a composition in our range by various manufacturing methods and changing the microstructure.

FIG. 3 illustrates the specimen shape and the test conditions. The sample material (specimen 1) in which a single through-thickness edge notch is introduced into the center was fixed with clamps 5, then a tensile load (arrow 6) was applied to 0.8 mm in terms of displacement of a clip gage 3 between knife-edges 4 that are screwed, the load was removed, and then the specimen was ground to the central zone and mirror polished. Then, the presence of crack initiation at the notch tip was evaluated. The case where the ductile crack from the notch bottom was 50 μm or more was defined as crack initiation.

We believe that the results illustrated in FIG. 4 are obtained due to the fact that the yield ratio (or Y/T ratio) (0.2% proof stress/tensile strength) decreased and the degree of distortion concentration at the notch tip zone decreased by the use of a base material having a complex structure of ferrite and a hard phase.

Moreover, it is also considered to be one of the factors that the slip plane greatly leaned to the crack initiation direction in the base material as it is and also after the simulated heat cycle by increasing the average aspect ratio of the ferrite, i.e., the development of the specific aggregate structure. The aspect ratio refers to the ferrite grain size in the rolling direction (major axis)/the ferrite grain size in the plate thickness direction (minor axis) in a cross section parallel to the rolling direction.

The same results as those of FIG. 2 were obtained also when the highest heating temperature of the simulated heat cycle was 760° C., 900° C., and 1200° C.

The steel material is obtained by successively subjecting the steel material of the above-described chemical compositions to a hot rolling process, a water cooling process, or further a tempering process.

The hot rolling includes reheating to 1000° C. or more and performing rolling in such a manner that the rolling reduction rate in a temperature range of 900° C. or more is 50% or more and the rolling finish temperature becomes Ar3 to Ar3-50° C. A more preferable rolling finish temperature is lower than Ar3 to Ar3-40° C. By setting the rolling finish temperature in the invention range, processing strain (or residual strain) can be added to ferrite generated during rolling to thereby increase the aspect ratio of the ferrite. When the reheating temperature is lower than 1000° C., hot rolling that gives a desired cumulative rolling reduction rate cannot be performed to the steel material.

When the cumulative rolling reduction rate at 900° C. or more is lower than 50%, desired strength and toughness cannot be secured. When the rolling finish temperature exceeds Ar3, the aspect ratio of ferrite does not reach 1.5 or more. When the rolling finish temperature is lower than Ar3-50° C., the area fraction of the hard phase obtained by the subsequent water cooling does not reach 50% or more.

In the water cooling process, the water cooling is started at Ar3-10° C. to Ar3-70° C. immediately after hot rolling, and then the water cooling is terminated at 500° C. or lower. When the water cooling start temperature exceeds Ar3-10° C., ferrite of lower than 10% in terms of area fraction (hard phase exceeding 90% in terms of area fraction) precipitates. When the water cooling start temperature is lower than Ar3-70° C. or water cooling is not started immediately after (within 300 seconds) hot rolling, ferrite exceeding 50% in terms of area fraction (hard phase not reaching 50% in terms of area fraction) or pearlite, which is not intended to precipitate, precipitates. Thus, desired characteristics cannot be satisfied.

After performing the cooling, tempering treatment can be further performed at a temperature of lower than the Ac1 point. By performing tempering treatment, toughness and ductility increase, and desired strength and toughness can be achieved. When the tempering temperature exceeds the Ac1 point, a large amount of island martensite generates to reduce the toughness.

The Ar3 point and the Ac1 point can be calculated by the following equation based on the content (% by mass) of each chemical composition:


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


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

The disclosure will be described in more detail based on Examples.

EXAMPLES

Steel materials containing the chemical compositions shown in Table 1 were subjected to hot rolling at the conditions shown in Table 2 to thereby obtain steel plates having a plate thickness of 12 to 100 mm.

The obtained steel plates were subjected to microstructure observation, a tensile test, a toughness test, a ductile crack initiation test after a simulated heat cycle, and a ductile crack initiation test of base materials. The test methods were performed as described in the following items (1) to (5).

(1) Microstructure Observation

From the obtained steel plates, specimens were extracted in the cross section parallel to the rolling direction. Then, the specimens were mirror polished, and then etched with nital. Thereafter, the microstructure at the ¼ position of the plate thickness and the microstructure 1 mm below the surface were observed. The observation of each of the positions was performed with Field number: 20 fields of view. The area fraction was determined by binarizing the ferrite and the hard phase and observing at a magnification of 200×. The average aspect ratio of the ferrite was determined by determining the length in the rolling direction and the length in the plate thickness direction of each ferrite present in the field of view at a magnification of 400×, determining the length in the rolling direction/the length in the plate thickness direction, and then determining the average value thereof

(2) Tensile Test

From the obtained steel plates, full thickness JIS No. 5 specimens were extracted so that the tensile direction was perpendicular to the rolling direction of the steel plate according to the regulation of JIS Z 2201 (1998). The tensile test was performed according to JIS Z 2241 (1998), and then the 0.2% proof (σ0.2) and the tensile strength (TS) were determined to evaluate the static tensile properties.

(3) Toughness Test

From the obtained steel plates, V notch specimens were extracted so that the longitudinal direction was in parallel to the rolling direction according to the regulation of JIS Z 2242 (2005), and then the ductile-brittle fracture transition temperature was determined to evaluate the toughness. The specimens were extracted in such a manner that the ¼ position of the plate thickness when the plate thickness was 20 mm or more or the ½ position of the plate thickness when the plate thickness was lower than 20 mm was the center.

(4) Ductile Crack Initiation Test after Simulated Heat Cycle

From the obtained steel plates, specimens of 12 mm thickness (=plate thickness direction=t)×12 mm width and 200 mm in full length were extracted at the ¼ center of the plate thickness (½ center of the plate thickness when the plate thickness was 25 mm or lower). The specimens were subjected to a simulated heat cycle of a welded heat affected zone in which the highest heating temperature was 760° C., 900° C., 1200° C., and 1400° C. (time for reaching the highest heating temperature: 6 s, Cooling rate from the highest heating temperature to room temperature: 40° C./s) using a Gleeble tester.

Thereafter, as illustrated in FIG. 1, a single through-thickness edge notch was introduced with the length of 3 mm in the plate thickness direction into the center of the simulated heat cycle zone. The notch processing was carried out by electrical discharge machining, and the notch tip radius was 0.1 mm.

In the test, a tensile load was applied while gripping the specimens with both right and left ends thereof with a constraint length of 50 mm. During the test, the displacement between the knife-edges screwed near the notch was measured with the clip gage. A tensile load was applied to 0.6 mm in terms of clip gage displacement, and then the load was removed. Thereafter, the specimen was ground to the width center and mirror polished. Then, the crack initiation state at the notch bottom was analyzed under a microscope with a magnification of 50×. It was defined that the ductile crack initiation occurred when a ductile crack extended in the length of 50 μm or more from the notch bottom.

(5) Ductile Crack Initiation Test of Base Material

From the obtained steel plates, specimens of 12 mm thickness (=plate thickness direction=t)×12 mm width and 200 mm in full length were extracted at the ¼ center of the plate thickness (½ center of the plate thickness when the plate thickness was 25 mm or lower).

To the obtained specimens, a single through-thickness edge notch was introduced with the length of 3 mm in the plate thickness direction into the center of the specimens as illustrated in FIG. 3. The notch processing was carried out by electrical discharge machining, and the notch tip radius was 0.1 mm.

In the test, a tensile load was applied while gripping the specimens with both right and left ends thereof with a constraint length of 50 mm. During the test, the displacement between the knife-edges screwed near the notch was measured with the clip gage. A tensile load was applied to 0.8 mm in terms of clip gage displacement, and then the load was removed. Thereafter, the test was ground to the width center and mirror polished. Then, the crack initiation state at the notch bottom was analyzed under a microscope with a magnification of 50×. It was defined that the ductile crack initiation occurred when a ductile crack extended in the length of 50 μm or more from the notch bottom.

With respect to the specimens that were subjected to the simulated heat cycle, the obtained experimental results are shown in Table 3. All of the steel plates of Nos. 1 to 10 produced using the chemical compositions and our manufacturing method have our structure. We found that the steel plates have excellent strength and toughness and have excellent resistance of ductile crack initiation of a welded heat affected zone.

In contrast, the steel plate (Steel type K*) of No. 11 in which the C content does not satisfy the lower limit of our range has low tensile strength. The steel plate (Steel type L*) of No. 12 in which the content of each of C, P, and S exceeds the upper limit of our range has low toughness and has poor ductile crack initiation characteristics of a welded heat affected zone.

The steel plate of No. 13 in which the reheating temperature of slab is lower than our and the cumulative rolling reduction rate at 900° C. or more is outside our range has low toughness. In the steel plate of No. 14 in which the rolling finish temperature and the water cooling start temperature exceed our range, ferrite is not generated, our microstructure is not obtained, and the resistance of ductile crack initiation of a welded heat affected zone is poor.

In the steel plate of No. 15 in which the cooling start temperature is lower than our range and the steel plate of No. 16 in which the water cooling stop temperature exceeds our range, the hard phase area fraction and the average aspect ratio of ferrite do not satisfy our values and both the steel plates have low tensile strength and poor resistance of ductile crack initiation of welded heat affected zones. In the steel plate of No. 17 in which the tempering temperature exceeds our range, since a large amount of island martensite is generated, the toughness is low and the resistance of ductile crack initiation of a welded heat affected zone is poor.

The obtained experimental results of the base material are shown in Table 4. All of the steel plates of Nos. 18 to 27 produced using the chemical compositions and our manufacturing method have our structure. We found that the steel plates have excellent strength and toughness and have excellent resistance of ductile crack initiation of a welded heat affected zone.

In contrast, the steel plate (Steel type W*) of No. 28 in which the C content does not satisfy the lower limit of our range has low tensile strength. The steel plate (Steel type X*) of No. 29 in which the content of each of C, P, and S exceeds the upper limit of our range has low toughness. The steel plate of No. 30 in which the reheating temperature of slab is lower than our range and the cumulative rolling reduction rate at 900° C. or more does not satisfy our range has low toughness.

In the steel plate of No. 31 in which the rolling finish temperature and the water cooling start temperature exceed our range, ferrite is not generated, our microstructure is not obtained, and the resistance of ductile crack initiation is poor.

In the steel plate of No. 32 in which the cooling start temperature is lower than our range and the steel plate of No. 33 in which the water cooling stop temperature exceeds our range, the hard phase area fraction and the average aspect ratio of ferrite do not satisfy our values and both the steel plates have low tensile strength and poor resistance of ductile crack initiation. In the steel plate of No. 34 in which the tempering temperature exceeds our value, a large amount of island martensite (M-A constituent) is generated. Thus, the toughness is low and the resistance of ductile crack initiation is poor.

REFERENCE SIGNS LIST

    • 1. Specimen
    • 2. Simulated heat cycle zone
    • 3. Clip gage
    • 4. Knife-edge
    • 5. Clamp
    • 6. Tensile load

TABLE 1 Steel Chemical composition (mass %) type C Si Mn P S Cu Ni Cr Mo Nb V A 0.14 0.33 1.59 0.005 0.002 — — — — — — B 0.06 0.11 1.96 0.009 0.001 0.25 0.14 0.04 0.21 0.046 0.005 C 0.18 0.04 1.16 0.006 0.005 — — — — — 0.048 D 0.12 0.39 0.54 0.008 0.003 — — 0.22 0.35 — — E 0.03 0.26 0.52 0.003 0.005 — 4.49 — — 0.012 — F 0.09 0.32 1.32 0.042 0.007 0.98 1.33 — — 0.022 0.015 G 0.08 0.24 1.18 0.002 0.009 — — 2.48 0.98 0    0.018 H 0.11 0.18 1.22 0.001 0.004 — 0.52 0.16 0.21 0.045 0.033 I 0.05 0.32 1.38 0.002 0.043 — 2.43 — 0.25 0.033 0.019 J 0.09 0.25 1.44 0.005 0.002 — — 0.08 0.11 0.022 0.038 K* 0.01* 0.21 1.56 0.004 0.003 — — — — — — L* 0.32* 0.18 0.55 0.193* 0.183* 0.25 0.15 0.23 0.14 — — M 0.15 0.32 1.58 0.006 0.001 — — — — — — N 0.06 0.12 1.95 0.008 0.004 0.22 0.15 0.02 0.21 0.045 0.004 O 0.19 0.02 1.15 0.005 0.005 — — — — — 0.047 P 0.11 0.38 0.52 0.007 0.003 — — 0.21 0.33 — — Q 0.03 0.25 0.51 0.003 0.004 — 4.51 — — 0.018 — R 0.08 0.31 1.33 0.041 0.006 0.95 1.26 — — 0.025 0.011 S 0.09 0.20 1.14 0.003 0.004 — — 2.45 0.97 — 0.009 T 0.12 0.16 1.25 0.004 0.003 — 0.55 0.15 0.22 0.043 0.032 U 0.05 0.27 1.37 0.001 0.042 — 2.42 — 0.28 0.032 0.019 V 0.09 0.22 1.44 0.003 0.003 — — 0.07 0.15 0.028 0.042 W* 0.01* 0.25 1.55 0.005 0.004 — — — — — — X* 0.31* 0.15 0.51 0.180* 0.173* 0.23 0.11 0.21 0.15 — — Chemical composition Ar3 Ac1 Steel (mass %) [° C.] [° C.] type Ti B Ca REM Al N Note (1) Note (2) A — — — — 0.033 0.0048 739 729 B 0.011 0.0003 — — 0.032 0.0042 705 697 C — — — — 0.044 0.0029 761 708 D — — — 0.097 0.029 0.0041 798 729 E 0.049 — — — 0.018 0.0029 612 657 F — — 0.0089 0.031 0.022 0.0031 684 692 G — — — — 0.025 0.0028 675 770 H 0.017 0.0046 — — 0.018 0.0035 731 706 I — — 0.0033 0.044 0.022 0.0028 630 676 J 0.013 0.0011 — — 0.032 0.0041 757 710 K* — — — — 0.028 0.0039 782 706 L* — — 0.0022 0.008 0.022 0.0038 739 722 M — — — — 0.032 0.0048 737 729 N 0.012 0.0002 — — 0.031 0.0041 706 697 O — — — — 0.048 0.0029 759 707 P — — — 0.098 0.028 0.0042 805 729 Q 0.048 — — — 0.016 0.0028 612 656 R — — 0.0091 0.032 0.017 0.0041 691 693 S — — — — 0.022 0.0032 677 769 T 0.018 0.0048 — — 0.011 0.0035 723 705 U — — 0.0032 0.048 0.023 0.0028 629 675 V 0.012 0.0015 — — 0.032 0.0041 754 709 W* — — — — 0.031 0.0039 783 707 X* — — 0.0021 0.011 0.028 0.0037 747 722 Note: The cells marked by * are outside our range and the steel types K, L, W, and X are comparative steels. Note (1): Ar3(° C.) = 910-310 C—80 Mn—20 Cu—15 Cr—55 Ni—80 Mo Each alloy element amount indicates the content (%). Note (2): Ar1(° C.) = 723-14 Mn + 22 Si—14.4 Ni + 23.3 Cr Each alloy element amount indicates the content (%).

TABLE 2 Cumulative rolling Water Water Slab reduction Rolling cooling cooling Plate reheating rate at finish start stop Tempering Steel thickness temperature 900° C. or temperature temperature temperature temperature No. type (mm) [° C.] more [%] [° C.] [° C.] [° C.] [° C.] 1 A 14 1160 87 702 683 431 — 2 B 22 1190 75 679 665 378 — 3 C 12 1210 92 731 687 298 — 4 D 100 1150 56 782 779 421 — 5 E 75 1240 62 583 578  72 620 6 F 35 1190 73 672 634 388 — 7 G 24 1150 81 641 623  28 580 8 H 68 1240 55 701 687 426 — 9 I 34 1170 72 607 598 426 — 10 J 18 1160 82 718 704 388 — 11 K* 22 1120 78 748 726 315 — 12 L* 45 1180 68 725 706 248 — 13 C 73  970*  34* 741 732  42 650 14 A 14 1160 87  785*  777* 413 — 15 B 28 1230 72 695  600* 388 — 16 J 19 1240 78 712 699  638* — 17 D 75 1090 64 768 749  62  760* 18 M 15 1150 86 695 681 401 — 19 N 20 1180 76 686 664 308 — 20 O 12 1200 91 721 697 498 — 21 P 100 1130 55 792 777 418 — 22 Q 75 1250 61 602 589 25 600 23 R 35 1200 72 668 643 418 — 24 S 25 1160 73 647 625  72 500 25 T 72 1250 58 708 697 457 — 26 U 37 1170 71 618 605 412 — 27 V 15 1150 83 723 703 378 — 28 W* 25 1100 84 758 748 258 — 29 X* 48 1200 69 721 710 243 — 30 O 75  930*  33* 737 717  23 600 31 M 15 1150 88  755*  747* 428 — 32 N 25 1220 71 679  605* 352 — 33 V 18 1250 77 715 703  658* — 34 P 77 1080 62 776 748 245  750* Note: The steel types marked by * are outside our range.

TABLE 3 Microstructure of Microstructure 1 mm ¼ Plate thickness/4 below the surface Hard Hard phase Hard Ferrite phase Ferrite Ferrite struc- phase average struc- phase average Ductile crack initiation ture fraction aspect ture fraction aspect σ0.2 TS vTrs characteristics Note (2) Classi- No. Note (1) [%] ratio Note (1) [%] ratio [MPa] [MPa] [° C.] 760° C. 900° C. 1200° C. 1400° C. fication 1 B 59 1.9 B 55 2.4 428 548 −57 ∘ ∘ ∘ ∘ Example 2 B 75 2.2 B 68 3.1 563 728 −105  ∘ ∘ ∘ ∘ Example 3 B, M 54 2.3 B, M 77 4.8 521 689 −33 ∘ ∘ ∘ ∘ Example 4 B 64 1.6 B 48 2.2 408 521 −29 ∘ ∘ ∘ ∘ Example 5 TB 90 1.7 TM 41 2.6 555 667 −98 ∘ ∘ ∘ ∘ Example 6 B 62 1.8 B 59 2.3 473 621 −47 ∘ ∘ ∘ ∘ Example 7 TM 55 2.1 TM 72 2.4 481 582 −92 ∘ ∘ ∘ ∘ Example 8 B 83 1.8 B 42 2.1 529 683 −64 ∘ ∘ ∘ ∘ Example 9 B 87 1.7 B 40 2.2 433 538 −41 ∘ ∘ ∘ ∘ Example 10 B 75 2.5 M 58 3.3 428 548 −72 ∘ ∘ ∘ ∘ Example 11 B 73 2.2 B 53 3.0 325  421* −18 ∘ ∘ ∘ ∘ Comparative Example 12 B, M 72 1.7 B, M 43 2.3 677 991   15* ∘ x x x Comparative Example 13 TM 72 2.3 TM 40 2.5 521 609   8* ∘ ∘ ∘ ∘ Comparative Example 14 B 100* — B  0* —* 548 678 −21 x x x x Comparative Example 15 P  14*  1.1* P 87  1.4* 344  472* −11 x x x x Comparative Example 16 P  21*  1.3* P 81  1.4* 388  488* −18 x x x x Comparative Example 17 B, MA 63 1.8 M, MA 48 2.8 521 622   6* x x x x Comparative Example Note: The cells marked by * are outside our range. Note (1): B: Bainite., M: Martensite, P: Pearlite, TB: Tempered bainite, TM: Tempered martensite, MA: Island martensite Note (2): ∘: No ductile crack initiation x: Ductile crack initiation

TABLE 4 Microstructure of Microstructure 1 mm ¼ Plate thickness below the surface Hard Hard Ferrite Hard Ferrite Ferrite Ductile crack phase phase average phase phase average initiation structure fraction aspect structure fraction aspect σ0.2 TS vTrs characteristics No. Note (1) [%] ratio Note (1) [%] ratio [MPa] [MPa] [° C.] Note (2) Classification 18 B 55 1.8 B 57 3.1 436 528 −48 ∘ Example 19 B 72 2.1 B 42 4.9 573 726 −121  ∘ Example 20 B, M 52 2.2 B, M 66 3.9 511 698 −21 ∘ Example 21 B 62 1.6 B 48 2.2 359 515 −28 ∘ Example 22 TB 89 1.8 TM 41 4.1 552 628 −111  ∘ Example 23 B 68 1.9 B 49 2.8 487 615 −35 ∘ Example 24 TM 59 2.0 TM 57 3.1 472 577 −98 ∘ Example 25 B 84 1.6 B 42 2.7 507 641 −63 ∘ Example 26 B 88 1.7 B 43 2.9 402 513 −34 ∘ Example 27 B 77 2.4 B 53 3.3 425 538 −66 ∘ Example 28 B 74 2.1 M 58 3.7 368  411* −38 ∘ Comparative Example 29 B, M 78 1.8 M 55 2.2 687 983  10* ∘ Comparative Example 30 TM 69 2.4 TM 42 2.4 513 618   7* ∘ Comparative Example 31 B 100* — B  0* —:* 558 688 −18 x Comparative Example 32 P  12*  1.2* P 89  1.4* 358  451* −13 x Comparative Example 33 P  18*  1.4* P 83  1.4* 398  473* −21 x Comparative Example 34 B, MA 68 1.7 M, MA 44 2.8 535 637   5* x Comparative Example Note: The cells marked by * are outside our range. Note (1): B: Bainite., M: Martensite, P: Pearlite, TB: Tempered bainite, TM: Tempered martensite, MA: Island martensite Note (2): ∘: No ductile crack initiation x: Ductile crack initiation

Claims

1. A steel material excellent in resistance of ductile crack initiation from welded heat affected zone and a base material,

comprising:
a composition of C: 0.02 to 0.2%, Si: 0.01 to 0.5%, Mn: 0.5 to 2.5%, P: 0.05% or lower, S: 0.05% or lower, Al: 0.1% or lower, and N: 0.01% or lower in terms of % by mass, and the balance Fe with inevitable impurities,
having a microstructure at ¼ position of plate thickness containing ferrite and a hard phase,
an area fraction of the hard phase of 50 to 90%, and
an average aspect ratio of the ferrite of 1.5 or more.

2. The steel material according to claim 1, further comprising, in the chemical composition, one or more elements selected from the group consisting of Cu: 0.01 to 2%, Ni: 0.01 to 5%, Cr: 0.01 to 3%, Mo: 0.01 to 2%, Nb: 0.1% or lower, V: 0.1% or lower, Ti: 0.1% or lower, B: 0.01% or lower, Ca: 0.01% or lower, and REM: 0.1% or lower in terms of % by mass.

3. The steel material according to claim 1, wherein the microstructure on a surface of a steel plate contains ferrite and a hard phase, the area fraction of the ferrite exceeds 40%, and the average aspect ratio of the ferrite grain size exceeds 2.

4. A method for manufacturing a steel material excellent in resistance of ductile crack initiation from welded heat affected zone and a base material comprising:

reheating a steel base material of claim 1 to 1000° C. or more,
rolling the same such that a rolling reduction rate in a temperature range of 900° C. or more is 50% or more and a rolling finish temperature is Ar3 point to Ar3-50° C.,
starting water cooling at Ar3-10° C. to Ar3-70° C., and
terminating the water cooling at 500° C. or lower.

5. The method according to claim 4 further comprising, after the water cooling, performing tempering treatment at a temperature lower than the highest heating temperature Ac1 point.

6. The steel material according to claim 2, wherein the microstructure on a surface of a steel plate contains ferrite and a hard phase, the area fraction of the ferrite exceeds 40%, and the average aspect ratio of the ferrite grain size exceeds 2.

7. A method for manufacturing a steel material excellent in resistance of ductile crack initiation from welded heat affected zone and a base material comprising:

reheating a steel base material of claims 2 to 1000° C. or more,
rolling the same such that a rolling reduction rate in a temperature range of 900° C. or more is 50% or more and a rolling finish temperature is Ar3 point to Ar3-50° C.,
starting water cooling at Ar3-10° C. to Ar3-70° C., and
terminating the water cooling at 500° C. or lower.
Patent History
Publication number: 20130000798
Type: Application
Filed: Dec 25, 2009
Publication Date: Jan 3, 2013
Applicant: JFE STEEL CORPORATION (Tokyo)
Inventors: Teruki Sadasue (Tokyo), Satoshi Igi (Tokyo)
Application Number: 13/141,373
Classifications
Current U.S. Class: With Flattening, Straightening, Or Tensioning By External Force (148/645); Ferrous (i.e., Iron Base) (148/320); Copper Containing (148/332); Nickel Containing (148/336); Chromium Containing, But Less Than 9 Percent (148/333); Beryllium Or Boron Containing (148/330); Three Percent Or More Manganese Containing Or Containing Other Transition Metal In Any Amount (148/337); Rare Earth Meal Containing (148/331)
International Classification: C22C 38/04 (20060101); C22C 38/08 (20060101); C22C 38/12 (20060101); C21D 8/00 (20060101); C22C 38/06 (20060101); C22C 38/14 (20060101); C22C 38/16 (20060101); C22C 38/18 (20060101);