HIGH-YIELD-RATIO HIGH-STRENGTH ELECTROGALVANIZED STEEL SHEET AND METHOD FOR MANUFACTURING THE SAME

Information

  • Patent Application
  • 20210381085
  • Publication Number
    20210381085
  • Date Filed
    August 06, 2019
    4 years ago
  • Date Published
    December 09, 2021
    2 years ago
Abstract
A high-yield-ratio high-strength electrogalvanized steel sheet having an electrogalvanized coating layer formed on a surface of a base steel sheet, in which the base steel sheet has a certain chemical composition, and a steel microstructure, in which a total area fraction of one or both of bainite containing carbides having an average grain diameter of 50 nm or less and tempered martensite containing carbides having an average grain diameter of 50 nm or less is 90% or more in the whole of the steel microstructure, and in which a total area fraction of one or both of the bainite containing and the tempered martensite containing carbides is 80% or more in a region from the surface of the base steel sheet to a position located at ⅛ of a thickness of the base steel sheet, and diffusible hydrogen in steel in an amount of 0.20 mass ppm or less.
Description
FIELD OF THE INVENTION

The present invention relates to a high-yield-ratio high-strength electrogalvanized steel sheet and a method for manufacturing the steel sheet. In more detail, the present invention relates to a high-yield-ratio high-strength electrogalvanized steel sheet which is used for automobile parts and the like and a method for manufacturing the steel sheet, and, in particular, to a high-yield-ratio high-strength electrogalvanized steel sheet having excellent bendability and a method for manufacturing the steel sheet.


BACKGROUND OF THE INVENTION

Nowadays, since there is an active trend toward decreasing the weight of an automobile body, the strength of a steel sheet which is used for an automobile body is being increased to decrease the thickness of the steel sheet and to thereby decrease the weight of the automobile body. In particular, there has been a growing trend toward using a high-strength steel sheet having a TS (tensile strength) of 1320 MPa to 1470 MPa class for automobile body skeleton parts such as those for center pillar R/F (reinforcement), bumpers, impact beam parts, and the like (hereinafter, also referred to as “parts”). Moreover, consideration is also being given to using a steel sheet having strength represented by a TS of 1800 MPa class (1.8 GPa class) or above to further decrease the weight of an automobile body. In addition, there is an increasing demand for a steel sheet having a high yield ratio from the viewpoint of collision safety.


There is concern of delayed fracturing (hydrogen embrittlement) occurring due to an increase in the strength of a steel sheet. Nowadays, due to a coating layer, it becomes difficult to release hydrogen which enters a steel sheet in the manufacturing process of the steel sheet, which suggests an increased risk of fracturing occurring when the steel sheet is subjected to stress.


For example, Patent Literature 1 discloses a technique for improving delayed fracture resistance by controlling the amount of carbides. Specifically, Patent Literature 1 provides an ultrahigh-strength steel sheet having a tensile strength of 980 MPa or more and good delayed fracture resistance, the steel sheet having a chemical composition containing, by mass %, C: 0.05% to 0.25%, Mn: 1.0% to 3.0%, S: 0.01% or less, Al: 0.025% to 0.100%, and N: 0.008% or less and a microstructure in which the amount of precipitates having a grain diameter of 0.1 μm or less in martensite is 3×105/m2 or less.


In addition, Patent Literature 2 provides a high-strength steel sheet having a high yield ratio, excellent bendability, and a tensile strength of 1.0 GPa to 1.8 GPa, the steel sheet having a chemical composition containing, by mass %, C: 0.12% to 0.3%, Si: 0.5% or less, Mn: less than 1.5%, P: 0.02% or less, S: 0.01% or less, Al: 0.15% or less, N: 0.01% or less, and a balance of Fe and inevitable impurities and a tempered martensite single-phase structure.


In addition, Patent Literature 3 provides a high-strength steel sheet having an excellent strength-ductility balance and a tensile strength of 980 MPa to 1.8 GPa, the steel sheet having a chemical composition containing, by mass %, C: 0.17% to 0.73%, Si: 3.0% or less, Mn: 0.5% to 3.0%, P: 0.1% or less, S: 0.07% or less, Al: 3.0% or less, N: 0.010% or less, and a balance of Fe and inevitable impurities and a microstructure in which a martensite phase is formed to increase strength, in which retained austenite necessary to realize a TRIP effect is stably formed by utilizing upper bainite transformation, and in which some portion of martensite is made into tempered martensite.


PATENT LITERATURE

PTL 1: Japanese Unexamined Patent Application Publication No. 7-197183


PTL 2: Japanese Unexamined Patent Application Publication No. 2011-246746


PTL 3: Japanese Unexamined Patent Application Publication No. 2010-90475


SUMMARY OF THE INVENTION

Since a steel sheet which is used for an automobile body is subjected to press forming, fracturing occurring in the steel sheet starts at an end surface which is formed when shearing or punching is performed (hereinafter, referred to as “sheared end surface”) in many cases. Moreover, it is clarified that such fracturing tends to be caused by hydrogen which exists in steel. Therefore, it is necessary to evaluate fracturing by evaluating crack growth from a sheared end surface. In addition, when a steel sheet is subjected to forming for use in an automobile, stress is applied by performing bending work. Therefore, to evaluate fracturing, it is necessary to evaluate bendability by performing bending work on a small piece having a sheared end surface.


In the case of the technique disclosed in Patent Literature 1, delayed fracturing is evaluated by immersing a test piece in an acidic solution for a certain time after applying bending stress to the test piece and by applying an electrical potential to cause hydrogen to enter the steel. However, in such a test, since delayed fracturing is evaluated by forcibly causing hydrogen to enter the steel sheet, it is not possible to evaluate the effect of hydrogen which enters a steel sheet in the manufacturing process of the steel sheet.


In the case of the technique disclosed in Patent Literature 2, although it is possible to achieve excellent strength as a result of forming a tempered martensite single-phase structure, since it is not possible to decrease the amount of inclusions, which promote crack growth, it is considered that there is no improvement in bendability.


In the case of the technique disclosed in Patent Literature 3, although there is no mention of bendability, it is considered that there is no improvement in bendability, because it is considered that the amount of diffusible hydrogen in steel is large in the steel specified by Patent Literature 3, in which a large amount of austenite is utilized. This is because the amount of solid solution hydrogen is larger in austenite, which has an FCC structure, than in martensite or bainite, which has a BCC structure or a BCT structure.


An object according to aspects of the present invention is to provide a high-yield-ratio high-strength electrogalvanized steel sheet having excellent bendability and a method for manufacturing the steel sheet.


Here, in accordance with aspects of the present invention, the expression “high-yield-ratio high-strength” denotes a case of a yield ratio of 0.80 or more and a tensile strength of 1320 MPa or more.


In addition, the expression “the surface of a base steel sheet” of an electrogalvanized steel sheet denotes the interface between the base steel sheet and the electrogalvanized coating layer.


In addition, a region from the surface of the base steel sheet to a position located at ⅛ of the thickness of the base steel sheet is referred to as a “surface layer”.


The present inventors diligently conducted investigations to solve the problems described above and, as a result, found that it is necessary to decrease the amount of diffusible hydrogen in steel to 0.20 mass ppm or less to achieve excellent bendability. In addition, the present inventors found that diffusible hydrogen in steel is released by cooling the steel sheet to a low temperature before an electrogalvanizing treatment is performed and succeeded in manufacturing an electrogalvanized steel sheet having excellent bendability. In addition, it was found that, by performing rapid cooling in such a cooling process, it is possible to form a microstructure mainly including tempered martensite and bainite and to thereby achieve a high yield ratio and high strength.


As described above, the present inventors conducted various investigations to solve the problems described above and, as a result, found that it is possible to obtain a high-yield-ratio high-strength electrogalvanized steel sheet having excellent bendability by decreasing the amount of diffusible hydrogen in steel and completed in accordance with aspects of the present invention. The subject matter of aspects of the present invention is as follows.


[1] A high-yield-ratio high-strength electrogalvanized steel sheet having an electrogalvanized coating layer formed on a surface of a base steel sheet, in which the base steel sheet has a chemical composition containing, by mass %, C: 0.14% or more and 0.40% or less, Si: 0.001% or more and 2.0% or less, Mn: 0.10% or more and 1.70% or less, P: 0.05% or less, S: 0.0050% or less, Al: 0.01% or more and 0.20% or less, N: 0.010% or less, and a balance of Fe and inevitable impurities, a steel microstructure, in which a total area fraction of one or both of bainite containing carbides having an average grain diameter of 50 nm or less and tempered martensite containing carbides having an average grain diameter of 50 nm or less is 90% or more in the whole of the steel microstructure, and in which a total area fraction of one or both of bainite containing carbides having an average grain diameter of 50 nm or less and tempered martensite containing carbides having an average grain diameter of 50 nm or less is 80% or more in a region from the surface of the base steel sheet to a position located at ⅛ of a thickness of the base steel sheet, and diffusible hydrogen in steel in an amount of 0.20 mass ppm or less.


[2] The high-yield-ratio high-strength electrogalvanized steel sheet according to item [1], in which the base steel sheet has the chemical composition and the steel microstructure, the steel microstructure includes carbides having an average grain diameter of 0.1 μm or more and inclusions, and a sum of perimeters of the carbides having an average grain diameter of 0.1 μm or more and the inclusions is 50 μm/mm2 or less.


[3] The high-yield-ratio high-strength electrogalvanized steel sheet according to item [1] or [2], in which the chemical composition further contains, by mass %, B: 0.0002% or more and less than 0.0035%.


[4] The high-yield-ratio high-strength electrogalvanized steel sheet according to any one of items [1] to [3], in which the chemical composition further contains, by mass %, one or both selected from Nb: 0.002% or more and 0.08% or less and Ti: 0.002% or more and 0.12% or less.


[5] The high-yield-ratio high-strength electrogalvanized steel sheet according to any one of items [1] to [4], in which the chemical composition further contains, by mass %, one or both selected from Cu: 0.005% or more and 1% or less and Ni: 0.01% or more and 1% or less.


[6] The high-yield-ratio high-strength electrogalvanized steel sheet according to any one of items [1] to [5], in which the chemical composition further contains, by mass %, one, two, or more selected from Cr: 0.01% or more and 1.0% or less, Mo: 0.01% or more and less than 0.3%, V: 0.003% or more and 0.5% or less, Zr: 0.005% or more and 0.20% or less, and W: 0.005% or more and 0.20% or less.


[7] The high-yield-ratio high-strength electrogalvanized steel sheet according to any one of items [1] to [6], in which the chemical composition further contains, by mass %, one, two, or more selected from Ca: 0.0002% or more and 0.0030% or less, Ce: 0.0002% or more and 0.0030% or less, La: 0.0002% or more and 0.0030% or less, and Mg: 0.0002% or more and 0.0030% or less.


[8] The high-yield-ratio high-strength electrogalvanized steel sheet according to any one of items [1] to [7], in which the chemical composition further contains, by mass %, one or both selected from Sb: 0.002% or more and 0.1% or less and Sn: 0.002% or more and 0.1% or less.


[9] A method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet, the method including a hot rolling process of performing hot rolling on a steel slab having the chemical composition according to any one of items [1] to [8] with a slab heating temperature of 1200° C. or higher and a finishing delivery temperature of 840° C. or higher, cooling the hot-rolled steel sheet to a primary cooling stop temperature of 700° C. or lower in such a manner that cooling is performed at an average cooling rate of 40° C./sec or higher in a temperature range from the finishing delivery temperature to a temperature of 700° C., further cooling the cooled steel sheet to a coiling temperature of 630° C. or lower in such a manner that cooling is performed at an average cooling rate of 2° C./sec or higher in a temperature range from the primary cooling stop temperature to a temperature of 650° C., and coiling the cooled steel sheet, an annealing process of holding the steel sheet obtained in the hot rolling process at an annealing temperature equal to or higher than the AC3 temperature for 30 seconds or more, cooling the held steel sheet from a cooling start temperature of 680° C. or higher to a cooling stop temperature of 260° C. or lower in such a manner that cooling is performed at an average cooling rate of 70° C./sec or higher in a temperature range of 680° C. to 260° C., and holding the cooled steel sheet at a holding temperature of 150° C. to 260° C. for 20 seconds to 1500 seconds, and an electroplating process of cooling the steel sheet after the annealing process to room temperature and performing an electrogalvanizing treatment on the cooled steel sheet for an electrogalvanizing time of 300 seconds or less.


[10] The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to item [9], the method further including a cold rolling process of performing cold rolling on the steel sheet after the hot rolling process between the hot rolling process and the annealing process.


[11] The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to item [9] or [10], the method further including a tempering process of holding the steel sheet after the electroplating process in a temperature range of 250° C. or lower for a holding time t which satisfies relational expression (1) below.





(T+273)(log t+4)≤2700  (1)


Here, in relational expression (1), T denotes a holding temperature (° C.) in the tempering process and t denotes the holding time (sec) in the tempering process.


[12] The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to any one of items [9] to [11], in which a rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature in the hot rolling process is 200 seconds or less.


In accordance with aspects of the present invention, by controlling the chemical composition and the manufacturing method, the steel microstructure is controlled so that there is a decrease in the amount of diffusible hydrogen in steel. As a result, the high-yield-ratio high-strength electrogalvanized steel sheet according to aspects of the present invention has excellent bendability.


By using the high-yield-ratio high-strength electrogalvanized steel sheet according to aspects of the present invention for the structural members of an automobile, it is possible to obtain a steel sheet for an automobile having both increased strength and improved bendability. That is, aspects of the present invention provide an automobile body with enhanced performance.







DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION

Hereafter, the embodiments of the present invention will be described. Here, the present invention is not limited to the embodiments below.


The high-yield-ratio high-strength electrogalvanized steel sheet according to aspects of the present invention has an electrogalvanized coating layer formed on the surface of a steel sheet, which is the material of the high-yield-ratio high-strength electrogalvanized steel sheet, that is, a base steel sheet.


First, the chemical composition of the base steel sheet (hereafter, also simply referred to as “steel sheet”) according to aspects of the present invention will be described. In the description of the chemical composition below, “%”, which is a unit of the content of each of the constituents of the chemical composition, denotes “mass %”.


C: 0.14% or More and 0.40% or Less


Since C is an element which improves hardenability, C is necessary to achieve a predetermined area fraction of tempered martensite and/or bainite. In addition, C is necessary to increase the strength of tempered martensite and bainite and to thereby achieve a TS of 1320 MPa or more and a YR of 0.80 or more. In addition, as a result of hydrogen in steel being trapped due to carbides being finely dispersed, since there is a decrease in the amount of diffusible hydrogen in steel, there is an improvement in bendability. In the case where the C content is less than 0.14%, it is not possible to achieve excellent bendability or predetermined strength. Therefore, the C content is set to be 0.14% or more. Here, it is preferable that the C content be more than 0.18% or more preferably 0.20% or more to achieve higher TS, that is, a TS of 1470 MPa or more. On the other hand, in the case where the C content is more than 0.40%, since there is an increase in the grain diameter of carbides inside tempered martensite and bainite, there is a deterioration in bendability. Therefore, the C content is set to be 0.40% or less, preferably 0.38% or less, or more preferably 0.36% or less.


Si: 0.001% or More and 2.0% or Less


Si is an element which increases strength through solid solution strengthening. In addition, when a steel sheet is tempered at a temperature range of 200° C. or higher, Si contributes to improving bendability by inhibiting the formation of an excessive amount of carbides having a large grain dimeter. Moreover, Si also contributes to inhibiting the formation of MnS by decreasing the amount of Mn segregated in the central portion in the thickness direction. In addition, Si also contributes to inhibiting decarburization and deboronization due to oxidation of the surface layer of a steel sheet when continuous annealing is performed. Here, to sufficiently realize the effects described above, the Si content is set to be 0.001% or more, preferably 0.003% or more, or more preferably 0.005% or more. On the other hand, in the case where the Si content is excessively high, since the segregation of Si is expanded in the thickness direction, MnS having a large grain diameter tends to be formed in the thickness direction, which results in a deterioration in bendability. Therefore, the Si content is set to be 2.0% or less, preferably 1.5% or less, or more preferably 1.2% or less.


Mn: 0.10% or More and 1.70% or Less


Mn is added to improve the hardenability of steel and to thereby achieve a predetermined area fraction of tempered martensite and/or bainite. In the case where the Mn content is less than 0.10%, since ferrite is formed in the surface layer of a steel sheet, there is a decrease in strength and yield ratio. Therefore, the Mn content is set to be 0.10% or more, preferably 0.40% or more, or more preferably 0.80% or more. On the other hand, Mn is an element which particularly promotes the formation of MnS and an increase in the grain diameter thereof. In the case where the Mn content is more than 1.70%, since there is an increase in the amount of inclusions having a large grain diameter, there is a marked deterioration in bendability. Therefore, the Mn content is set to be 1.70% or less, preferably 1.60% or less, or more preferably 1.50% or less.


P: 0.05% or Less


P is an element which increases the strength of steel. However, in the case where the P content is high, since crack generation is promoted, there is a marked deterioration in bendability. Therefore, the P content is set to be 0.05% or less, preferably 0.03% or less, or more preferably 0.01% or less. Here, although there is no particular limitation on the lower limit of the P content, the lower limit within an industrially feasible range is about 0.003% at present.


S: 0.0050% or Less


Since S has a strong negative effect on bendability through the formation of MnS, TiS, Ti(C, S), or the like, it is necessary to strictly control the S content. To decrease such a negative effect due to inclusions, it is necessary that the S content be 0.0050% or less, preferably 0.0020% or less, more preferably 0.0010% or less, or even more preferably 0.0005% or less. Here, although there is no particular limitation on the lower limit of the S content, the lower limit within an industrially feasible range is about 0.0002% at present.


Al: 0.01% or More and 0.20% or Less


Al is added to sufficiently perform deoxidation and thereby to decrease the amount of inclusions having a large grain diameter in steel. To realize such an effect, the Al content is set to be 0.01% or more or preferably 0.02% or more. On the other hand, in the case where the Al content is more than 0.20%, since carbides such as cementite which are formed when coiling is performed after hot rolling has been performed and which contain mainly Fe are less likely to form a solid solution in an annealing process, inclusions and carbides having a large grain diameter are formed, which results in a deterioration in bendability. Therefore, the Al content is set to be 0.20% or less, preferably 0.17% or less, or more preferably 0.15% or less.


N: 0.010% or Less


Since N is an element which forms nitride- and carbonitride-based inclusions having a large grain diameter such as TiN, (Nb, Ti) (C, N), and AlN in steel, N causes a deterioration in bendability through the formation of such inclusions. To prevent a deterioration in bendability, it is necessary that the N content be 0.010% or less, preferably 0.007% or less, or more preferably 0.005% or less. Here, although there is no particular limitation on the lower limit of the N content, the lower limit within an industrially feasible range is about 0.0006% at present.


The steel sheet according to aspects of the present invention has a chemical composition containing the constituents described above and a balance being Fe (iron) and inevitable impurities. The steel sheet according to aspects of the present invention preferably has the chemical composition consisting of the constituents described above and the balance being Fe and inevitable impurities. The steel sheet according to aspects of the present invention may further contain the constituents described below as optional constituents. Here, in the case where one of the optional constituents described below is contained in an amount less than the lower limit of the content of such a constituent, such a constituent is regarded as being contained as an inevitable impurity.


B: 0.0002% or More and Less than 0.0035%


Since B is an element which improves the hardenability of steel, it is possible to realize the effect of achieving a predetermined area fraction of tempered martensite and bainite as a result of B being added, even in the case where the Mn content is low. To realize such an effect of B, the B content is set to be 0.0002% or more, preferably 0.0005% or more, or more preferably 0.0007% or more. In addition, to fix N, it is preferable that B be added in combination with Ti whose content is 0.002% or more. On the other hand, in the case where the B content is 0.0035% or more, since there is a decrease in the dissolution rate of cementite when annealing is performed, carbides such as cementite which contain mainly Fe remain undissolved. As a result, since inclusions and carbides having a large grain diameter are formed, there is a deterioration in bendability. Therefore, the B content is set to be less than 0.0035%, preferably 0.0030% or less, or more preferably 0.0025% or less.


One or Both Selected from Nb: 0.002% or More and 0.08% or Less and Ti: 0.002% or More and 0.12% or Less


Nb and Ti contribute to increasing strength and improving bendability through a decrease in prior γ grain diameter. In addition, as a result of Nb and Ti forming carbides having a small grain diameter, since such carbides having a small grain diameter function as trap sites for trapping hydrogen so that there is a decrease in the amount of diffusible hydrogen in steel, there is an improvement in bendability. To realize such an effect, it is necessary that at least one of Nb and Ti be added in an amount of 0.002% or more, preferably 0.003% or more, or more preferably 0.005% or more. On the other hand, in the case where the Nb content or the Ti content is large, since there is an increase in the amounts of Nb-based precipitates having a large grain diameter such as NbN, Nb(C, N), and (Nb, Ti) (C, N) and Ti-based precipitates having a large grain diameter such as TiN, Ti(C, N), Ti(C, S), and TiS which remain undissolved when slab heating is performed in a hot rolling process, there is a deterioration in bendability. Therefore, the Nb content is set to be 0.08% or less, preferably 0.06% or less, or more preferably 0.04% or less. The Ti content is set to be 0.12% or less, preferably 0.10% or less, or more preferably 0.08% or less.


One or Both Selected from Cu: 0.005% or More and 1% or Less and Ni: 0.01% or More and 1% or Less


Cu and Ni are effective for improving the corrosion resistance of an automobile in its practical service environment, and corrosion products thereof are effective for inhibiting hydrogen from entering a steel sheet as a result of coating the surface of the steel sheet. To realize such effects, it is necessary that the Cu content be 0.005% or more. It is necessary that the Ni content be 0.01% or more. To improve bendability, it is preferable that each of the Cu content and the Ni content be 0.05% or more or more preferably 0.08% or more. However, in the case where the Cu content or the Ni content is excessively large, since the occurrence of surface defects is brought about, there is a deterioration in coatability or phosphatability. Therefore, each of the Cu content and the Ni content is set to be 1% or less, preferably 0.8% or less, or more preferably 0.6% or less.


One, Two, or More Selected from Cr: 0.01% or More and 1.0% or Less, Mo: 0.01% or More and Less than 0.3%, V: 0.003% or More and 0.5% or Less, Zr: 0.005% or More and 0.20% or Less, and W: 0.005% or More and 0.20% or Less


Cr, Mo, and V may be added to improve the hardenability of steel and to increase the effect of improving bendability due to a decrease in the grain diameter of tempered martensite. To realize such effects, it is necessary that each of the Cr content and the Mo content be 0.01% or more, preferably 0.02% or more, or more preferably 0.03% or more. It is necessary that the V content be 0.003% or more, preferably 0.005% or more, or more preferably 0.007% or more. However, in the case where the content of any one of these elements is excessively large, there is a deterioration in bendability due to an increase in the grain diameter of carbides. Therefore, the Cr content is set to be 1.0% or less, preferably 0.4% or less, or more preferably 0.2% or less. The Mo content is set to be less than 0.3%, preferably 0.2% or less, or more preferably 0.1% or less. The V content is set to be 0.5% or less, preferably 0.4% or less, or more preferably 0.3% or less.


Zr and W contribute to increasing strength and improving bendability through a decrease in prior γ grain diameter. To realize such an effect, it is necessary that each of the Zr content and the W content be 0.005% or more, preferably 0.006% or more, or more preferably 0.007% or more. However, in the case where the Zr content or the W content is excessively large, since there is an increase in the amount of precipitates having a large grain diameter which remain undissolved when slab heating is performed in a hot rolling process, there is a deterioration in bendability. Therefore, each of the Zr content and the W content is set to be 0.20% or less, preferably 0.15% or less, or more preferably 0.10% or less.


One, Two, or More Selected from Ca: 0.0002% or More and 0.0030% or Less, Ce: 0.0002% or More and 0.0030% or Less, La: 0.0002% or More and 0.0030% or Less, and Mg: 0.0002% or More and 0.0030% or Less


Ca, Ce, and La contribute to improving bendability by fixing S in the form of sulfides and thereby functioning as trap sites for trapping hydrogen in steel so that there is a decrease in the amount of diffusible hydrogen in steel. To realize such an effect, it is necessary that each of the Ca content, the Ce content, and the La content be 0.0002% or more, preferably 0.0003% or more, or more preferably 0.0005% or more. On the other hand, in the case where the content of any one of these elements is large, there is a deterioration in bendability due to an increase in the grain diameter of sulfides. Therefore, each of the Ca content, Ce content, and the La content is set to be 0.0030% or less, preferably 0.0020% or less, or more preferably 0.0010% or less.


Mg contributes to improving bendability by fixing 0 in the form of MgO, which functions as a trap site for trapping hydrogen in steel so that there is a decrease in the amount of diffusible hydrogen in steel. To realize such an effect, the Mg content is set to be 0.0002% or more, preferably 0.0003% or more, or more preferably 0.0005% or more. On the other hand, in the case where the Mg content is large, since there is an increase in the grain diameter of MgO, there is a deterioration in bendability. Therefore, the Mg content is set to be 0.0030% or less, preferably 0.0020% or less, or more preferably 0.0010% or less.


One or Both Selected from Sb: 0.002% or More and 0.1% or Less and Sn: 0.002% or More and 0.1% or Less


Sb and Sn inhibit a decrease in the amounts of C and B due to oxidation and nitriding of the surface layer of a steel sheet by inhibiting oxidation and nitriding of the surface layer of the steel sheet. In addition, as a result of a decrease in the amounts of C and B being inhibited, the formation of ferrite in the surface layer of the steel sheet is inhibited, which contributes to increasing strength. To realize such effects, it is necessary that each of the Sb content and Sn content be 0.002% or more, preferably 0.003% or more, or more preferably 0.004% or more. On the other hand, in the case where any one of the Sb content and Sn content is more than 0.1%, since Sb and Sn are segregated at prior γ grain boundaries, crack generation is promoted, which results in a deterioration in bendability. Therefore, each of the Sb content and the Sn content is set to be 0.1% or less, preferably 0.08% or less, or more preferably 0.06% or less.


Hereafter, the steel microstructure of the steel sheet according to aspects of the present invention will be described.


Total area fraction of one or both of bainite containing carbides having an average grain diameter of 50 nm or less and tempered martensite containing carbides having an average grain diameter of 50 nm or less: 90% or more


To achieve both a high strength represented by a TS of 1320 MPa or more and excellent bendability, the total area fraction of bainite and/or tempered martensite containing carbides having an average grain diameter of 50 nm or less is set to be 90% or more in the whole microstructure. In the case where the total area fraction is less than 90%, since there is an increase in the amount of at least one of ferrite, retained γ (retained austenite), and martensite, there is a decrease in strength or yield ratio. Here, the total area fraction of tempered martensite and bainite described above may be 100% in the whole microstructure. In addition, a case where the area fraction of one of tempered martensite and bainite is within the range described above is satisfactory, and a case where the total area fraction of tempered martensite and bainite is within the range described above is satisfactory. Moreover, in the case where the average grain diameter of carbides inside the tempered martensite and bainite is more than 50 nm, since the carbides do not function as trap sites for trapping diffusible hydrogen in steel, and since the carbides become origins of fracture, there is a deterioration in bendability. In accordance with aspects of the present invention, the term “martensite” denotes a hard phase which is formed from austenite at a low temperature (equal to or lower than the martensite transformation temperature) and the term “tempered martensite” denotes a phase which is formed as a result of martensite being tempered when martensite is reheated. The term “bainite” denotes a hard phase which is formed from austenite at a relatively low temperature (equal to or higher than the martensite transformation temperature) and which is identified as a phase in which carbides having a small grain diameter are dispersed in ferrite having a needle- or plate-like shape. The term “average grain diameter” here denotes the average value of the grain diameters of all the carbides existing inside prior austenite in which bainite or tempered martensite is contained.


Note that examples of the remaining phases which are different from tempered martensite and bainite include ferrite, retained γ, and martensite, and it is acceptable that the total amount of the remaining phases be 10% or less in terms of area fraction. The total amount of the remaining phases described above may be 0% in terms of area fraction. In accordance with aspects of the present invention, the term “ferrite” denotes a phase which is formed through transformation from austenite at a comparatively high temperature and which composed of crystal grains having a BCC lattice structure.


Here, the area fraction of each of the phases in the steel microstructure is determined by using the method described in EXAMPLES below.


Total area fraction of one or both of bainite containing carbides having an average grain diameter of 50 nm or less and tempered martensite containing carbides having an average grain diameter of 50 nm or less: 80% or more in a region from the surface of the base steel sheet to a position located at ⅛ of the thickness of the base steel sheet


Since a crack which is generated due to bending work is generated in the surface layer on the ridge line at the bending position of a coated steel sheet, the microstructure of the surface layer of the steel sheet is significantly important. In accordance with aspects of the present invention, as a result of utilizing carbides having a small grain diameter in the surface layer as trap sites for trapping hydrogen so that there is a decrease in the amount of diffusible hydrogen in steel existing in the vicinity of the surface layer of the steel sheet, there is an improvement in bendability. Therefore, it is possible to achieve the desired bendability by controlling the total area fraction of one or both of bainite containing carbides having an average grain diameter of 50 nm or less and tempered martensite containing carbides having an average grain diameter of 50 nm or less to be 80% or more in a region from the surface of the base steel sheet to a position located at ⅛ of the thickness of the base steel sheet. It is preferable that the total area fraction described above be 82% or more or more preferably 85% or more. There is no particular limitation on the upper limit of the total area fraction described above, the total area fraction may be 100%. In addition, in the region described above, a case where the area fraction of one of tempered martensite and bainite is within the range described above is satisfactory, and a case where the total area fraction of tempered martensite and bainite is within the range described above is satisfactory.


Amount of Diffusible Hydrogen in Steel: 0.20 Mass Ppm or Less


In accordance with aspects of the present invention, the term “the amount of diffusible hydrogen” denotes the amount of accumulated hydrogen which is released when heating is performed by using a thermal desorption analytical device at a heating rate of 200° C./hr for a measuring period of time corresponding to a temperature range from a heating start temperature (25° C.) to a temperature of 200° C. from an electrogalvanized steel sheet from which the coating layer has just been removed. In the case where the amount of diffusible hydrogen in steel is more than 0.20 mass ppm, there is a deterioration in bendability. Therefore, the amount of diffusible hydrogen in steel is set to be 0.20 mass ppm or less, preferably 0.15 mass ppm or less, or more preferably 0.10 mass ppm or less. There is no particular limitation on the lower limit of the amount of diffusible hydrogen, and the amount of diffusible hydrogen may be 0 mass ppm. Here, the amount of diffusible hydrogen in steel is determined by using the method described in EXAMPLES below. In accordance with aspects of the present invention, it is necessary that the amount of diffusible hydrogen in steel be 0.20 mass ppm or less before the steel sheet is subjected to forming work or welding. However, in the case of a product (member) which has been manufactured by performing forming work or welding on a steel sheet, when the amount of diffusible hydrogen in steel of a sample taken from such a product which has been used in a common practical service environment is determined and the amount of diffusible hydrogen in steel determined is 0.20 mass ppm or less, the amount of diffusible hydrogen in steel before forming work or welding is performed is also regarded as being 0.20 mass ppm or less.


Sum of Perimeters of Carbides Having an Average Grain Diameter of 0.1 μm or More and Inclusions: 50 μm/Mm2 or Less (Preferable Condition)


In the case where inclusions or carbides having a large grain diameter are included, voids tend to be generated at the interface between the parent phase and the inclusions or the carbides. Since the frequency of void generation is proportional to the area of the interfaces between inclusions or carbides and the parent phase, decreasing the total area of the interfaces inhibits the generation of voids, thereby improving bendability. Therefore, it is preferable that the sum of perimeters (total perimeters) of carbides having an average grain diameter of 0.1 μm or more and inclusions be 50 μm/mm2 or less (50 μm or less per 1 mm2), more preferably 45 μm/mm2 or less, or even more preferably 40 μm/mm2 or less. Here, the term “average grain diameter” denotes the average value of a long side length and a short side length. The term “long side length” or “short side length” denotes the long axis length or short axis length of the equivalent ellipse of a grain. Here, the total perimeters of carbides having an average grain diameter of 0.1 μm or more and inclusions is determined by using the method described in EXAMPLES below.


The high-yield-ratio high-strength electrogalvanized steel sheet according to aspects of the present invention has an electrogalvanized coating layer formed on the surface of a steel sheet, which is the material of the high-yield-ratio high-strength electrogalvanized steel sheet, that is, a base steel sheet. There is no particular limitation on the kind of the electrogalvanized coating layer, and the kind of the electrogalvanized coating layer may be any one of, for example, a zinc coating layer (pure Zn) and a zinc-alloy coating layer (such as Zn—Ni, Zn—Fe, Zn—Mn, Zn—Cr, and Zn—Co). It is preferable that the coating weight of the electrogalvanized coating layer be 25 g/m2 per side or more to improve corrosion resistance. In addition, it is preferable that the coating weight of the electrogalvanized coating layer be 50 g/m2 per side or less to inhibit a deterioration in bendability. Although it is acceptable that the high-yield-ratio high-strength electrogalvanized steel sheet according to aspects of the present invention have an electrogalvanized coating layer on both sides or one side of the base steel sheet, it is preferable that the high-yield-ratio high-strength electrogalvanized steel sheet according to aspects of the present invention have an electrogalvanized coating layer on both sides of the base steel sheet when the high-yield-ratio high-strength electrogalvanized steel sheet is used for an automobile.


Hereafter, the properties of the high-yield-ratio high-strength electrogalvanized steel sheet according to aspects of the present invention will be described.


The high-yield-ratio high-strength electrogalvanized steel sheet according to aspects of the present invention has high strength. Specifically, the steel sheet has a tensile strength of 1320 MPa or more, preferably 1400 MPa or more, more preferably 1470 MPa or more, or even more preferably 1600 MPa or more. Here, although there is no particular limitation on the upper limit of the tensile strength, it is preferable that the tensile strength be 2200 MPa or less to easily balance the tensile strength with other properties. Here, the tensile strength is determined by using the method described in EXAMPLES below.


The high-yield-ratio high-strength electrogalvanized steel sheet according to aspects of the present invention has a high yield ratio. Specifically, the steel sheet has a yield ratio of 0.80 or more, preferably 0.81 or more, or more preferably 0.82 or more. Here, although there is no particular limitation on the upper limit of the yield ratio, it is preferable that the yield ratio be 0.95 or less to easily balance the yield ratio with other properties. In particular, it is possible to achieve a yield ratio of 0.82 or more and an a tensile strength of 1600 MPa or more by performing cooling to the cooling stop temperature in the annealing process at an average cooling rate equivalent to that of ultrarapid cooling such as water quenching under the conditions of a cooling stop temperature of 50° C. or lower and a holding temperature of 150° C. to 200° C. Here, the yield ratio is calculated from the tensile strength and the yield strength which are determined by using the method described in EXAMPLES below.


The high-yield-ratio high-strength electrogalvanized steel sheet according to aspects of the present invention has excellent bendability. Specifically, when the bending test described in EXAMPLES below is performed, the ratio of the bending radius (R) to the thickness (t), that is, R/t, is less than 3.5 in the case of a tensile strength of 1320 MPa or more and less than 1530 MPa, less than 4.0 in the case of a tensile strength of 1530 MPa or more and less than 1700 MPa, and less than 4.5 in the case of a tensile strength of 1700 MPa or more. It is preferable that R/t be 3.0 or less in the case of a tensile strength of 1320 MPa or more and less than 1530 MPa, 3.5 or less in the case of a tensile strength of 1530 MPa or more and less than 1700 MPa, and 4.0 or less in the case of a tensile strength of 1700 MPa or more.


Hereafter, the method for manufacturing the high-yield-ratio high-strength electrogalvanized steel sheet according to an embodiment of the present invention will be described.


The method for manufacturing the high-yield-ratio high-strength electrogalvanized steel sheet according to the embodiment of the present invention includes at least a hot rolling process, an annealing process, and an electroplating process. In addition, a cold rolling process may be included between the hot rolling process and the annealing process. In addition, a tempering process may be included after the electroplating process. Hereafter, each of the processes will be described. Here, the temperature described below denotes the temperature of the surface of a slab, a steel sheet, or the like.


Hot Rolling Process


The hot rolling process is a process of performing hot rolling on a steel slab having the chemical composition described above with a slab heating temperature of 1200° C. or higher and a finishing delivery temperature of 840° C. or higher, cooling the hot-rolled steel sheet to a primary cooling stop temperature of 700° C. or lower in such a manner that cooling is performed at an average cooling rate of 40° C./sec or higher in a temperature range from the finishing delivery temperature to a temperature of 700° C., further cooling the cooled steel sheet to a coiling temperature of 630° C. or lower in such a manner that cooling is performed at an average cooling rate of 2° C./sec or higher in a temperature range from the primary cooling stop temperature to a temperature of 650° C., and coiling the cooled steel sheet.


The steel slab having the chemical composition described above is subjected to hot rolling. By controlling the slab heating temperature to be 1200° C. or higher, since it is possible to promote the dissolution of sulfides and inhibit the segregation of Mn, it is possible to decrease the amounts of the inclusions and the carbides having a large grain diameter described above, which results in an improvement in bendability. Therefore, the slab heating temperature is set to be 1200° C. or higher, preferably 1230° C. or higher, or more preferably 1250° C. or higher. Although there is no particular limitation on the upper limit of the slab heating temperature, it is preferable that the slab heating temperature be 1400° C. or less. In addition, for example, it is acceptable that the heating rate for slab heating be 5° C./min to 15° C./min and that the slab soaking time be 30 minutes to 100 minutes.


It is preferable that the rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature in the hot rolling process be 200 seconds or less. By decreasing the rolling time, it is possible to inhibit the formation of carbonitrides having a large grain diameter and inclusions. In addition, even if inclusions are formed, it is possible to inhibit an increase in the grain diameter of the inclusions. Therefore, by decreasing the rolling time, it is possible to contribute to improving bendability. As described above, it is preferable that the rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature be 200 seconds or less, more preferably 180 seconds or less, or even more preferably 160 seconds or less. Although there is no particular limitation on the lower limit of the rolling time, it is preferable that the rolling time be 40 seconds or more.


It is necessary that the finishing delivery temperature be 840° C. or higher. In the case where the finishing delivery temperature is lower than 840° C., since there is an increase in the time required for reaching the finishing delivery temperature, there is a deterioration in bendability due to the formation of carbides having a large grain diameter and inclusions, and there may be a deterioration in the internal quality of the steel sheet. Therefore, it is necessary that the finishing delivery temperature be 840° C. or higher or preferably 860° C. or higher. On the other hand, although there is no particular limitation on the upper limit of the finishing delivery temperature, cooling to the coiling temperature is difficult in the case of an excessively high finishing delivery temperature. Therefore, it is preferable that the finishing delivery temperature be 950° C. or lower, or more preferably 920° C. or lower.


After finish rolling has been performed, cooling is performed at an average cooling rate of 40° C./sec or higher in a temperature range from the finishing delivery temperature to a temperature of 700° C. In the case where the cooling rate is low, since inclusions are formed, and since there is an increase in the grain diameter of the formed inclusions, there is a deterioration in bendability. In addition, since there is a decrease in the area fraction of martensite and bainite, which contain carbides, in the surface layer of the steel due to the decarburization of the surface layer, there is a decrease in the amount of carbides having a small grain diameter, which function as trap sites for trapping hydrogen in the vicinity of the surface layer, which makes it difficult to achieve the desired bendability. Therefore, after finish rolling has been performed, the average cooling rate in a temperature range from the finishing delivery temperature to a temperature of 700° C. is set to be 40° C./sec or higher or preferably 50° C./sec or higher. Although there is no particular limitation on the upper limit of the average cooling rate, it is preferable that upper limit of the average cooling rate be about 250° C./sec. In addition, the primary cooling stop temperature is set to be 700° C. or lower. In the case where the primary cooling stop temperature is higher than 700° C., since carbides tend to be formed in a temperature range higher than 700° C., and since there is an increase in the grain diameter of the formed carbides, there is a deterioration in bendability. Although there is no particular limitation on the lower limit of the primary cooling stop temperature, there is a decrease in the effect of inhibiting the formation of carbides due to rapid cooling in the case where the primary cooling stop temperature is 650° C. or lower. Therefore, it is preferable that the primary cooling stop temperature be higher than 650° C.


Subsequently, cooling is performed to a coiling temperature of 630° C. or lower in such a manner that cooling is performed at an average cooling rate of 2° C./sec or higher in a temperature range from the primary cooling stop temperature to a temperature of 650° C. In the case where the cooling rate to a temperature of 650° C. is low, since inclusions are formed, and since there is an increase in the grain diameter of the formed inclusions, there is a deterioration in bendability. In addition, since there is a decrease in the area fraction of martensite and bainite, which contain carbides, in the surface layer of the steel due to the decarburization of the surface layer, there is a decrease in the amount of carbides having a small grain diameter, which function as trap sites for trapping hydrogen in the vicinity of the surface layer, which makes it difficult to achieve the desired bendability. Therefore, as described above, after cooling has been performed to the primary cooling stop temperature of 700° C. or lower in such a manner that cooling is performed at an average cooling rate of 40° C./sec or higher in a temperature range higher than 700° C., the average cooling rate from the primary cooling stop temperature to a temperature of 650° C. is set to be 2° C./sec or more, preferably 3° C./sec or more, or more preferably 5° C./sec. Although there is no particular limitation on the average cooling rate from a temperature of 650° C. to the coiling temperature, it is preferable that the average cooling rate be 0.1° C./sec or higher and 100° C./sec or lower.


Here, the average cooling rate is calculated by using the expression (cooling start temperature−cooling stop temperature)/(cooling time in a temperature range from cooling start temperature to cooling stop temperature), unless otherwise noted.


The coiling temperature is set to be 630° C. or lower. In the case where the coiling temperature is higher than 630° C., since there is a risk of decarburization occurring on the surface of the base steel sheet, a difference in microstructure is produced between the inside and surface of the steel sheet, which results in a variation in alloy concentrations. In addition, since ferrite is formed due to decarburization in the surface layer, there is a decrease in tensile strength, yield ratio, or both. Therefore, the coiling temperature is set to be 630° C. or lower, or preferably 600° C. or lower. Although there is no particular limitation on the lower limit of the coiling temperature, it is preferable that the coiling temperature be 500° C. or higher to inhibit a deterioration in cold rolling capability in the case where cold rolling is performed.


The hot-rolled steel sheet after coiling has been performed may be subjected to pickling. There is no particular limitation on the conditions applied for pickling. Here, pickling need not be performed on the hot-rolled steel sheet.


Cold Rolling Process


The cold rolling process is a process of performing cold rolling on the hot-rolled steel sheet obtained in the hot rolling process. Although there is no particular limitation on the rolling reduction ratio when cold rolling is performed, there is a risk of a deterioration in the flatness of the surface and risk of a variation in microstructure in the case where the rolling reduction ratio is less than 20%. Therefore, it is preferable that the rolling reduction ratio be 20% or more. Here, the cold rolling process is not an indispensable process, and the cold rolling process may be omitted as long as the steel microstructure and the mechanical properties satisfy the requirements according to aspects of the present invention.


Annealing Process


The annealing process is a process of holding (soaking) the cold-rolled steel sheet or the hot-rolled steel sheet at an annealing temperature equal to or higher than the AC3 temperature for 30 seconds or more, cooling the held steel sheet from a cooling start temperature of 680° C. or higher to a cooling stop temperature of 260° C. or lower in such a manner that cooling is performed at an average cooling rate of 70° C./sec or higher in a temperature range of 680° C. to 260° C., and holding the cooled steel sheet at a holding temperature of 150° C. to 260° C. for 20 seconds to 1500 seconds.


The hot-rolled steel sheet or the cold-rolled steel sheet is heated to the annealing temperature equal to or higher than the AC3 temperature and soaked thereafter. In the case where the annealing temperature is lower than the AC3 temperature, since there is an excessive increase in the amount of ferrite, it is difficult to obtain a steel sheet having a YR of 0.80 or more. Therefore, it is necessary that the annealing temperature be equal to or higher than the AC3 temperature, preferably equal to or higher than the AC3 temperature+10° C. Although there is no particular limitation on the upper limit of the annealing temperature, it is preferable that the annealing temperature be 910° C. or lower to inhibit an increase in austenite grain diameter and to thereby inhibit a deterioration in bendability.


Here, the AC3 temperature (° C.) is calculated by using the equation below. In addition, in the equation below, under the assumption that symbol M is used instead of the atomic symbol of some element, symbol (% M) denotes the content (mass %) of the element denoted by symbol M.





AC3=910−203(% C)1/2+45(% Si)−30(% Mn)−20(% Cu)−15(% Ni)+11(% Cr)+32(% Mo)+104(% V)+400(% Ti)+460(% Al)


The holding time at the annealing temperature (annealing holding time) is set to be 30 seconds or more. In the case where the annealing holding time is less than 30 seconds, since the dissolution of carbides or austenite transformation does not sufficiently progress, there is an increase in the grain diameter of the retained carbides in a subsequent heat treatment, which results in a deterioration in bendability. Therefore, the annealing holding time is set to be 30 seconds or more or preferably 35 seconds or more. Although there is no particular limitation on the upper limit of the annealing holding time, it is preferable that the annealing holding time be 900 seconds or less to inhibit an increase in austenite grain diameter and to thereby inhibit a deterioration in bendability.


After holding at the annealing temperature has been performed, cooling is performed from a cooling start temperature of 680° C. or higher to a cooling stop temperature of 260° C. or lower in such a manner that cooling is performed at an average cooling rate of 70° C./sec or higher in a temperature range of 680° C. to 260° C. In the case where the upper limit of the temperature range, in which the average cooling rate is specified as described above, is lower than 680° C., it is difficult to obtain a steel sheet having a YR of 0.80 or more due to the formation of ferrite. Therefore, the upper limit of the temperature range, in which the average cooling rate is specified as described above, is set to be 680° C. or higher or preferably 700° C. or higher. In the case where the lower limit of the temperature range, in which the average cooling rate is specified as described above, is higher than 260° C., since tempering does not sufficiently progress, martensite and retained austenite are formed in the final microstructure, which results in a decrease in yield ratio. In addition, since hydrogen in steel is not released into the atmosphere, hydrogen remains in steel, which results in a deterioration in bendability. Therefore, the lower limit of the temperature range, in which the average cooling rate is specified as described above, is set to be 260° C. or lower or preferably 240° C. or lower. In the case where the average cooling rate described above is lower than 70° C./sec, since upper bainite and lower bainite tend to be formed in large amounts, martensite and retained austenite are formed in the final microstructure, which results in a decrease in yield ratio. Therefore, the average cooling rate described above is set to be 70° C./sec or higher, preferably 100° C./sec or higher, or more preferably 500° C./sec or higher. Although there is no particular limitation on the upper limit of the average cooling rate described above, the common upper limit is about 2000° C./sec. Here, there is no particular limitation on the average cooling rate in a temperature range from the annealing temperature to a temperature of 680° C. or the average cooling rate in a temperature range from a temperature of 260° C. to the cooling stop temperature (in the case where the cooling stop temperature is lower than 260° C.)


After reheating treatment is performed as needed (although reheating is necessary in the case where the cooling stop temperature is lower than 150° C., reheating may be performed, even in the case where the cooling stop temperature is 150° C. or higher), holding is performed at a holding temperature range of 150° C. to 260° C. for 20 seconds to 1500 seconds. Carbides distributed inside tempered martensite and/or bainite are carbides which are formed when holding is performed in a low temperature range after quenching has been performed and which function as trap sites for trapping hydrogen, thereby preventing a deterioration in bendability. To achieve good delayed fracturing resistance, it is preferable that holding be performed for 20 seconds to 1500 seconds, after quenching to near room temperature (5° C. to 40° C.) followed by reheating to a temperature of 150° C. to 260° C. or that holding be performed for 20 seconds to 1500 seconds after rapid cooling has been performed to a cooling stop temperature of 150° C. to 260° C. In the case where the holding temperature is lower than 150° C. or the holding time is less than 20 seconds, since carbides are not formed in a sufficient amount inside tempered martensite and/or bainite, there is a decrease in the amount of trap sites for trapping diffusible hydrogen in steel, which results in a deterioration in bendability due to an increase in the amount of diffusible hydrogen in steel. On the other hand, in the case where the holding temperature is higher than 260° C. or the holding time is more than 1500 seconds, since there is an increase in the grain diameter of carbides inside prior γ grains and at prior γ grain boundaries, the average grain diameter of the carbide become more than 50 nm, which conversely results in a deterioration in bendability. Here, it is preferable that the holding time be 120 seconds or more and 1200 seconds or less. Here, there is no particular limitation on the conditions applied for reheating. In addition, in the case where the cooling stop temperature is lower than 150° C., it is necessary to perform reheating.


Electroplating Process


The electroplating process is an electrogalvanizing process.


The electrogalvanizing process is a process in which the steel sheet after the annealing process is cooled to room temperature and subjected to an electrogalvanizing treatment. Although there is no particular limitation on the average cooling rate for cooling from a temperature range of 150° C. to 260° C. at which holding is performed to room temperature (10° C. to 30° C.), it is preferable that cooling be performed at an average cooling rate of 1° C./sec or more to a temperature of 50° C. After cooling has been performed to room temperature, an electrogalvanizing treatment is performed. To inhibit hydrogen from entering steel and to thereby control the amount of diffusible hydrogen in steel to be 0.20 mass ppm or less, the electrogalvanizing time is important. In the case where the electrogalvanizing time is more than 300 seconds, since the period of time for which the steel sheet is dipped in acid is long, there is an increase in the amount of diffusible hydrogen in steel to more than 0.20 mass ppm, which results in a deterioration in bendability. Therefore, the electrogalvanizing time is set to be 300 seconds or less, preferably 250 seconds or less, or more preferably 200 seconds or less. In addition, although there is no particular limitation on the lower limit of the electrogalvanizing time, it is preferable that the electrogalvanizing time be 30 seconds or more. There is no particular limitation on the conditions other than the electrogalvanizing time such as current efficiency as long as it is possible to achieve a sufficient coating weight.


Tempering Process


The tempering process is a process which is performed to release hydrogen from inside steel, in which it is possible to decrease the amount of diffusible hydrogen in steel by holding the steel sheet in a temperature range of 250° C. or lower for a holding time t which satisfies relational expression (1) below, and which can thereby be utilized to further improve bendability. In the case where the tempering temperature is higher than 250° C. or the holding time does not satisfy the relational expression below, since there is an increase in the grain diameter of carbides in bainite or tempered martensite, there may be a deterioration in bendability. Therefore, it is preferable that the holding temperature be 250° C. or lower, preferably 200° C. or lower, or more preferably 150° C. or lower.





(T+273)(log t+4)≤2700  (1)


Here, in relational expression (1), T denotes the holding temperature (° C.) in the tempering process and t denotes the holding time (sec) in the tempering process.


Note that the hot-rolled steel sheet after the hot rolling process may be subjected to a heat treatment to soften the microstructure, and the steel sheet after the electroplating process may be subjected to skin pass rolling to adjust the shape.


According to the manufacturing method according to the present embodiment described above, as a result of controlling the manufacturing conditions before the electrogalvanizing treatment and the electrogalvanizing conditions, since there is a decrease in the amount of diffusible hydrogen in steel, it is possible to obtain a high-yield-ratio high-strength electrogalvanized steel sheet having excellent bendability.


EXAMPLES

The present invention will be specifically described with reference to examples.


1. Manufacturing Steel Sheet for Evaluation


After molten steels having the chemical compositions given in Table 1 and a balance of Fe and inevitable impurities had been prepared by using a vacuum melting furnace, slabbing rolling was performed to obtain rolled slabs having a thickness of 27 mm. The obtained slabs were subjected to hot rolling so as to be made into hot-rolled steel sheets having a thickness of 4.0 mm. Subsequently, samples to be cold-rolled were prepared by grinding the hot-rolled steel sheet to obtain a thickness of 3.2 mm, and the ground samples were subjected to cold rolling with the rolling reduction ratios given in Table 2-1 through Table 2-4 to obtain cold-rolled steel sheets having a thickness of 2.72 mm to 0.96 mm. Here, in Table 2-3, the samples whose rolling reduction ratios for cold rolling are not given were not subjected to cold rolling. Subsequently, the hot-rolled steel sheets and the cold-rolled steel sheets obtained as described above were subjected to annealing and an electrogalvanizing treatment under the conditions given in Table 2-1 through Table 2-4 to obtain electrogalvanized steel sheets. Here, the blank in Table 1 indicates that the corresponding element was not intentionally added, and there may be a case where the content of such an element was 0 mass % or a case where such an element was contained as an inevitable impurity. In addition, some of the samples were subjected to a tempering treatment to release hydrogen. Here, in Table 2-1 through Table 2-4, the blank in the column “Tempering Condition” indicates that the corresponding sample was not subjected to a tempering treatment.


When the above-described steel sheets for evaluation were manufactured, to manufacture the electrogalvanized steel sheets, the electrogalvanizing solution was prepared by adding zinc sulfate heptahydrate to pure water in an amount of 440 g/L and by further adding sulfuric acid to achieve a pH of 2.0 in the case of a pure Zn coating layer. In the case of a Zn—Ni coating layer, the electrogalvanizing solution was prepared by adding zinc sulfate heptahydrate in an amount of 150 g/L and nickel sulfate hexahydrate in an amount of 350 g/L to pure water and by further adding sulfuric acid to achieve a pH of 1.3. In the case of a Zn—Fe coating layer, the electrogalvanizing solution was prepared by adding zinc sulfate heptahydrate to pure water in an amount of 50 g/L and Fe sulfate in an amount of 350 g/L to pure water and by further adding sulfuric acid to achieve a pH of 2.0. In addition, the alloy compositions of the coating layers formed by using the three solutions were respectively 100% Zn, Zn-13% Ni, and Zn-46% Fe as determined by performing ICP analysis. The coating weight of the electrogalvanized coating layer was 25 g/m2 to 50 g/m2 per side. Specifically, the coating weight was 33 g/m2 per side in the case of the 100% Zn coating layer, 27 g/m2 per side in the case of the Zn-13% Ni coating layer, and 27 g/m2 per side in the case of the Zn-46% Fe coating layer. Here, such electrogalvanized coating layers were formed on both sides of the steel sheets.










TABLE 11







Steel
Chemical Composition (mass %)




















Grade
C
Si
Mn
P
S
Al
N
B
Nb
Ti
Cu
Ni
Cr





A
0.30
0.20
1.20
0.007
0.0008
0.05
0.0021


B
0.16
0.20
1.20
0.008
0.0003
0.07
0.0048


C
0.19
0.20
1.20
0.008
0.0005
0.08
0.0021


D
0.39
0.20
1.20
0.018
0.0002
0.02
0.0043


E
0.27
0.02
1.30
0.010
0.0010
0.08
0.0043


F
0.26
1.30
1.30
0.010
0.0010
0.05
0.0058


G
0.28
1.60
1.10
0.007
0.0004
0.04
0.0014


H
0.22
0.03
0.85
0.007
0.0010
0.08
0.0034


I
0.21
0.12
0.95
0.006
0.0007
0.10
0.0046


J
0.28
0.40
1.50
0.025
0.0002
0.09
0.0028


K
0.27
0.38
1.60
0.009
0.0009
0.03
0.0031


L
0.22
0.01
1.30
0.016
0.0004
0.04
0.0028
0.0020


M
0.23
0.07
1.00
0.005
0.0004
0.05
0.0015
0.0032


N
0.22
0.21
1.20
0.006
0.0010
0.07
0.0053
0.0004


O
0.23
0.30
1.21
0.038
0.0006
0.05
0.0040

0.0150


P
0.32
0.09
1.16
0.006
0.0002
0.06
0.0027

0.0700


Q
0.24
0.75
1.16
0.009
0.0002
0.06
0.0051

0.0025


R
0.20
0.11
1.35
0.007
0.0004
0.04
0.0051


0.017


S
0.25
0.10
1.20
0.006
0.0003
0.04
0.0037


0.090


T
0.36
0.04
1.25
0.017
0.0005
0.03
0.0019


 0.0025


U
0.28
0.20
1.25
0.009
0.0003
0.10
0.0060



0.15


V
0.28
0.60
1.10
0.025
0.0010
0.10
0.0020



0.90


W
0.26
0.12
1.16
0.008
0.0010
0.07
0.0020



0.02


X
0.22
0.35
1.20
0.009
0.0001
0.06
0.0043
0.0025

0.015

0.12


Y
0.23
1.10
1.20
0.009
0.0009
0.04
0.0029

0.0130



0.05


Z
0.20
1.30
1.30
0.009
0.0007
0.03
0.0039



0.13

0.03


AA
0.18
0.10
1.30
0.045
0.0010
0.03
0.0033


AB
0.17
0.10
1.25
0.007
0.0007
0.06
0.0027


AC

0.42

1.10
1.20
0.019
0.0002
0.04
0.0021


AD

0.12

1.20
1.20
0.006
0.0002
0.08
0.0055


AE
0.21

2.40

1.05
0.008
0.0010
0.02
0.0028


AF
0.22
0.12

1.90

0.026
0.0006
0.07
0.0024


AG
0.26
0.16

0.05

0.008
0.0007
0.06
0.0010


AH
0.28
0.84
1.20

0.070

0.0004
0.07
0.0058


AI
0.26
0.07
1.32
0.007

0.0080

0.06
0.0028


AJ
0.25
0.11
1.31
0.006
0.0003

0.25

0.0021


AK
0.21
0.05
1.28
0.018
0.0008
0.07

0.0150



AL
0.18
0.01
1.50
0.009
0.0005
0.08
0.0015

0.0040



AM
0.15
0.04
1.40
0.009
0.0002
0.05
0.0057


0.1000



AN
0.14
0.15
1.30
0.006
0.0009
0.07
0.0054



0.140















Steel
Chemical Composition (mass %)
Ac3




















Grade
Mo
V
Zr
W
Ca
Ce
La
Mg
Sb
Sn
Temperature







A










795



B










833



C










831



D










766



E










802



F










849



G










858



H










827



I










838



J










818



K










786



L










794



M










809



N










819



O










813



P










793



Q










838



R










808



S










831



T










769



U










815



V










823



W










808



X










825



Y
0.05









848



Z

0.012








853



AA


0.009
0.01
0.0008
0.0009
0.0006
0.0005


805



AB








0.007
0.004
821



AC










808



AD










893



AE










904



AF










795



AG










839



AH










836



AI










797



AJ










889



AK










813



AL










815



AM










816



AN










891







Underlined portions indicate items out of the range according to aspects of the present invention.

















TABLE 2-1









Hot Rolling
Cold














Average
Average

Rolling
Annealing Condition




















Slab

Finishing
Cooling
Cooling

Rolling

Annealing
Cooling




Heating
Rolling
Delivery
Rate to
Rate to
Coiling
Reduction
Annealing
Holding
Start



Steel
Temperature
Time*1
Temperature
700° C. *2
650° C. *3
Temperature
Ratio
Temperature
Time
Temperature


No.
Grade
° C.
sec
° C.
° C./s
° C./s
° C.
%
° C.
sec
° C.





1
A
1250
74
880
232
11
550
56
904
35
831


2

1250
225
880
245
13
550
56
867
35
801


3

1250
54
880
225
12
550
56
891
35
709


4

1250
85
880
246
14
550
56
860
35
845


5

1250
66
880
248
20
550
56
873
35
748


6

1250
90
880
247
18
550
56
887
35
697


7

1250
67
880
239
13
550
56
910
35
891


8

1250
66
880
251
11
550
56
864
35
719


9
B

1180

71
880
235
13
550
56
887
35
717


10

1220
74
880
237
15
550
56
902
35
900


11

1235
69
880
241
17
550
56
896
35
887


12

1250
71
880
242
14
550
56
890
35
761


13
C
1250
93

830

239
18
550
56
863
35
830


14

1250
83
850
242
15
550
56
904
35
858


15

1250
55
880
250
16
550
56
894
35
894


16

1250
54
940
247
14
550
56
862
35
767


17

1250
140
960
250
12
550
56
894
35
815


18
D
1250
60
880
100
11
550
56
872
35
827


19

1250
88
880
 40
18
550
56
880
35
819


20

1250
51
880
20
14
550
56
884
35
779


21

1250
51
880
228
1
550
56
898
35
803


22
E
1250
160
880
229
15
550
56
867
35
731


23

1250
59
880
231
17
550
56
883
35
860


24

1250
93
880
234
14
550
56
899
35
714


26

1250
58
880
229
13
550
56
880
35
730


27

1250
230
880
230
12
550
56
878
35
702


28

1250
55
880
231
16
550
56
909
35
820


29

1250
62
880
230
15
550
56
890
35
740


30

1250
56
880
234
18
550
56
909
35
890


31

1250
63
880
238
17
550
56
873
35
869


32

1250
99
880
237
14
550
56
880
35
750















Annealing Condition

















Average
Cooling

Electrogalvanizing Condition
Tempering Condition




















Cooling
Stop
Holding
Holding
Kind of
Electrogalvanizing
Holding
Holding





Rate*4
Temperature
Temperature
Time
Coating
Time
Temperature
Time



No.
° C./s
° C.
° C.
sec
Layer
sec
° C.
sec







1
1807
25
200
700
Zn—Ni
 50


Example



2
1615
25
200
900
Zn—Ni
100


Example



3
1816
50
200
800
Zn—Ni
150


Example



4
1594

300

200
700
Zn—Ni
200


Comparative Example



5
1525
25
200
600
Zn—Ni
230
250
10
Example



6
1618
25
200
800
Zn—Ni
280
80
3600
Example



7
1772
25
200
800
Zn—Ni
300


Example



8
1782
25
200
800
Zn—Ni

340



Comparative Example



9
1524
50
200
900
Zn—Ni
160


Comparative Example



10
1938
50
200
600
Zn—Ni
110


Example



11
1669
100 
200
800
Zn—Ni
110
200
30
Example



12
1788
100 
200
800
Zn—Ni
180
150
180
Example



13
1741
25
200
800
Zn—Ni
130


Comparative Example



14
1535
25
200
700
Zn—Ni
130


Example



15
1994
25
200
900
Zn—Ni
130


Example



16
1657
50
200
600
Zn—Ni
110
100
1200
Example



17
1932
50
200
800
Zn—Ni
120
80
180
Example



18
1637
25
200
600
Zn—Ni
190


Example



19
1585
25
200
800
Zn—Ni
200


Example



20
1909
100 
200
800
Zn—Ni
170


Comparative Example



21
1685
100 
200
800
Zn—Ni
100


Comparative Example



22
1880

300

200
900
Zn—Ni
110


Comparative Example



23
1648
250 
250
900
Zn—Ni
170


Example



24
1810
200 
250
900
Zn—Ni
100


Example



26
2100
200 
150
900
Zn—Ni
180
100
120
Example



27
1721
150 
200
900
Zn—Ni
130


Example



28
1765
150 
150
900
Zn—Ni
190


Example



29
2050
150 

100

900
Zn—Ni
170


Comparative Example



30
1657
100 
200
900
Zn—Ni
190


Example



31
1789
100 
150
900
Zn—Ni
150


Example



32
1950
100 
100
900
Zn—Ni
180


Comparative Example







*1Rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature



*2 Average cooling rate from the finishing delivery temperature to a temperature of 700° C.



*3 Average cooling rate in a temperature range of 700° C. (primary cooling stop temperature) to 650° C.



*4Average cooling rate in a temperature range of 680° C. to 260° C.



Underlined portions indicate items out of the range according to aspects of the present invention.

















TABLE 2-2









Hot Rolling
Cold














Average
Average

Rolling
Annealing Condition




















Slab

Finishing
Cooling
Cooling

Rolling

Annealing
Cooling




Heating
Rolling
Delivery
Rate to
Rate to
Coiling
Reduction
Annealing
Holding
start



Steel
Temperature
Time*1
Temperature
700° C. *2
650° C *3
Temperature
Ratio
Temperature
Time
Temperature


No.
Grade
° C.
sec
° C.
° C./s
° C./s
° C.
%
° C.
sec
° C.





33
F
1250
100
880
241
11

700

56
894
35
806


34

1250
51
880
235
12
630
56
882
35
835


35

1250
66
880
236
13
550
56
905
35
830


36
G
1250
55
880
238
15
550
15
906
35
807


37

1250
78
880
244
16
550
56
885
35
763


38

1250
53
880
241
18
550
70
882
35
758


39
H
1250
52
880
237
19
550
56

815

35
733


40

1250
82
880
229
14
550
56
850
35
772


41

1250
57
880
235
15
550
56
870
35
829


42
I
1250
85
880
234
22
550
56
870
35
809


43

1250
170
880
228
10
550
56
900
35
741


44

1250
51
880
229
12
550
56
930
35
680


45
J
1250
84
880
230
15
550
56
890

28

730


46

1250
89
880
247
17
550
56
880
32
799


47

1250
66
880
246
16
550
56
889
35
767


48
K
1250
95
880
241
14
550
56
879
35
755


49

1250
69
880
300
13
550
56
886
50
809


50

1250
86
880
220
12
550
56
870
70
849


51
L
1250
66
880
150
15
550
56
863
35

650



52

1250
64
880
170
18
550
56
861
35
700


53

1250
87
880
247
10
550
56
903
35
755


54
M
1250
56
880
242
11
550
56
891
35
702


55

1250
53
880
245
4
550
56
875
35
727


56

1250
62
880
239
15
550
56
878
35

635



57
N
1250
56
880
234
14
550
56
876
35
757


58

1250
55
880
235
15
550
56
895
35
824


59

1250
85
880
237
16
550
56
884
35
754














Annealing Condition
















Average
Cooling

Electrogalvanizing Condition
Tempering Condition




















Cooling
Stop
Holding
Holding
Kind of
Electrogalvanizing
Holding
Holding





Rate*4
Temperature
Temperature
Time
Coating
Time
Temperature
Time



No.
° C./s
° C.
° C.
sec
Layer
sec
° C.
sec







33
1977
25
200
700
Zn—Ni
130


Comparative Example



34
1809
25
200
700
Zn—Ni
130
150
20
Example



35
1503
25
200
800
Zn—Ni
120
150
150
Example



36
1592
25
200
700
Zn—Ni
110


Example



37
1653
25
200
600
Zn—Ni

380



Comparative Example



38
1513
25
200
600
Zn—Ni
180


Example



39
1914
50
200
700
Zn—Ni
120


Comparative Example



40
1873
50
200
800
Zn—Ni
120


Example



41
1807
50
200
900
Zn—Ni
170


Example



42
1596
50

100

800
Zn—Ni
200


Comparative Example



43
1810
25
200
900
Zn—Ni
100


Example



44
1961
25
200
600
Zn
160


Example



45
1745
100
200
600
Zn
120


Comparative Example



46
1688
100
200
900
Zn
120


Example



47
1913
100
200
900
Zn

370



Comparative Example



48
1556
100
200
700
Zn
120


Example



49
1519
100
200
700
Zn
100


Example



50
1545
100
200
700
Zn
190


Example



51
1968
100
200
900
Zn
100


Comparative Example



52
1659
100
200
600
Zn
120


Example



53
1683
100
200
800
Zn
160


Example



54
1709
50
200
900
Zn
170


Example



55
1726
50
200
700
Zn
120


Example



56
1888
50
200
800
Zn
150


Comparative Example



57
1500
50
200
700
Zn
190


Example



58
 800
25
200
700
Zn
130


Example



59
50
25
200
600
Zn
170


Comparative Example







*1Rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature



*2 Average cooling rate from the finishing delivery temperature to a temperature of 700° C.



*3 Average cooling rate in a temperature range of 700° C. (primary cooling stop temperature) to 650° C.



*4Average cooling rate in a temperature range of 680° C. to 260° C.



Underlined portions indicate items out of the range according to aspects of the present invention.

















TABLE 2-3









Hot Rolling
Cold














Average
Average

Rolling
Annealing Condition




















Slab

Finishing
Cooling
Cooling

Rolling

Annealing
Cooling




Heating
Rolling
Delivery
Rate to
Rate to
Coiling
Reduction
Annealing
Holding
start



Steel
Temperature
Time*1
Temperature
700° C. *2
650° C. *3
Temperature
Ratio
Temperature
Time
Temperature


No.
Grade
° C.
sec
° C.
° C./s
° C./s
° C.
%
° C.
sec
° C.





60
O
1250
80
880
180
11
550
56
881
35
694


61

1250
80
880
120
10
550
56
877
35
877


62

1250
62
880
60
17
550
56
876
35
793


63
P
1250
71
880
50
15
550
56
863
35
753


64

1250
70
880
237
18
550
56
877
35
848


65

1250
97
880
235
14
550
56
871
35
766


66
Q
1250
94
880
233
15
550
56
872
35
845


67

1250
65
880
238
11
550
56
871
35
788


68

1250
97
880
241
12
550
56
892
35
783


69
R
1250
91
880
240
15
550
56
909
35
882


70

1250
89
880
241
13
550
56
881
35
875


71

1250
78
880
240
14
550
56
860
35
684


72
S
1250
94
880
246
16
550
56
877
35
705


73

1250
87
880
238
11
550
56
898
35
755


74

1250
64
880
237
12
550
56
894
35
702


75
T

1150

74
880
237
14
550
56
898
35
880


76

1250
83
880
235
17
550
56
869
35
743


77

1250
75
880
239
18

700

56
899
35
686


78
U
1250
72

830

242
15
550
56
908
35
896


79

1250
60
880
243
19
550
56
899
35
718


80

1250
63
880
400
15
550
56

800

35
754


81
V
1250
73
880
140
14
550

886
35
700


82

1250
60
880
45
12
550

897
35
694


83

1250
69
880
160
15
550

894
35
803


84
W
1250
69
880
1148
16
550
56
890
35
838


85

1250
88
880
500
12
550
56
889
35
753


86

1250
92
880
170
11
550
56
893
35
826


87
X
1250
73
880
45
10
550
56
876
35
700


88

1250
51
880
110
15
550
56
898
35
857


89

1250
60
880
70
17
550
56
908
35
740














Annealing Condition
















Average
Cooling

Electrogalvanizing Condition
Tempering Condition




















Cooling
Stop
Holding
Holding
Kind of
Electrogalvanizing
Holding
Holding





Rate*4
Temperature
Temperature
Time
Coating
Time
Temperature
Time



No.
° C./s
° C.
° C.
sec
Layer
sec
° C.
sec







60
80
25
200
700
Zn
160


Example



61
800
25
200
600
Zn
140


Example



62
1500
25
200
700
Zn
190


Example



63
1786
25
200
10
Zn
140


Comparative Example



64
1756
25
200
 80
Zn
160


Example



65
1956
25
200
300
Zn
150


Example



66
1824
25
200
700
Zn
200


Example



67
1787
25
200
1300 
Zn
140


Example



68
1676
25
200

1600

Zn
180


Comparative Example



69
1990
25
200
800
Zn
150


Example



70
1732
25
200
700
Zn
240


Example



71
1809
25
200
600
Zn

350



Comparative Example



72
1634
25
200
900
Zn
180


Example



73
1737
25

300

900
Zn
140


Comparative Example



74
1851
25
200
900
Zn

360



Comparative Example



75
1804
25
200
600
Zn—Fe
200


Comparative Example



76
1666
25
200
700
Zn—Fe
130


Example



77
1965
25
200
700
Zn—Fe
140


Comparative Example



78
1999
25
200
700
Zn—Fe
160


Comparative Example



79
1823
25
200
900
Zn—Fe
100


Example



80
1574
25
200
700
Zn—Fe
110


Comparative Example



81
1621
25
200
600
Zn—Fe
100


Example



82
1864
25
200
800
Zn—Fe
130


Example



83
1781
25
200
800
Zn—Fe
140


Example



84
1909
25
150
700
Zn—Fe
160


Example



85
1651
25
170
10
Zn—Fe
100


Comparative Example



86
1969
25
190
900
Zn—Fe
180


Example



87
1526
25
210

1600

Zn—Fe
130


Comparative Example



88
1594
25
230
900
Zn—Fe
160


Example



89
1915
25
250
700
Zn—Fe
110


Example







*1Rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature



*2 Average cooling rate from the finishing delivery temperature to a temperature of 700° C.



*3 Average cooling rate in a temperature range of 700° C. (primary cooling stop temperature) to 650° C.



*4Average cooling rate in a temperature range of 680° C. to 260° C.



Underlined portions indicate items out of the range according to aspects of the present invention.

















TABLE 2-4









Hot Rolling
Cold














Average
Average

Rolling
Annealing Condition




















Slab

Finishing
Cooling
Cooling

Rolling

Annealing
Cooling




Heating
Rolling
Delivery
Rate to
Rate to
Coiling
Reduction
Annealing
Holding
Start



Steel
Temperature
Time*1
Temperature
700° C. *2
650° C. *3
Temperature
Ratio
Temperature
Time
Temperature


No.
Grade
° C.
sec
° C.
° C./s
° C./s
° C.
%
° C.
sec
° C.





90
Y
1250
220
880
 50
18
550
56
908
35
740


91

1250
90
880
1187 
16
550
56
908
35
740


92

1250
105
880
130
15
550
56
908
35
740


93

1250
68
880
 60
18
550
56
886
35
881


94

1250
75
880
15
15
550
56
889
35
705


95

1250
50
880
120
15
550
56
883
35
853


96
Z
1250
80
880
237
60
550
56
894
35
715


97

1250
77
880
234
 4
550
56
904

28

697


98

1250
81
880
241
28
550
56
905
85
804


99
AA
1250
91
880
246
31
550
56
898
35
831


100

1250
66
880
242
 8
550
56
902
35
801


101

1250
57
880
236
14
550
56
906
35
726


102
AB
1250
99
880
235
 8
550
56
910
35
807


103

1250
100
880
233
 4
550
56
883
35
688


104

1250
51
880
232
1
550
56
875
35
764


105

AC

1250
99
880
229
15
550
56
873
35
829


106

AD

1250
50
880
230
16
550
56
904
35
680


107

AE

1250
60
880
227
14
550
56
912
35
792


108

AF

1250
62
880
230
12
550
56
894
35
755


109

AG

1250
59
880
229
11
550
56
890
35
719


110

AH

1250
66
880
225
10
550
56
870
35
794


111

AI

1250
54
880
234
15
550
56
869
35
733


112

AJ

1250
95
880
236
18
550
56
900
35
682


113

AK

1250
67
880
228
17
550
56
886
35
870


114

AL

1250
64
880
229
15
550
56
877
35
697


115

AM

1250
57
880
230
16
550
56
904
35
782


116

AN

1250
53
880
230
15
550
56
891
35
820















Annealing Condition

















Average
Cooling

Electrogalvanizing Condition
Tempering Condition




















Cooling
Stop
Holding
Holding
Kind of
Electrogalvanizing
Holding
Holding





Rate*4
Temperature
Temperature
Time
Coating
Time
Temperature
Time



No.
° C./s
° C.
° C.
sec
Layer
sec
° C.
sec







90
1915
25
250
700
Zn—Fe
110


Example



91
1915
25
250
700
Zn—Fe
110


Example



92
1915
25
250
700
Zn—Fe
110


Example



93
 100
25
200
600
Zn—Fe
110


Example



94
 300
25
200
600
Zn—Fe
100


Comparative Example



95
 700
25
200
600
Zn—Fe
140


Example



96
1000
50
200
900
Zn—Fe
150


Example



97
1890
50
200
700
Zn—Fe
180


Comparative Example



98
1586
50
200
600
Zn—Fe
190


Example



99
1706
50

270

800
Zn—Fe
110


Comparative Example



100
1600
50
250
800
Zn—Fe
170


Example



101
1831
50
230
800
Zn—Fe
190


Example



102
60
50
200
800
Zn—Fe
190


Comparative Example



103
 450
50
200
800
Zn—Fe
120


Example



104
1730
50
200
600
Zn—Fe
120


Comparative Example



105
1526
50
200
600
Zn—Ni
110


Comparative Example



106
1799
50
200
600
Zn—Ni
150


Comparative Example



107
1987
50
200
800
Zn—Ni
200


Comparative Example



108
1692
50
200
900
Zn—Ni
130


Comparative Example



109
1654
50
200
600
Zn—Ni
120


Comparative Example



110
1743
50
200
800
Zn—Ni
140


Comparative Example



111
1671
50
200
700
Zn—Ni
130


Comparative Example



112
1564
50
200
900
Zn—Ni
130


Comparative Example



113
1898
50
200
700
Zn—Ni
160


Comparative Example



114
1922
50
200
600
Zn—Ni
160


Comparative Example



115
1539
50
200
800
Zn—Ni
190


Comparative Example



116
1843
50
200
700
Zn—Ni
130


Comparative Example







*1Rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature



*2 Average cooling rate from the finishing delivery temperature to a temperature of 700° C.



*3 Average cooling rate in a temperature range of 700° C. (primary cooling stop temperature) to 650° C.



*4Average cooling rate in a temperature range of 680° C. to 260° C.



Underlined portions indicate items out of the range according to aspects of the present invention.






2. Evaluation Method


The phase fractions, tensile properties such as tensile strength, and bendability of the electrogalvanized steel sheets obtained under various manufacturing conditions were observed by performing respectively steel microstructure analysis, a tensile test, and a bending test. Each of the evaluation methods is as follows.


(Total Area Fraction of One or Both of Bainite Containing Carbides Having an Average Grain Diameter of 50 Nm or Less and Tempered Martensite Containing Carbides Having an Average Grain Diameter of 50 nm or Less)


After a test piece in the rolling direction or in a direction perpendicular to the rolling direction had been taken from each of the electrogalvanized steel sheet, mirror polishing was performed on the L-cross-section in the thickness direction parallel to the rolling direction of the test piece, etching was performed on the polished L-cross-section in a Nital solution to reveal the microstructure, observation with a scanning electron microscope was performed on the etched L-cross-section, and the area fractions of tempered martensite (denoted by TM in Table 3-1 through Table 3-4) and bainite (denoted by B in Table 3-1 through Table 3-4) were investigated by using a point-counting method in such a manner that a grid having a number of grid points of 16×15 at intervals of 4.8 μm was placed on a region having an actual size of 82 μm×57 μm in a SEM image at a magnification of 1500 times and the number of grid points found on each of the phases was counted. The total area fraction of one or both of bainite containing carbides having an average grain diameter of 50 nm or less and tempered martensite containing carbides having an average grain diameter of 50 nm or less in the whole microstructure was defined as the average value of the area fractions in the SEM images obtained by continuously performing observation with a SEM at a magnification of 1500 times across the whole thickness. The total area fraction of one or both of bainite containing carbides having an average grain diameter of 50 nm or less and tempered martensite containing carbides having an average grain diameter of 50 nm or less in a region from the surface of the base steel sheet to a position located at ⅛ of the thickness of the base steel sheet was defined as the average value of the area fractions in the SEM images obtained by continuously performing observation with a SEM at a magnification of 1500 times across the whole region from the surface of the base steel sheet to a position located at ⅛ of the thickness of the base steel sheet. Tempered martensite and bainite are identified as white microstructures in which blocks and packets are observed inside prior austenite grains and in which carbides having a small grain diameter are precipitated. In addition, since there may be a case where the carbides are difficult to observe depending on the plane orientation of a block grain or etching quality, it is necessary to sufficiently perform etching for confirmation in such a case. Here, the average grain diameter of carbides contained in tempered martensite and bainite was calculated by using the following method.


(Average Grain Diameter of Carbides Inside Tempered Martensite and Bainite)


After a test piece in the rolling direction or in a direction perpendicular to the rolling direction had been taken from each of the electrogalvanized steel sheet, mirror polishing was performed on the L-cross-section in the thickness direction parallel to the rolling direction of the test piece, etching was performed on the polished L-cross-section in a Nital solution to reveal the microstructure, observation with a scanning electron microscope was continuously performed across the whole region from the surface of the base steel sheet to a position located at ⅛ of the thickness of the base steel sheet, the number of carbides inside prior austenite grains containing tempered martensite and bainite was calculated from one of the SEM images at a magnification of 5000 times, and the total area of carbides inside one crystal grain was calculated by binarizing the microstructure. From the number of carbides and the total area of carbides, the area per one carbide grain was calculated, and the average grain diameter of carbides in the region from the surface of the base steel sheet to a position located at ⅛ of the thickness of the base steel sheet was calculated. The average grain diameter of carbides in the whole microstructure was determined by using the same calculating method as that for calculating the average grain diameter of carbides in the region from the surface of the base steel sheet to a position located at ⅛ of the thickness of the base steel sheet after having observed a position located at ¼ of the thickness of the base steel sheet with a scanning electron microscope. Here, the microstructure at a position located at ¼ of the thickness of the steel sheet is regarded as representing the average microstructure of the whole microstructure.


(Sum of Perimeters of Carbides Having an Average Grain Diameter of 0.1 μm or More and Inclusions)


After a test piece in the rolling direction or in a direction perpendicular to the rolling direction had been taken from each of the electrogalvanized steel sheet, mirror polishing was performed on the L-cross-section in the thickness direction parallel to the rolling direction of the test piece, observation with an optical microscope was performed on the polished L-section without performing etching to reveal the microstructure, and inclusions were identified as black regions in an optical microscope photograph at a magnification of 400 times. In addition, after a test piece in the rolling direction or in a direction perpendicular to the rolling direction was taken from each of the electrogalvanized steel sheet, mirror polishing was performed on the L-cross-section in the thickness direction parallel to the rolling direction of the test piece, etching was performed on the polished L-cross-section in a Nital solution to reveal the microstructure, observation with a scanning electron microscope was performed on the etched L-cross-section, and carbides having a large average grain diameter of 0.1 μm or more were observed in a SEM image at a magnification of 5000 times. The long side length and short side length of the inclusions or the carbides were determined, and the average value of the side lengths was defined as the average grain diameter. In addition, the perimeter of each of the carbides having an average grain diameter of 0.1 μm or more and the inclusions was calculated by multiplying the average grain diameter by the circular constant π, and the sum of the calculated perimeters was defined as the sum of the perimeters of the carbides having an average grain diameter of 0.1 μm or more and the inclusions.


(Tensile Test)


After a JIS No. 5 test piece in the rolling direction having a gage length of 50 mm, a gage width of 25 mm, and a thickness of 1.4 mm had been taken from each of the electrogalvanized steel sheet, a tensile test was performed with a cross head speed of 10 mm/min to determine the tensile strength (denoted by TS in Table 3-1 through Table 3-4), the yield strength (denoted by YS in Table 3-1 through Table 3-4), and the elongation (denoted by El in Table 3-1 through Table 3-4). In addition, the yield ratio (denoted by YR in Table 3-1 through Table 3-4) was calculated as YS/TS.


(Bending Test)


After a strip-shaped test piece having a long side length of 100 mm and a short side length of 30 mm in a direction perpendicular to the rolling direction had been taken for each of the electrogalvanized steel sheet by performing shearing on the long side having a length of 100 mm with the sheared end surface being left as sheared (without performing machining to remove burrs), bending work was performed so that the burrs were on the outer side of bending. Bending work was performed so that the bending angle on the inner side of the peak-like bending position was 90 degrees (V-bend). The end bending radius was defined as R, the thickness of the steel sheet was defined as t, and evaluation was performed on the basis of R/t.


(Hydrogen Analysis Method)


A strip-shaped test piece having a long side length of 30 mm and a short side length of 5 mm was taken from the central portion in the width direction of each of the electrogalvanized steel sheet. After the coating layer formed on the surface of the strip-shaped test piece had been completely removed by using a handy router, hydrogen analysis was performed by using a thermal desorption analytical device at a heating rate of 200° C./hr. The hydrogen analysis was performed immediately after the strip-shaped test piece had been taken and the coating layer had been removed. The amount of accumulated hydrogen which was released in a temperature range from the heating start temperature (25° C.) to a temperature of 200° C. was determined, and the determined value was defined as the amount of diffusible hydrogen in steel.


3. Evaluation Result


The evaluation results obtained as described above are given in Table 3-1 through Table 3-4.













TABLE 3-1









Microstructure
















Total Perimeter






TM + B
of Inclusion and
Diffusible



in Surface
Carbide Having
Hydrogen
Mechanical Property




















Steel
TM + B*1
Layer *2
Large Grain Diameter*3
in Steel
YS
TS
El





No.
Grade
%
%
μm/mm2
mass ppm
MPa
MPa
%
YR
R/t





















1
A
94
87
3.5
0.12
1512
1810
6.9
0.84
4.1
Example


2

95
88
65
0.04
1452
1720
7.4
0.84
3.8
Example


3

95
88
5
0.02
1537
1820
6.6
0.84
3.5
Example


4


86

90
30

0.21

1376
1800
7.2

0.76


4.6

Comparative Example


5

92
87
0
0.06
1480
1810
6.8
0.82
3.5
Example


6

98
92
15
0.03
1551
1780
6.8
0.87
3.6
Example


7

95
80
35
0.17
1512
1790
6.9
0.84
4.2
Example


8

100 
82
20

0.29

1609
1810
6.7
0.89

4.8

Comparative Example


9
B

85

88
60
0.03
1324
1520
8.4
0.87

3.8

Comparative Example


10

99
83
40
0.14
1364
1550
8.1
0.88
3.6
Example


11

96
84
5
0.05
1306
1530
8.5
0.85
3.2
Example


12

93
89
5
0.04
1232
1490
8.1
0.83
2.7
Example


13
C

84

87
65
0.15
1320
1580
7.7
0.84

4.1

Comparative Example


14

96
85
30
0.11
1357
1590
8.1
0.85
3.5
Example


15

100 
87
15
0.03
1431
1610
8.1
0.89
3.6
Example


16

90
83
10
0.09
1248
1560
8.1
0.80
3.6
Example


17

98
91
10
0.04
1368
1570
8.2
0.87
3.5
Example


18
D
93
93
70
0.01
1637
1980
6.2
0.83
4.3
Example


19

92
81
35
0.05
1733
2010
6.5
0.86
4.3
Example


20

99

77

15
0.08
1760
2000
6.3
0.88

4.8

Comparative Example


21

93

71

20
0.07
1629
1970
6.6
0.83

4.8

Comparative Example


22
E

87

83
15

0.30

1369
1770
7.1

0.77


4.7

Comparative Example


23

91
81
30
0.16
1448
1790
6.7
0.81
4.3
Example


24

100 
82
40
0.11
1618
1820
6.8
0.89
4.1
Example


26

90
88
30
0.02
1424
1780
7.1
0.80
3.6
Example


27

100 
89
75
0.13
1609
1810
7.0
0.89
4.1
Example


28

94
90
30
0.14
1496
1790
7.2
0.84
4.0
Example


29

98
86
15

0.26

1568
1800
7.2
0.87

4.6

Comparative Example


30

91
87
30
0.12
1432
1770
6.9
0.81
3.9
Example


31

95
84
20
0.18
1503
1780
7.2
0.84
4.2
Example


32

98
84
5

0.26

1559
1790
7.0
0.87

4.7

Comparative Example





*1The total area fraction of one or both of B containing carbides having an average grain diameter of 50 nm or less and TM containing carbides having an average grain diameter of 50 nm or less in the whole microstructure


*2 The total area fraction of one or both of B containing carbides having an average grain diameter of 50 nm or less and TM containing carbides having an average grain diameter of 50 nm or less in a region (surface layer) from the surface of the base steel sheet to a position located at ⅛ of the thickness of the base steel sheet


*3The sum of perimeters of carbides having an average grain diameter of 0.1 μm or more and inclusions


Underlined portions indicate items out of the range according to aspects of the present invention.

















TABLE 3-2









Microstructure
















Total Perimeter






TM+B
of Inclusion and
Diffusible



in Surface
Carbide Having
Hydrogen
Mechanical Property




















Steel
TM + B*1
Layer *2
Large Grain Diameter*3
in Steel
YS
TS
El





No.
Grade
%
%
μm/mm2
mass ppm
MPa
MPa
%
YR
R/t





















33
F

88

84
10
0.02
1291
1650
7.7

0.78


4.3

Comparative Example


34

90
84
5
0.03
1344
1680
7.5
0.80
3.5
Example


35

93
83
40
0.01
1430
1730
7.2
0.83
3.8
Example


36
G
92
84
10
0.08
1423
1740
7.2
0.82
3.7
Example


37

96
86
20

0.28

1493
1750
7.0
0.85

4.6

Comparative Example


38

99
81
10
0.14
1549
1760
7.2
0.88
4.2
Example


39
H

86

84
15
0.04
1170
1530
7.9

0.76

3.2
Comparative Example


40

91
85
25
0.08
1246
1540
8.4
0.81
3.3
Example


41

94
85
40
0.10
1287
1540
7.9
0.84
3.5
Example


42
I
98
96
40

0.25

1359
1560
8.3
0.87

4.1

Comparative Example


43

93
86
15
0.06
1273
1540
8.1
0.83
3.6
Example


44

95
86
40
0.03
1309
1550
7.7
0.84
3.5
Example


45
J

80


78

60
0.16
1671
1880
6.4
0.89

4.7

Comparative Example


46

91
82
5
0.10
1464
1810
6.9
0.81
3.8
Example


47

94
83
40

0.27

1521
1820
6.6
0.84

4.8

Comparative Example


48
K
91
83
30
0.17
1488
1840
7.1
0.81
4.3
Example


49

100 
84
30
0.13
1671
1880
6.6
0.89
4.2
Example


50

98
82
5
0.12
1629
1870
7.0
0.87
4.1
Example


51
L

83

81
30
0.18
1158
1570
8.1

0.74

3.7
Comparative Example


52

92
88
10
0.16
1325
1620
7.5
0.82
3.5
Example


53

97
93
10
0.12
1440
1670
7.5
0.86
3.4
Example


54
M
91
89
30
0.14
1278
1580
8.2
0.81
3.7
Example


55

95
82
15
0.02
1351
1600
8.1
0.84
3.4
Example


56


82

80
10
0.15
1086
1490
8.7

0.73

3.1
Comparative Example


57
N
93
91
25
0.14
1356
1640
7.4
0.83
3.6
Example


58

90
88
35
0.13
1296
1620
7.7
0.80
3.6
Example


59


80


76

40
0.13
1074
1510
8.2

0.71

3.3
Comparative Example





*1The total area fraction of one or both of B containing carbides having an average grain diameter of 50 nm or less and TM containing carbides having an average grain diameter of 50 nm or less in the whole microstructure


*2 The total area fraction of one or both of B containing carbides having an average grain diameter of 50 nm or less and TM containing carbides having an average grain diameter of 50 nm or less in a region (surface layer) from the surface of the base steel sheet to a position located at ⅛ of the thickness of the base steel sheet


*3The sum of perimeters of carbides having an average grain diameter of 0.1 μm or more and inclusions


Underlined portions indicate items out of the range according to aspects of the present invention.

















TABLE 3-3









Microstructure
















Total Perimeter






TM + B
of Inclusion and
Diffusible



in Surface
Carbide Having
Hydrogen
Mechanical Property




















Steel
TM + B*1
Layer *2
Large Grain Diameter*3
in Steel
YS
TS
El





No.
Grade
%
%
μm/mm2
mass ppm
MPa
MPa
%
YR
R/t





















60
O
90
85
40
0.12
1288
1610
7.8
0.80
3.7
Example


61

94
91
20
0.01
1379
1650
7.3
0.84
3.7
Example


62

98
82
5
0.08
1455
1670
7.2
0.87
3.8
Example


63
P
95
81
5

0.24

1537
1820
6.9
0.84

4.7

Comparative Example


64

93
82
0
0.18
1496
1810
7.0
0.83
4.4
Example


65

96
89
30
0.14
1570
1840
6.6
0.85
4.2
Example


66
Q
91
82
10
0.02
1335
1650
7.4
0.81
3.3
Example


67

90
87
15
0.12
1312
1640
7.7
0.80
3.6
Example


68


86

85
70
0.02
1449
1680
7.6
0.86

4.2

Comparative Example


69
R
96
88
5
0.01
1408
1650
7.4
0.85
3.1
Example


70

97
91
10
0.09
1431
1660
7.5
0.86
3.5
Example


71

94
88
25

0.22

1370
1640
7.6
0.84

4.2

Comparative Example


72
S
94
86
40
0.11
1420
1700
7.2
0.84
3.9
Example


73


86

85
65
0.17
1327
1640
7.7
0.81

4.2

Comparative Example


74

90
86
35

0.27

1304
1630
8.0
0.80

4.3

Comparative Example


75
T

88

84
70
0.14
1613
1930
6.6
0.84

4.6

Comparative Example


76

100 
96
25
0.09
1742
1960
6.3
0.89
4.0
Example


77


87

85
25
0.11
1415
1830
6.6

0.77


4.5

Comparative Example


78
U

88


79

65
0.12
1591
1790
7.1
0.89

4.7

Comparative Example


79

92
86
10
0.07
1415
1730
7.3
0.82
3.7
Example


80


82

81
25
0.04
1203
1650
7.4

0.73

3.6
Comparative Example


81
V
95
90
35
0.13
1461
1730
7.2
0.84
3.9
Example


82

96
82
25
0.13
1485
1740
7.1
0.85
3.9
Example


83

97
87
35
0.16
1509
1750
7.4
0.86
4.1
Example


84
W
97
91
30
0.14
1474
1710
7.1
0.86
4.0
Example


85

96
91
40

0.25

1451
1700
7.1
0.85

4.7

Comparative Example


86

94
89
35
0.15
1404
1680
7.4
0.84
3.7
Example


87
X

87

82
60
0.14
1382
1620
7.7
0.85

4.3

Comparative Example


88

94
89
5
0.07
1362
1630
8.0
0.84
3.3
Example


89

94
82
35
0.13
1362
1630
7.6
0.84
3.7
Example





*1The total area fraction of one or both of B containing carbides having an average grain diameter of 50 nm or less and TM containing carbides having an average grain diameter of 50 nm or less in the whole microstructure


*2 The total area fraction of one or both of B containing carbides having an average grain diameter of 50 nm or less and TM containing carbides having an average grain diameter of 50 nm or less in a region (surface layer) from the surface of the base steel sheet to a position located at ⅛ of the thickness of the base steel sheet


*3The sum of perimeters of carbides having an average grain diameter of 0.1 μm or more and inclusions


Underlined portions indicate items out of the range according to aspects of the present invention.

















TABLE 3-4









Microstructure
















Total Perimeter






TM + B
of Inclusion and
Diffusible



in Surface
Carbide Having
Hydrogen
Mechanical Property




















Steel
TM + B*1
Layer *2
Large Grain Diameter*3
in Steel
YS
TS
El





No.
Grade
%
%
μm/mm2
mass ppm
MPa
MPa
%
YR
R/t





















90
Y
99
85
70
0.03
1478
1680
7.3
0.88
3.4
Example


91

95
90
15
0.03
1402
1660
7.6
0.84
3.3
Example


92

98
91
55
0.06
1455
1670
7.7
0.87
3.5
Example


93

91
82
10
0.06
1310
1620
7.8
0.81
3.2
Example


94

94

78

25
0.08
1362
1630
7.6
0.84

4.4

Comparative Example


95

96
93
35
0.07
1425
1670
7.3
0.85
3.6
Example


96
Z
93
82
65
0.12
1454
1620
7.8
0.90
3.7
Example


97


89

81
55
0.12
1443
1640
7.7
0.88

4.1

Comparative Example


98

94
88
25
0.16
1362
1630
7.4
0.84
3.7
Example


99
AA

88

91
55
0.06
1298
1570
7.9
0.83

4.2

Comparative Example


100

94
92
30
0.09
1312
1570
8.0
0.84
3.4
Example


101

92
82
20
0.14
1276
1560
7.9
0.82
3.5
Example


102
AB

88

89
40
0.18
1134
1450
8.8

0.78

3.2
Comparative Example


103

94
83
25
0.08
1287
1540
8.0
0.84
3.5
Example


104

90

78

20
0.17
1224
1530
8.0
0.80

4.2

Comparative Example


105

AC


88

84
70
0.19
1813
2060
6.3
0.88

4.7

Comparative Example


106

AD


82


71

10
0.06
1013

1310

9.8

0.77

2.6
Comparative Example


107

AE

98
86
80
0.03
1376
1580
8.2
0.87

4.4

Comparative Example


108

AF

93
86
85
0.06
1521
1840
6.7
0.83

4.9

Comparative Example


109

AG


83

88
30
0.03
1055
1430
8.6

0.74

3.2
Comparative Example


110

AH

92
89
5
0.05
1431
1750
7.0
0.82

4.9

Comparative Example


111

AI

90
87
90
0.02
1384
1730
7.5
0.80

4.8

Comparative Example


112

AJ


79


78

75
0.04
1368
1710
7.0
0.80

4.8

Comparative Example


113

AK

93
91
75
0.07
1347
1630
7.8
0.83

4.2

Comparative Example


114

AL

90
86
80
0.02
1356
1620
7.9
0.84

4.9

Comparative Example


115

AM

96
85
90
0.14
1487
1660
7.9
0.90

4.8

Comparative Example


116

AN

94
85
65
0.13
1513
1730
7.7
0.87

4.8

Comparative Example





*1The total area fraction of one or both of B containing carbides having an average grain diameter of 50 nm or less and TM containing carbides having an average grain diameter of 50 nm or less in the whole microstructure


*2 The total area fraction of one or both of B containing carbides having an average grain diameter of 50 nm or less and TM containing carbides having an average grain diameter of 50 nm or less in a region (surface layer) from the surface of the base steel sheet to a position located at ⅛ of the thickness of the base steel sheet


*3The sum of perimeters of carbides having an average grain diameter of 0.1 μm or more and inclusions


Underlined portions indicate items out of the range according to aspects of the present invention.






In the present EXAMPLES, a case where TS was 1320 MPa or more, YR was 0.80 or more, and R/t was less than 3.5 in the case of a tensile strength of 1320 MPa or more and less than 1530 MPa, less than 4.0 in the case of a tensile strength of 1530 MPa or more and less than 1700 MPa, and less than 4.5 in the case of a tensile strength of 1700 MPa or more was judged as satisfactory and shown as “Example” in Table 3-1 through Table 3-4. In addition, a case where TS was less than 1320 MPa, YR was less than 0.80, and R/t did not satisfy the requirements described above was judged as unsatisfactory and shown as “Comparative Example” in Table 3-1 through Table 3-4. Here, in Table 3-1 through Table 3-4, underlined portions indicate items which do not satisfy at least one of the requirements, the manufacturing conditions, and the properties according to aspects of the present invention.

Claims
  • 1-12. (canceled)
  • 13. A high-yield-ratio high-strength electrogalvanized steel sheet comprising an electrogalvanized coating layer formed on a surface of a base steel sheet, wherein the base steel sheet hasa chemical composition containing, by mass %, C: 0.14% or more and 0.40% or less,Si: 0.001% or more and 2.0% or less,Mn: 0.10% or more and 1.70% or less,P: 0.05% or less,S: 0.0050% or less,Al: 0.01% or more and 0.20% or less,N: 0.010% or less, and a balance of Fe and inevitable impurities,a steel microstructure, in which a total area fraction of one or both of bainite containing carbides having an average grain diameter of 50 nm or less and tempered martensite containing carbides having an average grain diameter of 50 nm or less is 90% or more in a whole of the steel microstructure, and in which a total area fraction of one or both of bainite containing carbides having an average grain diameter of 50 nm or less and tempered martensite containing carbides having an average grain diameter of 50 nm or less is 80% or more in a region from the surface of the base steel sheet to a position located at ⅛ of a thickness of the base steel sheet, anddiffusible hydrogen in steel in an amount of 0.20 mass ppm or less.
  • 14. The high-yield-ratio high-strength electrogalvanized steel sheet according to claim 13, wherein the base steel sheet has the chemical composition and the steel microstructure,the steel microstructure includes carbides having an average grain diameter of 0.1 μm or more and inclusions, anda sum of perimeters of the carbides having an average grain diameter of 0.1 μm or more and the inclusions is 50 μm/mm2 or less.
  • 15. The high-yield-ratio high-strength electrogalvanized steel sheet according to claim 13, wherein the chemical composition further contains, by mass %, at least one selected from the group consisting of: group A: B: 0.0002% or more and less than 0.0035%.group B: one or both selected from Nb: 0.002% or more and 0.08% or less and Ti: 0.002% or more and 0.12% or less.group C: one or both selected from Cu: 0.005% or more and 1% or less and Ni: 0.01% or more and 1% or less.group D: one, two, or more selected from Cr: 0.01% or more and 1.0% or less, Mo: 0.01% or more and less than 0.3%, V: 0.003% or more and 0.5% or less, Zr: 0.005% or more and 0.20% or less, and W: 0.005% or more and 0.20% or less.group E: one, two, or more selected from Ca: 0.0002% or more and 0.0030% or less, Ce: 0.0002% or more and 0.0030% or less, La: 0.0002% or more and 0.0030% or less, and Mg: 0.0002% or more and 0.0030% or less.group F: one or both selected from Sb: 0.002% or more and 0.1% or less and Sn: 0.002% or more and 0.1% or less.
  • 16. The high-yield-ratio high-strength electrogalvanized steel sheet according to claim 14, wherein the chemical composition further contains, by mass %, at least one selected from the group consisting of: group A: B: 0.0002% or more and less than 0.0035%.group B: one or both selected from Nb: 0.002% or more and 0.08% or less and Ti: 0.002% or more and 0.12% or less.group C: one or both selected from Cu: 0.005% or more and 1% or less and Ni: 0.01% or more and 1% or less.group D: one, two, or more selected from Cr: 0.01% or more and 1.0% or less, Mo: 0.01% or more and less than 0.3%, V: 0.003% or more and 0.5% or less, Zr: 0.005% or more and 0.20% or less, and W: 0.005% or more and 0.20% or less.group E: one, two, or more selected from Ca: 0.0002% or more and 0.0030% or less, Ce: 0.0002% or more and 0.0030% or less, La: 0.0002% or more and 0.0030% or less, and Mg: 0.0002% or more and 0.0030% or less.group F: one or both selected from Sb: 0.002% or more and 0.1% or less and Sn: 0.002% or more and 0.1% or less.
  • 17. A method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet, the method comprising: a hot rolling process of performing hot rolling on a steel slab having the chemical composition according to claim 13 with a slab heating temperature of 1200° C. or higher and a finishing delivery temperature of 840° C. or higher, cooling the hot-rolled steel sheet to a primary cooling stop temperature of 700° C. or lower in such a manner that cooling is performed at an average cooling rate of 40° C./sec or higher in a temperature range from the finishing delivery temperature to a temperature of 700° C., further cooling the cooled steel sheet to a coiling temperature of 630° C. or lower in such a manner that cooling is performed at an average cooling rate of 2° C./sec or higher in a temperature range from the primary cooling stop temperature to a temperature of 650° C., and coiling the cooled steel sheet;an annealing process of holding the steel sheet obtained in the hot rolling process at an annealing temperature equal to or higher than the AC3 temperature for 30 seconds or more, cooling the held steel sheet from a cooling start temperature of 680° C. or higher to a cooling stop temperature of 260° C. or lower in such a manner that cooling is performed at an average cooling rate of 70° C./sec or higher in a temperature range of 680° C. to 260° C., and holding the cooled steel sheet at a holding temperature of 150° C. to 260° C. for 20 seconds to 1500 seconds; andan electroplating process of cooling the steel sheet after the annealing process to room temperature and performing an electrogalvanizing treatment on the cooled steel sheet for an electrogalvanizing time of 300 seconds or less.
  • 18. A method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet, the method comprising: a hot rolling process of performing hot rolling on a steel slab having the chemical composition according to claim 14 with a slab heating temperature of 1200° C. or higher and a finishing delivery temperature of 840° C. or higher, cooling the hot-rolled steel sheet to a primary cooling stop temperature of 700° C. or lower in such a manner that cooling is performed at an average cooling rate of 40° C./sec or higher in a temperature range from the finishing delivery temperature to a temperature of 700° C., further cooling the cooled steel sheet to a coiling temperature of 630° C. or lower in such a manner that cooling is performed at an average cooling rate of 2° C./sec or higher in a temperature range from the primary cooling stop temperature to a temperature of 650° C., and coiling the cooled steel sheet;an annealing process of holding the steel sheet obtained in the hot rolling process at an annealing temperature equal to or higher than the AC3 temperature for 30 seconds or more, cooling the held steel sheet from a cooling start temperature of 680° C. or higher to a cooling stop temperature of 260° C. or lower in such a manner that cooling is performed at an average cooling rate of 70° C./sec or higher in a temperature range of 680° C. to 260° C., and holding the cooled steel sheet at a holding temperature of 150° C. to 260° C. for 20 seconds to 1500 seconds; andan electroplating process of cooling the steel sheet after the annealing process to room temperature and performing an electrogalvanizing treatment on the cooled steel sheet for an electrogalvanizing time of 300 seconds or less.
  • 19. A method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet, the method comprising: a hot rolling process of performing hot rolling on a steel slab having the chemical composition according to claim 15 with a slab heating temperature of 1200° C. or higher and a finishing delivery temperature of 840° C. or higher, cooling the hot-rolled steel sheet to a primary cooling stop temperature of 700° C. or lower in such a manner that cooling is performed at an average cooling rate of 40° C./sec or higher in a temperature range from the finishing delivery temperature to a temperature of 700° C., further cooling the cooled steel sheet to a coiling temperature of 630° C. or lower in such a manner that cooling is performed at an average cooling rate of 2° C./sec or higher in a temperature range from the primary cooling stop temperature to a temperature of 650° C., and coiling the cooled steel sheet;an annealing process of holding the steel sheet obtained in the hot rolling process at an annealing temperature equal to or higher than the AC3 temperature for 30 seconds or more, cooling the held steel sheet from a cooling start temperature of 680° C. or higher to a cooling stop temperature of 260° C. or lower in such a manner that cooling is performed at an average cooling rate of 70° C./sec or higher in a temperature range of 680° C. to 260° C., and holding the cooled steel sheet at a holding temperature of 150° C. to 260° C. for 20 seconds to 1500 seconds; andan electroplating process of cooling the steel sheet after the annealing process to room temperature and performing an electrogalvanizing treatment on the cooled steel sheet for an electrogalvanizing time of 300 seconds or less.
  • 20. A method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet, the method comprising: a hot rolling process of performing hot rolling on a steel slab having the chemical composition according to claim 16 with a slab heating temperature of 1200° C. or higher and a finishing delivery temperature of 840° C. or higher, cooling the hot-rolled steel sheet to a primary cooling stop temperature of 700° C. or lower in such a manner that cooling is performed at an average cooling rate of 40° C./sec or higher in a temperature range from the finishing delivery temperature to a temperature of 700° C., further cooling the cooled steel sheet to a coiling temperature of 630° C. or lower in such a manner that cooling is performed at an average cooling rate of 2° C./sec or higher in a temperature range from the primary cooling stop temperature to a temperature of 650° C., and coiling the cooled steel sheet;an annealing process of holding the steel sheet obtained in the hot rolling process at an annealing temperature equal to or higher than the AC3 temperature for 30 seconds or more, cooling the held steel sheet from a cooling start temperature of 680° C. or higher to a cooling stop temperature of 260° C. or lower in such a manner that cooling is performed at an average cooling rate of 70° C./sec or higher in a temperature range of 680° C. to 260° C., and holding the cooled steel sheet at a holding temperature of 150° C. to 260° C. for 20 seconds to 1500 seconds; andan electroplating process of cooling the steel sheet after the annealing process to room temperature and performing an electrogalvanizing treatment on the cooled steel sheet for an electrogalvanizing time of 300 seconds or less.
  • 21. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 17, the method further comprising a cold rolling process of performing cold rolling on the steel sheet after the hot rolling process between the hot rolling process and the annealing process.
  • 22. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 18, the method further comprising a cold rolling process of performing cold rolling on the steel sheet after the hot rolling process between the hot rolling process and the annealing process.
  • 23. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 19, the method further comprising a cold rolling process of performing cold rolling on the steel sheet after the hot rolling process between the hot rolling process and the annealing process.
  • 24. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 20, the method further comprising a cold rolling process of performing cold rolling on the steel sheet after the hot rolling process between the hot rolling process and the annealing process.
  • 25. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 17, the method further comprising a tempering process of holding the steel sheet after the electroplating process in a temperature range of 250° C. or lower for a holding time t which satisfies relational expression (1) below: (T+273)(log t+4)≤2700  (1),where, in relational expression (1), T denotes a holding temperature (° C.) in the tempering process and t denotes the holding time (sec) in the tempering process.
  • 26. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 18, the method further comprising a tempering process of holding the steel sheet after the electroplating process in a temperature range of 250° C. or lower for a holding time t which satisfies relational expression (1) below: (T+273)(log t+4)≤2700  (1),where, in relational expression (1), T denotes a holding temperature (° C.) in the tempering process and t denotes the holding time (sec) in the tempering process.
  • 27. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 19, the method further comprising a tempering process of holding the steel sheet after the electroplating process in a temperature range of 250° C. or lower for a holding time t which satisfies relational expression (1) below: (T+273)(log t+4)≤2700  (1),where, in relational expression (1), T denotes a holding temperature (° C.) in the tempering process and t denotes the holding time (sec) in the tempering process.
  • 28. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 20, the method further comprising a tempering process of holding the steel sheet after the electroplating process in a temperature range of 250° C. or lower for a holding time t which satisfies relational expression (1) below: (T+273)(log t+4)≤2700  (1),where, in relational expression (1), T denotes a holding temperature (° C.) in the tempering process and t denotes the holding time (sec) in the tempering process.
  • 29. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 21, the method further comprising a tempering process of holding the steel sheet after the electroplating process in a temperature range of 250° C. or lower for a holding time t which satisfies relational expression (1) below: (T+273)(log t+4)≤2700  (1),where, in relational expression (1), T denotes a holding temperature (° C.) in the tempering process and t denotes the holding time (sec) in the tempering process.
  • 30. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 22, the method further comprising a tempering process of holding the steel sheet after the electroplating process in a temperature range of 250° C. or lower for a holding time t which satisfies relational expression (1) below: (T+273)(log t+4)≤2700  (1),where, in relational expression (1), T denotes a holding temperature (° C.) in the tempering process and t denotes the holding time (sec) in the tempering process.
  • 31. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 23, the method further comprising a tempering process of holding the steel sheet after the electroplating process in a temperature range of 250° C. or lower for a holding time t which satisfies relational expression (1) below: (T+273)(log t+4)≤2700  (1),where, in relational expression (1), T denotes a holding temperature (° C.) in the tempering process and t denotes the holding time (sec) in the tempering process.
  • 32. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 24, the method further comprising a tempering process of holding the steel sheet after the electroplating process in a temperature range of 250° C. or lower for a holding time t which satisfies relational expression (1) below: (T+273)(log t+4)≤2700  (1),where, in relational expression (1), T denotes a holding temperature (° C.) in the tempering process and t denotes the holding time (sec) in the tempering process.
  • 33. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 17, wherein a rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature in the hot rolling process is 200 seconds or less.
  • 34. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 18, wherein a rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature in the hot rolling process is 200 seconds or less.
  • 35. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 19, wherein a rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature in the hot rolling process is 200 seconds or less.
  • 36. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 20, wherein a rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature in the hot rolling process is 200 seconds or less.
  • 37. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 21, wherein a rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature in the hot rolling process is 200 seconds or less.
  • 38. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 22, wherein a rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature in the hot rolling process is 200 seconds or less.
  • 39. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 23, wherein a rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature in the hot rolling process is 200 seconds or less.
  • 40. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 24, wherein a rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature in the hot rolling process is 200 seconds or less.
  • 41. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 25, wherein a rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature in the hot rolling process is 200 seconds or less.
  • 42. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 26, wherein a rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature in the hot rolling process is 200 seconds or less.
  • 43. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 27, wherein a rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature in the hot rolling process is 200 seconds or less.
  • 44. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 28, wherein a rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature in the hot rolling process is 200 seconds or less.
  • 45. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 29, wherein a rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature in the hot rolling process is 200 seconds or less.
  • 46. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 30, wherein a rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature in the hot rolling process is 200 seconds or less.
  • 47. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 31, wherein a rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature in the hot rolling process is 200 seconds or less.
  • 48. The method for manufacturing a high-yield-ratio high-strength electrogalvanized steel sheet according to claim 32, wherein a rolling time in a temperature range from a temperature of 1150° C. to the finishing delivery temperature in the hot rolling process is 200 seconds or less.
Priority Claims (1)
Number Date Country Kind
2018-196590 Oct 2018 JP national
CROSS REFERENCE TO RELATED APPLICATIONS

This is the U.S. National Phase application of PCT/JP2019/030792, filed Aug. 6, 2019, which claims priority to Japanese Patent Application No. 2018-196590, filed Oct. 18, 2018, the disclosures of these applications being incorporated herein by reference in their entireties for all purposes.

PCT Information
Filing Document Filing Date Country Kind
PCT/JP2019/030792 8/6/2019 WO 00