HIGH-STRENGTH STEEL SHEET AND METHOD FOR MANUFACTURING THE SAME

- JFE STEEL CORPORATION

A high strength steel sheet has a tensile strength of 900 MPa or higher that can achieve both high strength and good formability and a composition including, on a mass basis, C: 0.1% or more and 0.3% or less; Si: 2.0% or less; Mn: 0.5% or more and 3.0% or less; P: 0.1% or less; S: 0.07% or less; Al: 1.0% or less; and N: 0.008% or less, with the balance Fe and incidental impurities. The steel sheet microstructure includes, on an area ratio basis, 5% or more and 80% or less of ferrite, 15% or more of autotempered martensite, 10% or less of bainite, 5% or less of retained austenite, and 40% or less of as-quenched martensite; the mean hardness of the autotempered martensite is HV≦700; and the mean number of precipitated iron-based carbide grains each having a size of 5 nm or more and 0.5 μm or less and included in the autotempered martensite is 5×104 or more per 1 mm2.

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Description
RELATED APPLICATIONS

This is a §371 of International Application No. PCT/JP2009/051915, with an international filing date of Jan. 29, 2009 (WO 2009/096596 A1, published Aug. 6, 2009), which is based on Japanese Patent Application Nos. 2008-021403, filed Jan. 31, 2008, and 2009-015840, filed Jan. 27, 2009, the subject matter of which is incorporated by reference.

TECHNICAL FIELD

This disclosure relates to a high strength steel sheet that is used in industrial fields such as the automobile and electrical industries, has good formability, and has a tensile strength of 900 MPa or higher and a method for manufacturing the same. The high strength steel sheet includes steel sheets whose surface is galvanized or galvannealed.

BACKGROUND

In recent years, the improvement in the fuel efficiency of automobiles has been an important subject from the viewpoint of global environmental conservation. Therefore, by employing a high strength automobile material, there has been an active move to reduce the thickness of components and thus to lighten the automobile body itself. However, since an increase in the strength of steel sheets reduces workability, the development of materials having both high strength and good workability has been demanded. To satisfy such a demand, various multiple-phase steel sheets such as a ferrite-martensite dual-phase steel (DP steel) and a TRIP steel that uses transformation-induced plasticity of retained austenite have been developed.

For example, the following disclose DP steels. JP 1853389 discloses a high strength steel sheet with a low yield ratio that is excellent in surface quality and bendability and has a tensile strength of 588 to 882 MPa and a method for manufacturing the steel sheet, by specifying the composition and the hot-rolling and annealing conditions. JP 3610883 discloses a high strength cold-rolled steel sheet with excellent bendability and a method for manufacturing the steel sheet, by specifying the hot-rolling, cold-rolling, and annealing conditions of steel having a certain composition. JP 11-61327 discloses a steel sheet that is excellent in collision safety and formability and a method for manufacturing the steel sheet, by specifying the volume fraction and grain diameter of martensite and the mechanical properties. JP 2003-213369 discloses a high strength steel sheet, a high strength galvanized steel sheet, and a high strength galvannealed steel sheet that are excellent in stretch-flangeability and crashworthiness and a method for manufacturing the steel sheets, by specifying the composition and the volume fraction and grain diameter of martensite. JP 2003-213370 discloses a high strength steel sheet, a high strength galvanized steel sheet, and a high strength galvannealed steel sheet that are excellent in stretch-flangeability, shape fixability, and crashworthiness and a method for manufacturing the steel sheets, by specifying the composition, the grain diameter and microstructure of ferrite, and the volume fraction of martensite. JP 2003-505604 discloses a high strength steel sheet having excellent mechanical properties and a method for manufacturing the steel sheet, by specifying the composition, the amount of martensite, and the manufacturing method. JP 6-093340 and JP 6-108152 each disclose a high strength galvanized steel sheet that is excellent in stretch-flangeability and bendability and a method and facility for manufacturing the steel sheet, by specifying the composition and the manufacturing conditions in a galvanizing line.

The following disclose steel sheets having a microstructure including a phase other than martensite as a hard second phase. JP 7-011383 discloses a steel sheet that is excellent in fatigue properties, by employing martensite and/or bainite as a hard second phase and specifying the composition, the grain diameter, the hardness ratio, and the like. JP 10-060593 discloses a steel sheet that is excellent in stretch-flangeability, by mainly employing bainite or pearlite as a second phase and specifying the composition and the hardness ratio. JP 2005-281854 discloses a high-strength and ductility galvanized steel sheet that is excellent in hole expandability and a method for manufacturing the steel sheet, by employing bainite and martensite as a hard second phase. JP 3231204 discloses a multiple-phase steel sheet that is excellent in fatigue properties by employing bainite and martensite as a hard second phase and specifying the fraction of constituent phases, the grain diameter, the hardness, and the mean free path of the entire hard phase. JP 2001-207234 discloses a high strength steel sheet that is excellent in ductility and hole expandability, by specifying the composition and the amount of retained austenite. JP 7-207413 discloses a high strength multiple-phase cold-rolled steel sheet that is excellent in workability, by employing a steel sheet including bainite and retained austenite and/or martensite and specifying the composition and the fraction of phases. JP 2005-264328 discloses a high strength steel sheet that is excellent in workability and a method for manufacturing the steel sheet, by specifying the distribution state of the grains of a hard second phase in ferrite and the ratio of the grains of tempered martensite and bainite to the grains of ferrite. JP 2616350 discloses an ultra-high strength cold-rolled steel sheet that is excellent in delayed fracture resistance and has a tensile strength of 1180 MPa or higher and a method for manufacturing the steel sheet, by specifying the composition and the manufacturing process. JP 2621744 discloses an ultra-high strength cold-rolled steel sheet that is excellent in bendability and has a tensile strength of 980 MPa or higher and a method for manufacturing the steel sheet, by specifying the composition and the manufacturing method. JP 2826058 discloses an ultra-high strength thin steel sheet that has a tensile strength of 980 MPa or higher and whose hydrogen embrittlement is prevented by limiting the number of iron-based carbide grains in tempered martensite to a certain number and a method for manufacturing the steel sheet.

However, the above-described disclosures pose the problems below. JP 1853389, JP 3610883, JP 11-061327, JP 2003-213369, JP 2003-213370, JP 2003-505604, JP 6-093340, JP 7-011383, JP 10-060593, JP 3231204, JP 2001-207234 and JP 7-207413 disclose steel sheets having a tensile strength of lower than 900 MPa, and the workability often cannot be maintained if the strength is further increased. JP 1853389 describes that annealing is performed in a single phase region and the subsequent cooling is performed to 400° C. at a cooling rate of 6 to 20° C./s. However, in the case of a galvanized steel sheet, the adhesion of a coating needs to be taken into account and heating needs to be performed before coating because 400° C. is lower than the temperature of a coating bath. Thus, the galvanized steel sheet cannot be manufactured in a continuous galvanizing and galvannealing line having no heating equipment before the coating bath. In JP 6-093340 and JP 6-108152, since tempered martensite needs to be formed during the heat treatment in a galvanizing line, there is required equipment for reheating the steel sheet after the cooling to Ms temperature or lower. In JP 2005-281854, bainite and martensite are employed as a hard second phase and the fraction is specified. However, the characteristics significantly vary in the specified range, and the operating conditions need to be precisely controlled to suppress the variation. In JP 2005-264328, since cooling is performed to Ms temperature or lower to form martensite before bainite transformation, equipment for reheating the steel sheet is required. Furthermore, the operating conditions need to be precisely controlled to achieve stable characteristics. Consequently, the costs for equipment and operation are increased. In JP 2616350 and JP 2621744, the steel sheet needs to be maintained in a bainite-formation temperature range after annealing to obtain a microstructure mainly composed of bainite, which makes it difficult to achieve ductility. In the case of a galvanized steel sheet, the steel sheet needs to be reheated to a temperature higher than the temperature of a coating bath. JP 2826058 only describes the improvement in hydrogen embrittlement of a steel sheet, and there is little consideration for workability although bendability is considered to some extent.

In general, the ratio of a hard second phase to the entire microstructure needs to be increased to increase the strength of a steel sheet. However, when the ratio of a hard second phase is increased, the workability of a steel sheet is strongly affected by that of the hard second phase. The reason is as follows. When the ratio of the hard second phase is low, minimal workability is achieved by the deformation of ferrite itself that is a parent phase even if the workability of the hard second phase is insufficient. However, when the ratio of the hard second phase is high, the formability of a steel sheet is directly affected by the deformability of the hard second phase, not the deformation of ferrite. If the workability is insufficient, the formability is considerably degraded.

Therefore, in the case of a cold-rolled steel sheet, for example, martensite is formed through water quenching by adjusting the fraction of ferrite and a hard second phase using a continuous annealing furnace that can perform water quenching. Subsequently, the temperature is increased and held to temper martensite, whereby the workability of the hard second phase is improved.

However, in the case where equipment has no ability to temper the thus-formed martensite by increasing temperature and holding high temperature, the strength can be ensured, but it is difficult to ensure the workability of the hard second phase such as martensite.

To achieve stretch-flangeability using a hard phase other than martensite, the workability of a hard second phase is ensured by employing ferrite as a parent phase and bainite or pearlite containing carbides as a hard second phase. Unfortunately, in this case, sufficient ductility cannot be achieved.

When bainite is used, there is a problem in that the characteristics significantly vary due to the variation in a bainite-formation temperature range and the holding time. When martensite or retained austenite (including bainite containing retained austenite) is employed as a second phase, for example, a mixed microstructure of martensite and bainite is considered to be used as a second phase microstructure to ensure both ductility and stretch-flangeability.

However, to employ a mixed microstructure composed of various phases as a second phase and precisely control the fraction or the like, the heat treatment conditions need to be precisely controlled, which often poses a problem of manufacturing stability.

It would therefore be helpful to provide a high strength steel sheet having a tensile strength of 900 MPa or higher that can minimize the formation of bainite, which easily causes a variation in characteristics such as strength and formability, and can have both high strength and good formability and to provide an advantageous method for manufacturing the high strength steel sheet.

SUMMARY

The formability is evaluated using TS×T. El and a λ value that represents stretch-flangeability. TS×T. El≧14500 MPa·% and λ≧15% are target characteristics.

We studied the formation process of martensite, in particular, the effect of the cooling conditions of a steel sheet on martensite. We subsequently found that a high strength steel sheet having both good formability and high strength with a tensile strength of 900 MPa or higher that can be obtained by the following method. By suitably controlling the heat treatment conditions after cold-rolling, martensite transformation is caused while at the same time the transformed martensite is tempered. The ratio of the thus-formed autotempered martensite is controlled to a certain ratio and also the distribution state of iron-based carbide grains included in the autotempered martensite is suitably controlled, whereby such a high strength steel sheet can be obtained.

We thus provide:

    • 1. A high strength steel sheet having a tensile strength of 900 MPa or higher, includes a composition including, on a mass basis:
      • C: 0.1% or more and 0.3% or less;
      • Si: 2.0% or less;
      • Mn: 0.5% or more and 3.0% or less;
      • P: 0.1% or less;
      • S: 0.07% or less;
      • Al: 1.0% or less; and
      • N: 0.008% or less, with the balance Fe and incidental impurities, wherein a steel microstructure includes, on an area ratio basis, 5% or more and 80% or less of ferrite, 15% or more of autotempered martensite, 10% or less of bainite, 5% or less of retained austenite, and 40% or less of as-quenched martensite; a mean hardness of the autotempered martensite is HV≦700; and the mean number of precipitated iron-based carbide grains each having a size of 5 nm or more and 0.5 μm or less and included in the autotempered martensite is 5×104 or more per 1 mm2.
    • 2. The high strength steel sheet according to the above-described 1, further includes, on a mass basis, at least one element selected from:
      • Cr: 0.05% or more and 5.0% or less;
      • V: 0.005% or more and 1.0% or less; and
      • Mo: 0.005% or more and 0.5% or less.
    • 3. The high strength steel sheet according to the above-described 1 or 2, further includes, on a mass basis, at least one element selected from:
      • Ti: 0.01% or more and 0.1% or less;
      • Nb: 0.01% or more and 0.1% or less;
      • B: 0.0003% or more and 0.0050% or less;
      • Ni: 0.05% or more and 2.0% or less; and
      • Cu: 0.05% or more and 2.0% or less.
    • 4. The high strength steel sheet according to any one of the above-described 1 to 3, further includes, on a mass basis, at least one element selected from:
      • Ca: 0.001% or more and 0.005% or less; and
      • REM: 0.001% or more and 0.005% or less.
    • 5. The high strength steel sheet according to any one of the above-described 1 to 4, wherein the area ratio of autotempered martensite in which the number of precipitated iron-based carbide grains each having a size of 0.1 μm or more and 0.5 μm or less is 5×102 or less per 1 mm2 to the entire autotempered martensite is 3% or more.
    • 6. The high strength steel sheet according to any one of the above-described 1 to 5, wherein a galvanized layer is disposed on a surface of the steel sheet.
    • 7. The high strength steel sheet according to any one of the above-described 1 to 5, wherein a galvannealed layer is disposed on a surface of the steel sheet.
    • 8. A method for manufacturing a high strength steel sheet, includes the steps of hot-rolling and then cold-rolling a slab to be formed into a steel sheet having the composition according to any one of the above-described 1 to 4 to form a cold-rolled steel sheet; annealing the cold-rolled steel sheet in a first temperature range of 700° C. or higher and 950° C. or lower for 15 seconds or longer and 600 seconds or shorter; in a second temperature range, which is a temperature range from the first temperature range to 420° C., cooling the steel sheet from the first temperature range to 550° C. at an average cooling rate of 3° C./s or higher and cooling the steel sheet from 550° C. to 420° C. within 600 seconds; and cooling the steel sheet at a cooling rate of 50° C./s or lower in a third temperature range of 250° C. or higher and 420° C. or lower to perform, in the third temperature range, autotempering treatment in which martensite transformation is caused while at the same time the transformed martensite is tempered.
    • 9. The method for manufacturing a high strength steel sheet according to the above-described 8, wherein when the steel sheet is cooled at a cooling rate of 50° C./s or lower in the third temperature range of 250° C. or higher and 420° C. or lower, the steel sheet is cooled at a cooling rate of 1.0° C./s or higher and 50° C./s or lower in a temperature range of at least (Ms temperature−50)° C. or lower to perform, in the third temperature range, autotempering treatment in which martensite transformation is caused while at the same time the transformed martensite is tempered.
    • 10. The method for manufacturing a high strength steel sheet according to the above-described 8 or 9, wherein martensite start temperature Ms of the slab is approximated by M represented by Formula (1) below, and the M is 300° C. or higher:


M(° C.)=540−361×{[C %]/(1−[α%]/100)}−6×[Si %]−40×[Mn %]+30×[Al %]−20×[Cr %]−35×[V %]−10×[Mo %]−17×[Ni %]−10×[Cu %]  (1)

    • where [X %] is mass % of a constituent element X of the slab and [α%] is an area ratio (%) of polygonal ferrite.

A high strength steel sheet having a tensile strength of 900 MPa or higher that can achieve high strength, good workability, and good ductility can be obtained by forming an appropriate amount of autotempered martensite in a steel sheet and suitably controlling the distribution state of carbide grains included in the autotempered martensite. Therefore, our steel sheets significantly contribute to the weight reduction of automobile bodies.

In the method for manufacturing a high strength steel sheet, since reheating the steel sheet after quenching is not needed, special manufacturing equipment is not required and the method can be easily applied to a galvanizing or galvannealing process. Therefore, our methods contributes to decreases in the number of steps and in the cost.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a schematic view showing quenching and tempering steps performed to obtain typical tempered martensite.

FIG. 2 is a schematic view showing an autotempering treatment step performed to obtain autotempered martensite.

 DETAILED DESCRIPTION

The reason for the above-described limitation of the microstructure of a steel sheet according to the present invention will be described below.

Area Ratio of Ferrite: 5% or More and 80% or Less

To achieve both workability and a tensile strength of 900 MPa or higher, the ratio between ferrite and a hard phase described below is important and thus the area ratio of ferrite needs to be 5% or more and 80% or less. If the area ratio of ferrite is less than 5%, ductility is not ensured. If the area ratio of ferrite is more than 80%, the area ratio of the hard phase becomes insufficient and thus the strength becomes insufficient. The area ratio of ferrite is preferably set in the range of 10% or more and 65% or less.

Area Ratio of Autotempered Martensite: 15% or More

Autotempered martensite is a microstructure obtained by simultaneously causing martensite transformation and tempering of the martensite through autotempering treatment, and not so-called “tempered martensite” obtained through quenching and tempering treatments as in the related art. The microstructure is not a uniformly tempered microstructure formed by completing martensite transformation through quenching and then performing tempering through a temperature increase as in typical quenching and tempering treatments, but is a microstructure including martensites in different tempered states obtained by performing martensite transformation and tempering of the martensite in stages through the control of a cooling process in a temperature range of Ms temperature or lower.

This autotempered martensite is a hard phase for increasing strength. If the area ratio of autotempered martensite is less than 15%, sufficient strength cannot be achieved and work hardening of ferrite cannot be facilitated. Thus, the area ratio of autotempered martensite needs to be 15% or more and is preferably 30% or more.

The microstructure of a steel sheet is preferably composed of ferrite and autotempered martensite within the above-described range. When such phases are formed, other phases such as bainite, retained austenite, and as-quenched martensite are sometimes formed. These phases may be formed as long as some parameters are within the tolerable ranges described below. The tolerable ranges will now be described.

Area Ratio of Bainite: 10% or Less (Including 0%)

Bainite is a hard phase that contributes to an increase in strength, but the characteristics significantly vary in accordance with the formation temperature range and the variation in the quality of material is sometimes increased. Therefore, the area ratio of bainite in a steel microstructure is desirably as low as possible, but up to 10% of bainite is tolerable. The area ratio of bainite is preferably 5% or less.

Area Ratio of Retained Austenite: 5% or Less (Including 0%)

Retained austenite is transformed into hard martensite when processed, which decreases stretch-flangeability. Thus, the area ratio of retained austenite in a steel microstructure is desirably as low as possible, but up to 5% of retained austenite is tolerable. The area ratio of retained austenite is preferably 3% or less.

Area Ratio of as-Quenched Martensite: 40% or Less (Including 0%)

Since as-quenched martensite has considerably poor workability, the area ratio of as-quenched martensite in a steel microstructure is desirably as low as possible, but up to 40% of as-quenched martensite is tolerable. The area ratio of as-quenched martensite is preferably 30% or less. Herein, as-quenched martensite can be differentiated from autotempered martensite in that carbides of as-quenched martensite are not observed with a scanning electron microscope (SEM) or a transmission electron microscope (TEM).

Mean Hardness of Autotempered Martensite: HV≦700

If the mean hardness of autotempered martensite is 700<HV, stretch-flangeability is considerably degraded. Thus, HV≦700 needs to be satisfied and HV≦630 is preferably satisfied.

Iron-Based Carbide in Autotempered Martensite

Size: 5 nm or More and 0.5 μm or Less, Mean Number of Precipitated Carbide Grains: 5×104 or More per 1 mm2

Autotempered martensite is martensite subjected to the heat treatment (autotempering treatment) performed by the method. However, even if the mean hardness of autotempered martensite is HV≦700, the workability is decreased when the autotempering treatment is improperly performed. The degree of autotempering treatment can be confirmed through the formation state (distribution state) of iron-based carbide grains in autotempered martensite. When the mean number of precipitated iron-based carbide grains each having a size of 5 nm or more and 0.5 μm or less is 5×104 or more per 1 mm2, it can be judged that desired autotempering treatment has been performed. Iron-based carbide grains each having a size of less than 5 nm are removed from the target of judgment because such carbide grains do not affect the workability of autotempered martensite. On the other hand, iron-based carbide grains each having a size of more than 0.5 μm are also removed from the target of judgment because such carbide grains may decrease the strength of autotempered martensite but hardly affect the workability. If the number of iron-based carbide grains is less than 5×104 per 1 mm2, it is judged that the autotempering treatment has been improperly performed because workability, particularly stretch-flangeability, is not improved. The number of iron-based carbide grains is preferably 1×105 or more and 1×106 or less per 1 mm2, more preferably 4×105 or more and 1×106 or less per 1 mm2. Herein, an iron-based carbide is mainly Fe3C, and ε carbides and the like may be further contained.

To confirm the formation state of carbide grains, it is effective to observe a mirror-polished sample using a SEM (scanning electron microscope) or a TEM (transmission electron microscope). Carbide grains can be identified by, for example, performing SEM-EDS (energy dispersive X-ray spectrometry), EPMA (electron probe microanalyzer), or FE-AES (field emission-Auger electron spectrometry) on samples whose section is polished.

In the steel sheet, the amount of autotempered martensite narrowed down by further limiting the size and number of iron-based carbide grains precipitated in the above-described autotempered martensite can be suitably set as follows.

Autotempered Martensite in which the Number of Precipitated Iron-Based Carbide Grains Each Having a Size of 0.1 μm or More and 0.5 μm or Less is 5×102 or Less per 1 mm2: the Area Ratio of the Autotempered Martensite to the Entire Autotempered Martensite is 3% or More

By increasing the ratio of autotempered martensite in which the number of precipitated iron-based carbide grains each having a size of 0.1 μm or more and 0.5 μm or less is 5×102 or less per 1 mm2, ductility is further improved. To produce such an effect, the area ratio of autotempered martensite in which the number of precipitated iron-based carbide grains each having a size of 0.1 μm or more and 0.5 μm or less is 5×102 or less per 1 mm2 to the entire autotempered martensite is preferably 3% or more. If a large amount of autotempered martensite in which the number of precipitated iron-based carbide grains each having a size of 0.1 μm or more and 0.5 μm or less is 5×102 or less per 1 mm2 is contained in a steel sheet, workability is considerably degraded. Thus, the area ratio of such autotempered martensite to the entire autotempered martensite is preferably 40% or less, more preferably 30% or less.

When the area ratio of autotempered martensite in which the number of precipitated iron-based carbide grains each having a size of 0.1 μm or more and 0.5 μm or less is 5×102 or less per 1 mm2 to the entire autotempered martensite is 3% or more, the number of fine iron-based carbide grains is increased in autotempered martensite. Therefore, the mean number of precipitated iron-based carbide grains in the entire autotempered martensite is increased. Thus, the mean number of precipitated iron-based carbide grains each having a size of 5 nm or more and 0.5 μm or less in autotempered martensite is preferably 1×105 or more and 5×106 or less per 1 mm2, more preferably 4×105 or more and 5×106 or less per 1 mm2.

The specific reason why ductility is further improved as described above is not clear, but it is believed to be as follows. When the area ratio of autotempered martensite in which the number of precipitated iron-based carbide grains each having a relatively large size of 0.1 μm or more and 0.5 μm or less is 5×102 or less per 1 mm2 to the entire autotempered martensite is 3% or more, the autotempered martensite microstructure includes a portion that contains a large number of iron-based carbide grains having a relatively large size and a portion that contains a small number of iron-based carbide grains having a relatively large size in a mixed manner. The portion that contains a small number of iron-based carbide grains having a relatively large size is hard autotempered martensite because a large number of fine iron-based carbide grains are contained. On the other hand, the portion that contains a large number of iron-based carbide grains having a relatively large size is soft autotempered martensite. By providing the hard autotempered martensite such that the hard autotempered martensite is surrounded by the soft autotempered martensite, the degradation of stretch-flangeability caused by the hardness difference in autotempered martensite can be suppressed. Furthermore, by dispersing the hard martensite in the soft autotempered martensite, work hardenability is improved and thus ductility is improved.

The reason why the composition is set in the above-described range in the steel sheet will be described below. The symbol “%” below used for each component means “% by mass.”

C: 0.1% or More and 0.3% or Less

C is an essential element for increasing the strength of a steel sheet. A C content of less than 0.1% causes difficulty in achieving both strength and workability such as ductility or stretch-flangeability of the steel sheet. On the other hand, a C content of more than 0.3% causes a significant hardening of welds and heat-affected zones, thereby reducing weldability. Thus, the C content is set in the range of 0.1% or more and 0.3% or less, preferably 0.12% or more and 0.23% or less.

Si: 2.0% or Less

Si is a useful element for solution hardening of ferrite, and the Si content is preferably 0.1% or more to ensure the ductility and the hardness of ferrite. However, the excessive addition of Si causes the degradation of surface quality due to the occurrence of red scale and the like and the degradation of the adhesion of a coating. Thus, the Si content is set to 2.0% or less, preferably 1.6% or less.

Mn: 0.5% or More and 3.0% or Less

Mn is an element that is effective in strengthening steel, stabilizes austenite, and is necessary for ensuring the area ratio of a hard phase. To achieve this, a Mn content of 0.5% or more is required. On the other hand, an excessive Mn content of more than 3.0% causes the degradation of castability or the like. Thus, the Mn content is set in the range of 0.5% or more and 3.0% or less, preferably 1.5% or more and 2.5% or less.

P: 0.1% or Less

P causes embrittlement due to grain boundary segregation and degrades shock resistance, but a P content of up to 0.1% is tolerable. Furthermore, in the case where a steel sheet is galvannealed, a P content of more than 0.1% significantly reduces the rate of alloying. Thus, the P content is set to 0.1% or less, preferably 0.05% or less.

S: 0.07% or Less

S is formed into MnS as an inclusion that causes the degradation of shock resistance and causes cracks along a flow of a metal in a weld zone. Thus, the S content is preferably minimized. However, a S content of up to 0.07% is tolerable in terms of manufacturing costs. The S content is preferably 0.04% or less.

Al: 1.0% or Less

Al is an element that contributes to ferrite formation and a useful element for controlling the amount of the ferrite formation during manufacturing. However, an excessive Al content degrades the quality of a slab during steelmaking. Thus, the Al content is set to 1.0% or less, preferably 0.5% or less. Since an excessively low Al content sometimes makes it difficult to perform deoxidization, the Al content is preferably 0.01% or more.

N: 0.008% or Less

N is an element that most degrades the anti-aging property of steel. Therefore, the N content is preferably minimized. A N content of more than 0.008% causes significant degradation of an anti-aging property. Thus, the N content is set to 0.008% or less, preferably 0.006% or less.

If necessary, the steel sheet can suitably contain the components described below in addition to the basic components described above.

At Least One Element Selected from Cr: 0.05% or More and 5.0% or Less, V: 0.005% or More and 1.0% or Less, and Mo: 0.005% or More and 0.5% or Less

Cr, V, and Mo have an effect of suppressing the formation of pearlite when a steel sheet is cooled from the annealing temperature and thus can be optionally added. The effect is produced at a Cr content of 0.05% or more, a V content of 0.005% or more, or a Mo content of 0.005% or more. On the other hand, an excessive Cr content of more than 5.0%, an excessive V content of more than 1.0%, or an excessive Mo content of more than 0.5% excessively increases the area ratio of a hard phase, thereby unnecessarily increasing the strength. Thus, when these elements are incorporated, the Cr content is preferably set in the range of 0.05% or more and 5.0% or less, the V content is preferably set in the range of 0.005% or more and 1.0% or less, and the Mo content is preferably set in the range of 0.005% or more and 0.5% or less.

Furthermore, at least one element selected from Ti, Nb, B, Ni, and Cu can be incorporated. The reason for the limitation of the content ranges is as follows.

Ti: 0.01% or More and 0.1% or Less and Nb: 0.01% or More and 0.1% or Less

Ti and Nb are useful for precipitation strengthening of steel and the effect is produced at a Ti content of 0.01% or more or a Nb content of 0.01% or more. On the other hand, a Ti content of more than 0.1% or a Nb content of more than 0.1% degrades the workability and shape flexibility. Thus, the Ti content and the Nb content are each preferably set in the range of 0.01% or more and 0.1% or less.

B: 0.0003% or More and 0.0050% or Less

B has an effect of suppressing the formation and growth of ferrite from austenite grain boundaries and thus can be optionally added. The effect is produced at a B content of 0.0003% or more. On the other hand, a B content of more than 0.0050% decreases workability. Thus, when B is incorporated, the B content is preferably set in the range of 0.0003% or more and 0.0050% or less. Herein, when B is incorporated, the formation of BN is preferably suppressed to produce the above-described effect. Thus, B is preferably added together with Ti.

Ni: 0.05% or More and 2.0% or Less and Cu: 0.05% or More and 2.0% or Less

In the case where a steel sheet is galvanized, Ni and Cu promote internal oxidation, thereby improving the adhesion of a coating. The effect is produced at a Ni content of 0.05% or more or a Cu content of 0.05% or more. On the other hand, a Ni content of more than 2.0% or a Cu content of more than 2.0% degrades the workability of a steel sheet. Ni and Cu are useful elements for strengthening steel. Thus, the Ni content and the Cu content are each preferably set in the range of 0.05% or more and 2.0% or less.

At Least One Element Selected from Ca: 0.001% or More and 0.005% or Less and REM: 0.001% or More and 0.005% or Less

Ca and REM are useful elements for spheroidizing the shape of a sulfide and improving an adverse effect of the sulfide on stretch-flangeability. The effect is produced at a Ca content of 0.001% or more or an REM content of 0.001% or more. On the other hand, a Ca content of more than 0.005% or an REM content of more than 0.005% increases the number of inclusions or the like and causes, for example, surface defects and internal defects. Thus, when Ca and REM are incorporated, the Ca content and the REM content are each preferably set in the range of 0.001% or more and 0.005% or less.

Components other than the components described above are Fe and incidental impurities. However, a component other than the components described above may be contained to the extent that the advantages are not impaired.

As described below, the composition of the steel sheet according to the present invention preferably satisfies M≧300° C. that represents a relation between the composition and the area ratio of polygonal ferrite to perform stable production, that is, to suppress the variation in characteristics due to the variation in manufacturing conditions.

A galvanized layer or a galvannealed layer may be disposed on a surface of a steel sheet.

A preferred method for manufacturing a steel sheet and the reason for the limitation of the conditions will now be described.

A slab prepared to have the above-described preferred composition is produced, hot-rolled, and then cold-rolled to obtain a cold-rolled steel sheet. These processes are not particularly limited, and can be performed by typical methods.

The preferred manufacturing conditions will now be described below. A slab is heated to 1100° C. or higher and 1300° C. or lower and subjected to finish hot-rolling at a temperature of 870° C. or higher and 950° C. or lower, which means that the hot-rolling end temperature is set to 870° C. or higher and 950° C. or lower. The thus-obtained hot-rolled steel sheet is wound at a temperature of 350° C. or higher and 720° C. or lower. Subsequently, the hot-rolled steel sheet is pickled and cold-rolled at a reduction ratio of 40% or higher and 90% or lower to obtain a cold-rolled steel sheet.

It is assumed that the hot-rolled steel sheet is produced through the typical steps of steel making, casting, and hot-rolling, but the hot-rolled steel sheet may be produced by thin slab casting without performing part or all of the hot-rolling steps.

The resultant cold-rolled steel sheet is annealed for 15 seconds or longer and 600 seconds or shorter in a first temperature range of 700° C. or higher and 950° C. or lower, specifically, in an austenite single-phase region or a dual-phase region of an austenite phase and a ferrite phase. If the annealing temperature is lower than 700° C. or the annealing time is shorter than 15 seconds, a carbide in the steel sheet is sometimes not sufficiently dissolved, or the recrystallization of ferrite is not completed and thus desired ductility and stretch-flangeability are sometimes not achieved. On the other hand, if the annealing temperature exceeds 950° C., austenite grains are significantly grown and the constituent phases produced by cooling performed later are coarsened, which may degrade ductility and stretch-flangeability. If the annealing time exceeds 600 seconds, a vast amount of energy is consumed and thus the cost is increased. Therefore, the annealing temperature is set in the range of 700° C. or higher and 950° C. or lower, preferably 760° C. or higher and 920° C. or lower. The annealing time is set in the range of 15 seconds or longer and 600 seconds or shorter, preferably 30 seconds or longer and 400 seconds or shorter.

In a second temperature range, which is a temperature range from the first temperature range to 420° C., the annealed cold-rolled steel sheet is cooled to 550° C. from the first temperature range at a cooling rate of 3° C./s or higher, and is then cooled from 550 to 420° C. within 600 seconds. Subsequently, the steel sheet is cooled at a cooling rate of 50° C./s or lower in a third temperature range of 250° C. or higher and 420° C. or lower.

The cooling conditions in a second temperature range from the first temperature range to 420° C. are essential to suppress the precipitation of phases other than intended ferrite and autotempered martensite phases. In the temperature range from the first temperature range to 550° C., pearlite transformation easily occurs. If the average cooling rate is lower than 3° C./s in the range from 700° C., which is the lower limit temperature of the first temperature range, to 550° C., pearlite or the like is precipitated and a desired microstructure is sometimes not obtained. Therefore, the cooling rate needs to be 3° C./s or higher, and is preferably 5° C./s or higher. The upper limit of the cooling rate is not particularly specified, but special cooling equipment is required to achieve a cooling rate of 200° C./s or higher. Thus, the cooling rate is preferably 200° C./s or lower.

When the steel sheet is held for a long time in a temperature range of 550° C. to 420° C., bainite transformation is caused. If the time required for cooling from 550° C. to 420° C. exceeds 600 seconds, bainite transformation is caused and thus a desired microstructure is sometimes not obtained. Therefore, the time required for cooling from 550° C. to 420° C. is 600 seconds or shorter, preferably 400 seconds or shorter.

After the process in the second temperature range, the steel sheet is processed in the third temperature range. The most important feature is that, in the third temperature range, autotempering treatment in which martensite transformation is caused while at the same time the transformed martensite is tempered is performed to obtain autotempered martensite in which the precipitation state of carbide grains is suitably controlled.

Typical martensite is obtained by performing annealing and then performing quenching with water cooling or the like. The martensite is a hard phase, and contributes to an increase in the strength of a steel sheet but degrades workability. To change the martensite into tempered martensite having satisfactory workability, a quenched steel sheet is normally heated again to perform tempering. FIG. 1 schematically shows the steps described above. In such normal quenching and tempering treatments, after martensite transformation is completed by quenching, the temperature is increased to perform tempering. Consequently, a uniformly tempered microstructure is obtained.

In contrast, autotempering treatment is a treatment in which a steel sheet is cooled in a certain cooling-rate range in the third temperature range as shown in FIG. 2. In the autotempering treatment, quenching and tempering through reheating are not performed, which is a method with high productivity. The steel sheet including autotempered martensite obtained through this autotempering treatment has strength and workability equal to or higher than those of the steel sheet obtained by performing quenching and tempering through reheating shown in FIG. 1. In the autotempering treatment, martensite transformation and the tempering can be made to occur continuously or stepwise by performing continuous cooling (including stepwise cooling and holding) in the third temperature range. Consequently, a microstructure including martensites in different tempered states can be obtained. Although the martensites in different tempered states have different characteristics in terms of strength and workability, desired characteristics as the entire steel sheet can be achieved by suitably controlling the amounts of martensites in different tempered states through autotempering treatment. Furthermore, since the autotempering treatment is performed without rapidly cooling a steel sheet to a low temperature range in which the martensite transformation is fully completed, the residual stress in the steel sheet is low and a steel sheet having a good plate shape is obtained, which is advantageous.

The third temperature range is 250° C. or higher and 420° C. or lower. If the temperature exceeds 420° C., bainite transformation is easily caused as described above. If the temperature is lower than 250° C., autotempering treatment requires a long time and thus proceeds insufficiently in a continuous annealing line or a continuous galvanizing and galvannealing line. In the third temperature range, the cooling rate of a steel sheet needs to be 50° C./s or lower to cause martensite transformation while at the same time tempering the transformed martensite and thus to obtain autotempered martensite. If the cooling rate exceeds 50° C./s, the autotempering treatment insufficiently proceeds and the workability of martensite is sometimes not ensured. If the cooling rate is less than 0.1° C./s, bainite transformation occurs or autotempering treatment excessively proceeds, whereby strength sometimes cannot be ensured. Thus, the cooling rate is preferably 0.1° C./s or higher.

In the method for manufacturing a steel sheet, the following configuration can be suitably added if necessary.

When a steel sheet is cooled at a cooling rate of 50° C./s or lower in a third temperature range of 250° C. or higher and 420° C. or lower, the steel sheet is preferably cooled at a cooling rate of 1.0° C./s or higher and 50° C./s or lower in a temperature range of at least (Ms temperature−50)° C. or lower. This is because, by further appropriately controlling the precipitation state of carbide grains included in autotempered martensite, the area ratio of autotempered martensite in which the number of precipitated iron-based carbide grains each having a size of 0.1 μm or more and 0.5 μm or less is 5×102 or less per 1 mm2 to the entire autotempered martensite can be set to 3% or more. If the cooling rate exceeds 50° C./s, autotempering treatment insufficiently proceeds and desired autotempered martensite is not obtained. Consequently, the workability of martensite is sometimes not ensured. If the cooling rate is less than 1.0° C./s, 3% or more of the area ratio of autotempered martensite in which the number of precipitated iron-based carbide grains each having a size of 0.1 μm or more and 0.5 μm or less is 5×102 or less per 1 mm2 to the entire autotempered martensite cannot be achieved, and desired ductility and strength are not ensured. Thus, the cooling rate is set to 1.0° C./s or higher. Herein, Ms temperature can be obtained in a typical manner through the measurement of thermal expansion or electrical resistance during cooling. Alternatively, M obtained from an approximate expression (1) of Ms temperature described below may be used.

In the method for manufacturing a steel sheet, autotempering treatment can be stably performed when M represented by the approximate expression (1) below is 300° C. or higher:


M(° C.)=540−361×{[C %]/(1−[α%]/100)}−6×[Si %]−40×[Mn %]+30×[Al %]−20×[Cr %]−35×[V %]−10×[Mo %]−17×[Ni %]−10×[Cu %]  (1)

where [X %] is mass % of an alloy element X and [α%] is the area ratio (%) of polygonal ferrite.

M represented by the above-described expression (1) is an empirical approximate expression of Ms temperature from which martensite transformation starts. It is believed that M is highly related to the precipitation behavior of iron-based carbide grains from martensite. Thus, M can be used as an indicator that indicates whether autotempered martensite in which the number of iron-based carbide grains each having a size of 5 nm or more and 0.5 μm or less is 5×104 or more per 1 mm2 can be stably obtained. Even if M is less than 300° C., autotempered martensite is obtained. However, since the temperature is low, martensite transformation and autotempering treatment tend to slowly proceed. Compared with the case of M≧300° C., a steel sheet needs to be cooled slowly or held at a low temperature for a long time to obtain desired autotempered martensite, which may considerably lower manufacturing efficiency. Thus, M is preferably 300° C. or higher.

The area ratio of polygonal ferrite is measured, for example, through the image processing and analysis of a SEM micrograph taken at 1000 to 3000 power. Polygonal ferrite is observed in the steel sheet that has been annealed and cooled under the above-described conditions. To ensure that M is 300° C. or higher, after a cold-rolled steel sheet having a desired composition is produced, the area ratio of polygonal ferrite is measured and thus M is obtained from the expression (1) using the contents of alloy elements that can be calculated from the composition of the steel sheet. In the case where M is less than 300° C., the heat treatment conditions are suitably adjusted such that the area ratio of polygonal ferrite becomes lower, to obtain desired M. For example, the annealing temperature in the first temperature range is further increased and the average cooling rate from the first temperature range to 550° C. is further increased. Alternatively, the contents of the components in the expression (1) may be adjusted.

The steel sheet can be galvanized and galvannealed. The galvanizing and galvannealing treatments are preferably performed in a continuous galvanizing and galvannealing line while the above-described annealing and cooling conditions are satisfied. The galvanizing and galvannealing treatments are preferably performed in a temperature range of 420° C. or higher and 550° C. or lower. In this case, the time required for cooling a steel sheet from 550° C. to 420° C., that is, the holding time in the temperature range of 420° C. or higher and 550° C. or lower needs to be 600 seconds or shorter, the time including galvanizing treatment time and/or galvannealing treatment time.

A method of galvanizing and galvannealing treatments is as follows. First, a steel sheet is immersed in a coating bath and the coating weight is adjusted using gas wiping or the like. In the case where the steel sheet is galvanized, the amount of dissolved Al in the coating bath is in the range of 0.12% or more and 0.22% or less. In the case where the steel sheet is galvannealed, the amount of dissolved Al is in the range of 0.08% or more and 0.18% or less.

In the case where the steel sheet is galvanized, the temperature of the coating bath is desirably 450° C. or higher and 500° C. or lower. In the case where the steel sheet is galvannealed by further performing alloying treatment, the temperature during alloying is preferably 450° C. or higher and 550° C. or lower. If the alloying temperature exceeds 550° C., an excessive amount of carbide grains are precipitated from untransformed austenite or the transformation into pearlite is caused, whereby desired strength and ductility are sometimes not achieved. Powdering is also degraded. If the alloying temperature is less than 450° C., the alloying does not proceed.

The coating weight is preferably in the range of 20 to 150 g/m2 per surface. If the coating weight is less than 20 g/m2, corrosion resistance is degraded. Meanwhile, even if the coating weight exceeds 150 g/m2, the corrosion resistance is saturated, which merely increases the cost. The degree of alloying is preferably in the range of 7 to 15% by mass on a Fe content basis in the coating layer. If the degree of alloying is less than 7% by mass, uneven alloying is caused and the surface appearance quality is degraded. Furthermore, a so-called “ζ phase” is formed in the coating layer and thus the slidability is degraded. If the degree of alloying exceeds 15% by mass, a large amount of hard brittle F phase is formed and the adhesion of the coating is degraded.

The holding temperature in the first temperature range, in the second temperature range, or the like is not necessarily constant. Even if the holding temperature is varied, the purpose of this step is not impaired as long as the holding temperature is within a predetermined temperature range. The same is true for the cooling rate. Furthermore, a steel sheet may be subjected to annealing and autotempering treatments with any equipment as long as heat history is just satisfied. Moreover, it is also included in the scope of this disclosure that, after autotempering treatment, temper rolling is performed on the steel sheet for shape correction.

EXAMPLES Example 1

Our steel sheets and methods will now be further described with respect to selected Examples. The disclosure is thus not limited to the Examples. It will be understood that modifications may be made without departing from the scope of this disclosure.

A slab to be formed into a steel sheet having the composition shown in Table 1 was heated to 1250° C. and subjected to finish hot-rolling at 880° C. The hot-rolled steel sheet was wound at 600° C., pickled, and cold-rolled at a reduction ratio of 65% to obtain a cold-rolled steel sheet having a thickness of 1.2 mm. The resultant cold-rolled steel sheet was subjected to heat treatment under the conditions shown in Table 2. Quenching was not performed on any sample shown in Table 2. Herein, the holding time in Table 2 was a time held at the holding temperature shown in Table 2. The annealing time in a first temperature range of 700° C. or higher and 950° C. or lower was 600 seconds or shorter under any of the conditions shown in Table 2.

In the galvanizing treatment, both surfaces were subjected to plating in a coating bath having a temperature of 463° C. at a coating weight of 50 g/m2 per surface. In the galvannealing treatment, the alloying treatment was performed such that Fe % (iron content) in the coating layer was adjusted to 9% by mass. The resultant steel sheet was subjected to temper rolling at a reduction ratio (elongation ratio) of 0.3% regardless of the presence or absence of a coating.

TABLE 1 Steel (mass %) type C Si Mn Al P S N Cr V Mo Ti Nb B Ni Cu Ca REM Remarks A 0.16 1.59 2.2 0.040 0.011 0.005 0.0039 0.5 — — — — — — — — — Suitable steel B 0.15 1.51 2.3 0.036 0.012 0.004 0.0023 0.9 — — — — — — — — — Suitable steel C 0.15 1.40 2.3 0.041 0.012 0.004 0.0029 — — — — 0.04 — — — — — Suitable steel D 0.15 1.00 2.2 0.039 0.009 0.004 0.0037 1.0 — — 0.021 — 0.0010 — — — — Suitable steel E 0.14 1.48 2.2 0.040 0.025 0.002 0.0038 — — — — — — — — — — Suitable steel F 0.21 1.42 2.3 0.041 0.010 0.004 0.0037 — — — — — — — — — — Suitable steel G 0.29 1.50 2.1 0.040 0.010 0.003 0.0041 — — — — — — — — — — Suitable steel H 0.16 0.51 2.2 0.039 0.013 0.004 0.0032 1.5 — — 0.020 — 0.0008 — — — — Suitable steel I 0.15 1.49 2.8 0.037 0.012 0.003 0.0033 — — — 0.019 — 0.0005 — — — — Suitable steel J 0.12 1.52 2.3 0.037 0.029 0.003 0.0041 1.0 — — 0.020 — 0.0009 — — — — Suitable steel K 0.21 0.49 1.6 0.037 0.029 0.003 0.0041 — — — 0.022 — 0.0012 — — — — Suitable steel L 0.15 1.50 2.3 0.043 0.013 0.002 0.0043 1.0 — — 0.050 — 0.0010 — — — — Suitable steel M 0.11 1.48 2.0 0.039 0.013 0.003 0.0037 0.9 — 0.03 0.021 — 0.0008 — — — — Suitable steel N 0.16 1.50 2.3 0.038 0.012 0.003 0.0041 0.8 0.10 — — — — — — — — Suitable steel O 0.12 0.99 1.2 0.040 0.013 0.003 0.0041 1.0 — — — — — 1.00 — — — Suitable steel P 0.15 1.53 2.1 0.041 0.011 0.004 0.0029 0.5 — — — — — — 0.3 — — Suitable steel Q 0.15 1.48 2.3 0.044 0.009 0.004 0.0031 1.0 — — 0.019 — 0.0008 — — — 0.002 Suitable steel R 0.05 1.05 2.1 0.037 0.008 0.004 0.0030 — — — — — — — — — — Comparative steel S 0.33 1.25 2.7 0.035 0.010 0.004 0.0042 — — — — — — — — — — Comparative steel T 0.23 1.51 3.5 0.040 0.008 0.004 0.0039 — — — — — — — — — — Comparative steel Note) Underline means the value is outside the suitable range.

TABLE 2 Second temperature Third range temperature Average range cooling Time Average rate required cooling First from for rate temperature first cooling from range temperature from 420° C. Holding Holding range 550° C. to Sample Steel Temperature time to 550° C. to 420° C. 250° C. No. type (° C.) (second) (° C./s) (second) (° C./s) Plating*2 Remarks 1 A 820 180 10 90 15 CR Invention Example 2 B 830 100 10 60 10 GI Invention Example 3 C 820 180 10 80 55 CR Comparative Example 4 C 850 180 45 60 10 CR Invention Example 5 D 830 250 40 60 10 GI Invention Example 6 E 820 180 10 60 100  CR Comparative Example 7 F 810 180 8 70 60 CR Comparative Example 8 G 820 180 5 60 55 GA Comparative Example 9 H 820 180 10 120  15 GA Invention Example 10 I 870 180 15 60 10 CR Invention Example 11 J 830 200 30 60 10 CR Invention Example 12 J 830 300 7 60  5 CR Invention Example 13 K 860 40 10 45 10 GI Invention Example 14 L 860 90 10 60 10 CR Invention Example 15 M 850 180 10 60  9 CR Invention Example 16 N 800 450 10 80 10 CR Invention Example 17 O 820 180 10 60  8 GI Invention Example 18 P 860 400 10 75  9 GI Invention Example 19 Q 800 180 10 60 10 CR Invention Example 20 R 800 180 10 80 10 CR Comparative Example 21 S 800 180 10 80 10 CR Comparative Example 22 T 800 180 10 80 10 CR Comparative Example 23 A 880 200 50 20 70 CR Comparative Example 24 E 810 200 10 90 10 CR Invention Example 25 G 850 350 5 650   5 CR Comparative Example 26 G 870 150 15 120   3 CR Invention Example *1Underline means the value is outside the suitable range. *2CR: no plating (cold-rolled steel sheet), GI: galvanizing, and GA: galvannealing

The characteristics of the resultant steel sheets were evaluated by the following methods.

To examine the microstructure of the steel sheets, two test pieces were cut from each of the steel sheets. One of the test pieces was polished without performing any treatment. The other of the test pieces was polished after heat treatment was performed at 200° C. for 2 hours. The polished surface was a section in the sheet thickness direction, the section being parallel to the rolling direction. By observing a steel microstructure of the polished surface with a scanning electron microscope (SEM) at a magnification of 3000×, the area ratio of each phase was measured to identify the phase structure of each crystal grain. The observation was performed for 10 fields and the area ratio was an average value of the 10 fields. The area ratios of autotempered martensite, polygonal ferrite, and bainite were obtained using the test pieces polished without performing any treatment. The area ratios of as-quenched martensite (untempered martensite) and retained austenite were obtained using the test pieces polished after heat treatment was performed at 200° C. for 2 hours. The test pieces polished after heat treatment was performed at 200° C. for 2 hours were prepared to differentiate untempered martensite from retained austenite in the SEM observation. In the SEM observation, it is difficult to differentiate untempered martensite from retained austenite. When martensite is tempered, an iron-based carbide is formed in the martensite. The iron-based carbide makes it possible to differentiate martensite from retained austenite. The heat treatment at 200° C. for 2 hours does not affect the phases other than martensite, that is, martensite can be tempered without changing the area ratio of each phase. As a result, martensite can be differentiated from retained austenite due to the formed iron-based carbide. By comparing the test pieces polished without performing any treatment to the test pieces polished after heat treatment was performed at 200° C. for 2 hours through SEM observation, it was confirmed that phases other than martensite were not changed.

The size and number of iron-based carbide grains included in autotempered martensite were measured through SEM observation. The test pieces were the same as those used in the microstructure observation. Obviously, the test pieces polished without performing any treatment were observed. The test pieces were observed at a magnification of 10000× to 30000× in accordance with the precipitation state and size of the iron-based carbide grains. The size of the iron-based carbide grains was evaluated using an average value of the major axis and minor axis of individual precipitates. The number of iron-based carbide grains each having a size of 5 nm or more and 0.5 μm or less was counted and thus the number of iron-based carbide grains per 1 mm2 of autotempered martensite was calculated. The observation was performed for 5 to 20 fields. The mean number was calculated from the total number of all the fields of each sample, and the mean number was employed as the number (per 1 mm2 of autotempered martensite) of iron-based carbide grains of each sample.

The hardness HV of autotempered martensite was measured using an ultramicro-Vickers hardness meter at a load of 0.02 N. After the microstructure of autotempered martensite in which iron-based carbide grains were precipitated was confirmed by observing an indentation with a SEM, the average value of ten or more measurement values was employed as the hardness HV.

A tensile test was performed in accordance with JIS Z2241 using a JIS No. 5 test piece taken from the steel sheet in the rolling direction of the steel sheet. Tensile strength (TS), yield strength (YS), and total elongation (T. El) were measured. The product of the tensile strength and the total elongation (TS×T. El) was calculated to evaluate the balance between the strength and the elongation. When TS×T. El≧14500 (MPa·%), the balance was determined to be satisfactory.

Stretch-flangeability was evaluated in compliance with The Japan Iron and Steel Federation Standard JFST 1001. The resulting steel sheet was cut into pieces each having a size of 100 mm×100 mm. A hole having a diameter of 10 mm was made in the piece by punching at a clearance of 12% of the thickness. A cone punch with a 60° apex was forced into the hole while the piece was fixed with a die having an inner diameter of 75 mm at a blank-holding pressure of 88.2 kN. The diameter of the hole was measured when a crack was initiated. The maximum hole-expanding ratio (%) was determined with Formula (2) to evaluate stretch-flangeability using the maximum hole-expanding ratio:


Maximum hole-expanding ratio λ(%)={(Df−D0)/D0}×100  (2)

where Df represents the hole diameter (mm) when a crack was initiated, and D0 represents an initial hole diameter (mm). λ≧15% was determined to be satisfactory.

Table 3 shows the evaluation results.

TABLE 3 Mean Number of hardness of iron-based Area ratio (%) auto- carbide Auto- As- tempered grains Sample Steel tempered Retained quenched martensite per No. type martensite Ferrite austenite Bainite martensite (HV) 1 mm2 *1  1 A 57 43 0 0 0 602 1 × 105  2 B 72 28 0 0 0 550 1 × 105  3 C 35 63 0 0 2 661 1 × 104  4 C 37 52 4 7 0 601 1 × 105  5 D 83 17 0 0 0 526 5 × 105  6 E  0 72 0 0 28 857 None  7 F 22 60 1 2 15  771 1 × 103  8 G 58 37 0 0 5 691 5 × 103  9 H 91  9 0 0 0 492 1 × 106 10 I 84 12 1 3 0 503 1 × 106 11 J 84 16 0 0 0 470 3 × 106 12 J 30 67 0 0 3 667 7 × 104 13 K 90 10 0 0 0 523 5 × 105 14 L 90 10 0 0 0 505 5 × 105 15 M 84 15 1 0 0 480 1 × 106 16 N 93  7 0 0 0 495 1 × 106 17 O 59 39 2 0 0 513 8 × 105 18 P 88 12 0 0 0 503 1 × 106 19 Q 86 14 0 0 0 502 1 × 106 20 R 18 82 0 0 0 470 4 × 106 21 S 70 20 0 0 10  802 1 × 103 22 T 82 12 0 0 6 790 1 × 103 23 A 49  8 1 0 42  563 5 × 105 24 E 52 48 0 0 0 589 1 × 105 25 G 10 27 14  46  0 603 1 × 106 26 G 93  7 0 0 0 592 1 × 106 Sample M YS TS T · El TS × T · El λ No. (° C.) (MPa) (Mpa) (%) (MPa · %) (%) Remarks  1 332 771 1255 14.8 18574 16 Invention Example  2 346 924 1341 12.0 16092 22 Invention Example  3 293 687 1238 13.4 16589 5 Comparative Example  4 330 660 1220 14.0 17080 21 Invention Example  5 361 849 1393 11.1 15462 45 Invention Example  6 261 576 1066 18.8 20041 13 Comparative Example  7 250 667 1226 14.2 17409 5 Comparative Example  8 281 817 1521 7.5 11408 1 Comparative Example  9 355 946 1385 10.9 15097 36 Invention Example 10 358 908 1392 11.0 15239 42 Invention Example 11 367 772 1270 13.9 17653 35 Invention Example 12 288 601 1021 17.5 17868 22 Invention Example 13 389 903 1449 10.9 15794 32 Invention Example 14 359 916 1418 11.8 16732 34 Invention Example 15 386 883 1305 12.5 16313 49 Invention Example 16 357 838 1420 12.4 17608 20 Invention Example 17 378 617 1125 15.2 17100 25 Invention Example 18 372 900 1389 10.5 14585 36 Invention Example 19 356 837 1371 12.2 16726 24 Invention Example 20 420 593  781 20.9 16323 29 Comparative Example 21 276 1081 1520 9.2 13984 1 Comparative Example 22 297 931 1481 9.6 14218 2 Comparative Example 23 370 1123 1481 9.7 14365 10 Comparative Example 24 346 763 1197 16.1 19272 18 Invention Example 25 304 1008 1423 14.1 20064 4 Comparative Example 26 334 1118 1635 11.2 18312 19 Invention Example *1 The size of iron-based carbide grains is 5 nm or more and 0.5 μm or less. *2) Underline means the value is outside the suitable range.

As is clear from Table 3, our steel sheets have a tensile strength of 900 MPa or higher, a value of TS×T. El≧14500 (MPa·%), and a value of λ≧15% that represents stretch-flangeability and thus has both high strength and good workability. In Invention Examples, the steel sheets having an M of 300° C. or higher are excellent in stretch-flangeability, particularly stretch-flangeability that is not degraded even if strength is increased.

In contrast, in sample Nos. 6 and 7, the hardness of martensite is 700<HV and the number of iron-based carbide grains included in martensite is less than 5×104 per 1 mm2 or martensite does not include iron-based carbide grains. Therefore, a tensile strength of 900 MPa is satisfied, but a value of λ, is less than 15%, which provides poor workability. This is because, in sample Nos. 6 and 7, the cooling rate in the third temperature range is high, which does not satisfy 50° C./s. In sample Nos. 3 and 8, the hardness of martensite is satisfactorily HV≦700, but the number of iron-based carbide grains included in martensite is less than 5×104 per 1 mm2. Therefore, a tensile strength of 900 MPa or higher is satisfied, but a value of λ, is less than 15%, which provides poor workability. This is because, in sample Nos. 3 and 8, the cooling rate in the third temperature range is 55° C./s, which does not satisfy 50° C./s or lower. In particular, since sample No. 8 has a relatively high C content, TS×. El is 14500 MPa·% or less.

It can be confirmed from the above description that steel sheets that include autotempered martensite sufficiently subjected to autotempering treatment such that the hardness of martensite is HV≦700 and the number of iron-based carbide grains in martensite is 5×104 or more per 1 mm2 have both high strength and good workability.

Example 2

To confirm the effect of further improvement in ductility achieved by suitably controlling the distribution state of iron-based carbide grains included in autotempered martensite, samples were manufactured in the same manner as the samples shown in Table 2, except that the cooling rate in a temperature range of 250° C. or higher and (Ms temperature−50)° C. or lower of the third temperature range was changed as shown in Table. 4. In Table 4, sample Nos. 9, 11, 13, 14, and 26 are the same as those shown in Table 2 and listed in Table 4 to clarify the temperature range of 250° C. or higher and (Ms temperature−50)° C. or lower. Note that M (° C.) was used as the Ms temperature.

TABLE 4 Second Third temperature temperature range range First Average Time Average Average cooling temperature cooling required cooling rate from range rate from first for cooling rate from (Ms temperature Holding Holding temperature from 550° C. 420° C. −50) Steel temperature time range to to 420° C. to 250° C. ° C. to 250° C. Sample No. type (° C.) (second) 550° C. (° C./s) (second) (° C./s) (° C./s) Plating *1 Remarks 9 H 820 180 10 120 15 0.8 GA Invention Example 11 J 830 200 30 60 10 20 CR Invention Example 13 K 860 40 10 45 10 0.5 GI Invention Example 14 L 860 90 10 60 10 0.8 CR Invention Example 26 G 870 150 15 120 3 10 CR Invention Example 27 H 820 180 10 120 15 30 GA Invention Example 28 J 830 200 30 60 10 0.5 CR Invention Example 29 K 860 40 10 45 10 25 GI Invention Example 30 L 860 90 10 60 10 20 CR Invention Example 31 G 870 150 15 120 3 0.4 CR Invention Example *1CR: no plating (cold-rolled steel sheet), GI: galvanizing, and GA: galvannealing

The characteristics of the thus-obtained steel sheets were evaluated in the same manner as in Example 1. Herein, the amount of autotempered martensite in which the number of precipitated iron-based carbide grains each having a size of 0.1 μm or more and 0.5 μm or less is 5×102 or less per 1 mm2 in the entire autotempered martensite was obtained as follows.

As described above, the test pieces polished without performing any treatment were observed at a magnification of 10000× to 30000× using a SEM. The size of the iron-based carbide grains was evaluated using an average value of the major axis and minor axis of individual precipitates. The area ratio of autotempered martensite in which the iron-based carbide grains have a size of 0.1 μm or more and 0.5 μm or less was measured. The observation was performed for 5 to 20 fields.

Table 5 shows the results.

As is apparent from Table 5, in sample Nos. 11, 26, 27, 29, and 30 with a cooling rate of 1.0° C./s or higher and 50° C./s or lower in the temperature range of 250° C. or higher and (Ms temperature−50)° C. or lower, the distribution state of iron-based carbide grains included in autotempered martensite is suitably controlled and thus TS×T. El≧17000 MPa·% is exhibited, that is, ductility is improved.

TABLE 5 Number of Mean iron-based hardness carbide Area ratio (%) of auto- grains Auto- As- tempered (5 nm to Sample Steel tempered Retained quenched martensite 0.5 μm) per No. type martensite Ferrite austenite Bainite martensite (HV) 1 mm2  9 H 91 9 0 0 0 492 1 × 106 11 J 84 16 0 0 0 470 3 × 106 13 K 90 10 0 0 0 523 5 × 105 14 L 90 10 0 0 0 505 5 × 105 26 G 93 7 0 0 0 592 1 × 106 27 H 91 9 0 0 0 564 1 × 106 28 J 84 16 0 0 0 460 3 × 106 29 K 90 10 0 0 0 553 5 × 105 30 L 90 10 0 0 0 526 5 × 105 31 G 93 7 0 0 0 541 1 × 106 Area ratio of auto- tempered martensite in which the number of precipitated iron-based carbide grains (5 nm to 0.5 μm) is 5 × 102 or less per 1 mm2 to the entire Sample autotempered M YS TS T · El TS × T · El λ No. martensite (%) (° C.) (MPa) (MPa) (%) (MPa · %) (%) Remarks  9 2 355 946 1385 10.9 15097 36 Invention Example 11 14 367 772 1270 13.9 17653 35 Invention Example 13 1 389 903 1449 10.9 15794 32 Invention Example 14 2 359 916 1418 11.8 16732 34 Invention Example 26 16 334 1118 1635 11.2 18312 19 Invention Example 27 24 355 952 1538 11.1 17072 32 Invention Example 28 2 367 797 1207 13.8 16657 36 Invention Example 29 16 389 907 1524 11.2 17069 29 Invention Example 30 14 359 918 1457 12.1 17630 30 Invention Example 31 0 334 1094 1497 11.3 16916 18 Invention Example

Claims

1. A high strength steel sheet having a tensile strength of 900 MPa or higher, comprising a composition including, on a mass basis:

C: 0.1% or more and 0.3% or less;
Si: 2.0% or less;
Mn: 0.5% or more and 3.0% or less;
P: 0.1% or less;
S: 0.07% or less;
Al: 1.0% or less; and
N: 0.008% or less, with the balance Fe and incidental impurities,
with a steel microstructure including, on an area ratio basis, 5% or more and 80% or less of ferrite, 15% or more of autotempered martensite, 10% or less of bainite, 5% or less of retained austenite, and 40% or less of as-quenched martensite; a mean hardness of the autotempered martensite is HV≦700; and the mean number of precipitated iron-based carbide grains each having a size of 5 nm or more and 0.5 μm or less and included in the autotempered martensite is 5×104 or more per 1 mm2.

2. The high strength steel sheet according to claim 1, further comprising, on a mass basis, at least one element selected from:

Cr: 0.05% or more and 5.0% or less;
V: 0.005% or more and 1.0% or less; and
Mo: 0.005% or more and 0.5% or less.

3. The high strength steel sheet according to claim 1, further comprising, on a mass basis, at least one element selected from:

Ti: 0.01% or more and 0.1% or less;
Nb: 0.01% or more and 0.1% or less;
B: 0.0003% or more and 0.0050% or less;
Ni: 0.05% or more and 2.0% or less; and
Cu: 0.05% or more and 2.0% or less.

4. The high strength steel sheet according to claim 1, further comprising, on a mass basis, at least one element selected from:

Ca: 0.001% or more and 0.005% or less; and
REM: 0.001% or more and 0.005% or less.

5. The high strength steel sheet according to claim 1, wherein the area ratio of autotempered martensite in which the number of precipitated iron-based carbide grains each having a size of 0.1 μm or more and 0.5 μm or less is 5×102 or less per 1 mm2 to the entire autotempered martensite is 3% or more.

6. The high strength steel sheet according to claim 1, wherein a galvanized layer is disposed on a surface of the steel sheet.

7. The high strength steel sheet according to claim 1, wherein a galvannealed layer is disposed on a surface of the steel sheet.

8. A method for manufacturing a high strength steel sheet, comprising:

hot-rolling and then cold-rolling a slab to be formed into a steel sheet having the composition according to claim 1 to form a cold-rolled steel sheet;
annealing the cold-rolled steel sheet in a first temperature range of 700° C. or higher and 950° C. or lower for 15 seconds or longer and 600 seconds or shorter;
in a second temperature range, which is a temperature range from the first temperature range to 420° C., cooling the steel sheet from the first temperature range to 550° C. at an average cooling rate of 3° C./s or higher and cooling the steel sheet from 550° C. to 420° C. within 600 seconds; and
cooling the steel sheet at a cooling rate of 50° C./s or lower in a third temperature range of 250° C. or higher and 420° C. or lower to perform, in the third temperature range, autotempering treatment in which martensite transformation is caused while at the same time the transformed martensite is tempered.

9. The method according to claim 8, wherein, when the steel sheet is cooled at a cooling rate of 50° C./s or lower in the third temperature range of 250° C. or higher and 420° C. or lower, the steel sheet is cooled at a cooling rate of 1.0° C./s or higher and 50° C./s or lower in a temperature range of at least (Ms temperature−50)° C. or lower to perform, in the third temperature range, autotempering treatment in which martensite transformation is caused while at the same time the transformed martensite is tempered.

10. The method according to claim 8, wherein martensite start temperature Ms of the slab is approximated by M represented by Formula (1) below, and the M is 300° C. or higher: where [X %] is mass % of a constituent element X of the slab and [α%] is an area ratio (%) of polygonal ferrite.

M(° C.)=540−361×{[C %]/(1−[α%]/100)}−6×[Si %]−40×[Mn %]+30×[Al %]−20×[Cr %]−35×[V %]−10×[Mo %]−17×[Ni %]−10×[Cu %]  (1)

11. The method according to claim 9, wherein martensite start temperature Ms of the slab is approximated by M represented by Formula (1) below, and the M is 300° C. or higher: where [X %] is mass % of a constituent element X of the slab and [α%] is an area ratio (%) of polygonal ferrite.

M(° C.)=540−361×{[C %]/(1−[α%]/100)}−6×[Si %]−40×[Mn %]+30×[Al %]−20×[Cr %]−35×[V %]−10×[Mo %]−17×[Ni %]−10×[Cu %]  (1)

12. The high strength steel sheet according to claim 2, further comprising, on a mass basis, at least one element selected from:

Ti: 0.01% or more and 0.1% or less;
Nb: 0.01% or more and 0.1% or less;
B: 0.0003% or more and 0.0050% or less;
Ni: 0.05% or more and 2.0% or less; and
Cu: 0.05% or more and 2.0% or less.

13. The high strength steel sheet according to claim 2, further comprising, on a mass basis, at least one element selected from:

Ca: 0.001% or more and 0.005% or less; and
REM: 0.001% or more and 0.005% or less.

14. The high strength steel sheet according to claim 3, further comprising, on a mass basis, at least one element selected from:

Ca: 0.001% or more and 0.005% or less; and
REM: 0.001% or more and 0.005% or less.

15. The high strength steel sheet according to claim 2, wherein the area ratio of autotempered martensite in which the number of precipitated iron-based carbide grains each having a size of 0.1 μm or more and 0.5 μm or less is 5×102 or less per 1 mm2 to the entire autotempered martensite is 3% or more.

16. The high strength steel sheet according to claim 3, wherein the area ratio of autotempered martensite in which the number of precipitated iron-based carbide grains each having a size of 0.1 μm or more and 0.5 μm or less is 5×102 or less per 1 mm2 to the entire autotempered martensite is 3% or more.

17. The high strength steel sheet according to claim 4, wherein the area ratio of autotempered martensite in which the number of precipitated iron-based carbide grains each having a size of 0.1 μm or more and 0.5 μm or less is 5×102 or less per 1 mm2 to the entire autotempered martensite is 3% or more.

18. The high strength steel sheet according to claim 2, wherein a galvanized layer is disposed on a surface of the steel sheet.

19. The high strength steel sheet according to claim 3, wherein a galvanized layer is disposed on a surface of the steel sheet.

20. The high strength steel sheet according to claim 4, wherein a galvanized layer is disposed on a surface of the steel sheet.

Patent History
Publication number: 20110030854
Type: Application
Filed: Jan 29, 2009
Publication Date: Feb 10, 2011
Applicant: JFE STEEL CORPORATION (Tokyo)
Inventors: Hiroshi Matsuda (Tokyo), Reiko Mizuno (Tokyo), Yoshimasa Funakawa (Tokyo), Yasushi Tanaka (Tokyo), Tatsuya Nakagaito (Tokyo), Saiji Matsuoka (Tokyo)
Application Number: 12/865,527
Classifications
Current U.S. Class: With Working Step (148/504); Age Or Precipitation Hardened Or Strengthed (148/328); With Working (148/624)
International Classification: C21D 11/00 (20060101); C22C 38/00 (20060101); C21D 8/02 (20060101); C22C 38/04 (20060101); C22C 38/18 (20060101); C22C 38/12 (20060101); C22C 38/02 (20060101); C22C 37/06 (20060101); C22C 38/60 (20060101);