HIGH STRENGTH STEEL SHEET

Abstract
High strength steel sheet having a tensile strength of 800 MPa or more comprising a middle part in sheet thickness and a soft surface layer arranged at one side or both sides of the middle part in sheet thickness, wherein each soft surface layer has a thickness of more than 10 μM and 30% or less of the sheet thickness, the soft surface layer has an average Vickers hardness of more than 0.60 time and 0.90 time or less the average Vickers hardness of the sheet thickness 1/2 position, and the soft surface layer has a nano-hardness standard deviation of 0.8 or less is provided.
Description
FIELD

The present invention relates to high strength steel sheet, more particularly high strength steel sheet with a tensile strength of 800 MPa or more, preferably 1100 MPa or more.


BACKGROUND

In recent years, from the viewpoint of improvement of fuel efficiency for the end purpose of environmental protection, higher strength of the steel sheet for automotive use has been strongly sought. In general, in ultra high strength cold rolled steel sheet, the methods of formation applied in soft steel sheet such as drawing and stretch forming cannot be applied. As the method of formation, bending has become principal. Further, to raise the strength, excellent bendability plus a high bending load are necessary. Therefore, if using ultra high strength cold rolled steel sheet as a structural part of an automobile, excellent bendability and bending load become important criteria for selection.


In this regard, in bending steel sheet, a large tensile stress acts in the circumferential direction of the surface layer part at the outer circumference of the bend. On the other hand, a large compressive stress acts on the surface layer part at the inner circumference of the bend. Therefore, the state of the surface layer part has a large effect on the bendability of ultra high strength cold rolled steel sheet. Accordingly, it is known that by providing a soft layer at the surface layer, the tensile stress and compressive stress occurring at the surface of the steel sheet at the time of bending are eased and the bendability is improved. Regarding high strength steel sheet having a soft layer at the surface layer in this way, PTLs 1 to 3 disclose the following such steel sheet and methods of producing the same.


First, PTL 1 describes high strength plated steel sheet characterized by having, in order from the interface of the steel sheet and plating layer toward the steel sheet side, an inner oxide layer containing an oxide of Si and/or Mn, a soft layer containing that inner oxide layer, and a hard layer comprised of structures of mainly martensite and bainite and having an average depth T of the soft layer of 20 μm or more and an average depth “t” of the inner oxide layer of 4 t.tm to less than T and a method of producing the same.


Next, PTL 2 describes high strength hot dip galvanized steel sheet characterized by having a value (ΔHv) of a Vickers hardness of a position 100 μm from the steel sheet surface minus a Vickers hardness of a position of 20 μM depth from the steel sheet surface of 30 or more and a method of producing the same.


Next, PTL 3 describes high strength hot dip galvanized steel sheet characterized by having a Vickers hardness at a position of 5 μm from the surface layer to the sheet thickness direction of 80% or less of the hardness at a 1/2 position in the sheet thickness direction and by having a hardness at a position of 15 μm from the surface layer to the sheet thickness direction of 90% or more of the Vickers hardness at a 1/2 position in the sheet thickness direction and a method of producing the same.


However, in each of PTLs 1 to 3, the variation of hardness of the soft layer is not sufficiently studied. For example, PTL 1 describes that the soft layer has an inner oxide layer, but, in this case, it is guessed that variation arises in hardness between the oxides and other structures inside the soft layer. If the hardness of the soft layer varies, sometimes sufficient bendability cannot be achieved in steel sheet having such a soft layer. Further, in each of PTLs 1 to 3 as well, control of the gradient of hardness at the transition zone between the soft layer of the surface layer and the hard layer of the inside is not alluded to at all. Further, due to the surface layer having the soft layer, the bending load is believed to deteriorate, but none of PTLs 1 to 3 allude to the bending load.


CITATION LIST
Patent Literature

[PTL 1] JP 2015-34334


[PTL 2] JP 2015-117403


[PTL 3] WO 2016/013145


SUMMARY
Technical Problem

The present invention advantageously solves the problems harbored by the above-mentioned prior art, and an object of the present invention is to provide high strength steel sheet having bendability suitable as a material for auto parts.


Solution to Problem

The inventors engaged in intensive studies to solve the problems relating to the bendability of ultra high strength steel sheet. First, the present inventors referred to conventional knowledge to produce steel sheets having a soft layer at the surface layer and investigate their bendability. Each steel sheet having a soft layer at its surface layer showed improvement in bendability. At this time, it was learned that lowering the average hardness of the soft layer more and making the thickness of the soft layer greater generally acted in a direction where the bendability was improved and the bending load deteriorated. However, the inventors continued to investigate this in more detail and as a result noticed that if using numerous types of methods to soften the surface layer, if just adjusting the average hardness of the soft layer of the surface layer and the thickness of the soft layer, the bendability of the steel sheet is not sufficiently improved and the bending load remarkably deteriorates.


Therefore, the inventors engaged in more detailed studies. As a result, they learned that double-layer steel sheet obtained by welding steel sheet having certain characteristics to one side or both sides of a matrix material and hot rolling or annealing them under specific conditions can improve the bendability the most without causing deterioration of the bending load. Further, they clarified that the biggest reason why the bendability is improved by the above method is the suppression of variation of micro hardness at the soft layer. This effect is extremely remarkable. Compared with when the variation of hardness of the soft layer is large, even if the average hardness of the soft layer is high and, further, even if the thickness of the soft layer is small, a sufficient improvement in bendability was obtained. Due to this, it became possible to minimize the deterioration of the tensile strength due to the soft layer and achieve both a tensile strength never obtained in the past, specifically a tensile strength of 800 MPa or more, preferably 1100 MPa or more, and bendability. The mechanism of this effect is not completely clear, but is believed to be as follows. If there is a variation of hardness at the soft layer, inside the soft layer, there will often be a plurality of structures (ferrite, pearlite, bainite, martensite, retained austenite) and/or oxides. The second phases (or second structures) with different mechanical characteristics become causes of concentration of strain and stress at the time of bending and can form voids becoming starting points of fracture. For this reason, it is believed that by suppressing variation of hardness of the soft layer, it was possible to improve the bendability. Further, the present inventors discovered that by not only suppressing variation in micro hardness at the soft layer of the surface layer but also reducing the gradient of the hardness in the sheet thickness direction at the region of transition from the soft layer of the surface layer to the hard layer at the inside (below, referred to as the “transition zone”) simultaneously, the bendability is further improved. When the gradient of the hardness of the transition zone of the soft layer and hard layer is sharp, the amounts of plastic deformation of the soft layer and hard layer greatly differ and the possibility of fracture occurring in the transition zone becomes higher. From this, it is believed that the bendability can be further improved by suppressing the variations in micro hardness at the soft layer and in addition simultaneously reducing the gradient in hardness in the sheet thickness direction at the transition zone of the soft layer and hard layer.


Variation of hardness at other than the soft surface layer (below, referred to as the “hard layer”) had no effect on the bendability. From this, it is possible to use steels which conventionally had been considered disadvantageous for bendability such as DP steel and TRIP (transformation induced plasticity) steel etc., excellent in ductility for the hard layer. The point that in addition to tensile strength and bendability, further, ductility can be achieved is one of the excellent points of the present invention.


The gist of the present invention obtained in this way is as follows:


(1) High strength steel sheet having a tensile strength of 800 MPa or more comprising a middle part in sheet thickness and a soft surface layer arranged at one side or both sides of the middle part in sheet thickness, wherein each soft surface layer has a thickness of more than 10 μm and 30% or less of the sheet thickness, the soft surface layer has an average Vickers hardness of more than 0.60 time and 0.90 time or less the average Vickers hardness of the sheet thickness 1/2 position, and the soft surface layer has a nano-hardness standard deviation of 0.8 or less.


(2) The high strength steel sheet according to (1), wherein the high strength steel sheet further comprises a hardness transition zone formed between the middle part in sheet thickness and each soft surface layer while adjoining them, wherein the hardness transition zone has an average hardness change in the sheet thickness direction of 5000 (ΔHv/mm) or less.


(3) The high strength steel sheet according to (1) or (2), wherein the middle part in sheet thickness comprises, by area percent, 10% or more of retained austenite.


(4) The high strength steel sheet according to any one of (1) to (3), wherein the middle part in sheet thickness comprises, by mass %,


C: 0.05 to 0.8%,


Si: 0.01 to 2.50%,


Mn: 0.010 to 8.0%,


P: 0.1% or less,


S: 0.05% or less,


Al: 0 to 3%, and


N: 0.01% or less, and


a balance of Fe and unavoidable impurities.


(5) The high strength steel sheet according to (4), wherein the middle part in sheet thickness further comprises, by mass %, at least one element selected from the group consisting of:


Cr: 0.01 to 3%,


Mo: 0.01 to 1%, and


B: 0.0001% to 0.01%.


(6) The high strength steel sheet according to (4) or (5), wherein the middle part in sheet thickness further comprises, by mass %, at least one element selected from the group consisting of:


Ti: 0.01 to 0.2%,


Nb: 0.01 to 0.2%, and


V: 0.01 to 0.2%.


(7) The high strength steel sheet according to any one of (4) to (6), wherein the middle part in sheet thickness further comprises, by mass %, at least one element selected from the group consisting of:


Cu: 0.01 to 1%, and


Ni: 0.01 to 1%.


(8) The high strength steel sheet according to any one of (4) to (7), wherein the C content of the soft surface layer is 0.30 time or more and 0.90 time or less the C content of the middle part in sheet thickness.


(9) The high strength steel sheet according to any one of (5) to (8), wherein the total of the Mn content, Cr content, and Mo content of the soft surface layer is 0.3 time or more the total of the Mn content, Cr content, and Mo content of the middle part in sheet thickness.


(10) The high strength steel sheet according to any one of (5) to (9), wherein the B content of the soft surface layer is 0.3 time or more the B content of the middle part in sheet thickness.


(11) The high strength steel sheet according to any one of (7) to (10), wherein the total of the Cu content and Ni content of the soft surface layer is 0.3 time or more the total of the Cu content and Ni content of the middle part in sheet thickness.


(12) The high strength steel sheet according to any one of (1) to (11), further comprising a hot dip galvanized layer, hot dip galvannealed layer, or electrogalvanized layer at the surface of the soft surface layer.


Advantageous Effects of Invention

The high strength steel sheet of the present invention has excellent bendability making it suitable as a material for auto part use. Therefore, the high strength steel sheet of the present invention can be suitably used as a material for auto part use. In addition, if the middle part in sheet thickness and the soft surface layer of the high strength steel sheet include between them a hardness transition zone with an average hardness change in the sheet thickness direction of 5000 (ΔHv/mm) or less, it is possible to further improve the bendability. Further, if the middle part in sheet thickness comprises, by area percent, 10% or more of retained austenite, in addition to improvement of the bendability, it is possible to improve the ductility.





BRIEF DESCRIPTION OF DRAWINGS


FIG. 1 shows one example of a distribution of hardness relating to high strength steel sheet according to a preferred embodiment of the present invention.



FIG. 2 is a schematic view explaining diffusion of C atoms at the time of production of the high strength steel sheet of the present invention.



FIG. 3 is a graph showing a change in dislocation density after a rolling pass relating to rough rolling used in the method of producing the high strength steel sheet of the present invention.





DESCRIPTION OF EMBODIMENTS

Below, embodiments of the present invention will be explained. The present invention is not limited to the following embodiments.


The steel sheet according to the present invention has to have an average Vickers hardness of the soft surface layer having a thickness of more than 10 μm and 30% or less of the sheet thickness, more specifically an average Vickers hardness of the soft surface layer as a whole, of more than 0.60 time and 0.90 time or less the average Vickers hardness of the 1/2 position in sheet thickness. With a thickness of the soft surface layer of 10 μm or less, a sufficient improvement of the bendability is not obtained, while if greater than 30%, the tensile strength remarkably deteriorates. The thickness of the soft surface layer more preferably is 20% or less of the sheet thickness, still more preferably 10% or less. If the average Vickers hardness of the soft surface layer is greater than 0.90 time the average Vickers hardness of the 1/2 position in sheet thickness, a sufficient improvement in the bendability is not obtained.


In the present invention, “the average Vickers hardness of the soft surface layer” is determined as follows: First, at certain intervals in the sheet thickness direction from the 1/2 position of sheet thickness toward the surface (for example, every 5% of sheet thickness. If necessary, every 1% or 0.5%), the Vickers hardness at a certain position in the sheet thickness direction is measured by an indentation load of 100 g, then the Vickers hardnesses at a total of at least three points, for example, five points or 10 points, are measured in the same way by an indentation load of 100 g on a line from that position in the direction vertical to sheet thickness and parallel to the rolling direction. The average value of these is deemed the average Vickers hardness at that position in the sheet thickness direction. The intervals between the measurement points aligned in the sheet thickness direction and rolling direction are preferably four times or more the indents when possible. In this Description, a “distance of four times or more the indents” means the distance of four times or more the length of the diagonal line at the rectangular shaped opening of the indent formed by a diamond indenter when measuring the Vickers hardness. When the average Vickers hardness at a certain position in the sheet thickness direction becomes 0.90 time or less the similarly measured average Vickers hardness at the 1/2 position of sheet thickness, the surface side from that position is defined as the “soft surface layer”. By randomly measuring the Vickers hardnesses at 10 points in the soft surface layer defined in this way and calculating the average value of these, the average Vickers hardness of the soft surface layer is determined. If the average Vickers hardness of the soft surface layer is more than 0.60 time and 0.90 time or less the average Vickers hardness of the 1/2 position in sheet thickness, the bendability is improved more. More preferably, it is more than 0.60 time and 0.85 time or less, still more preferably more than 0.60 time and 0.80 time or less.


The nano-hardness standard deviation of the soft surface layer has to be 0.8 or less. This is because, as explained above, by suppressing variation of hardness of the soft surface layer, the bendability is remarkably improved. If the standard deviation is greater than 0.8, this effect is insufficient. From this viewpoint, the standard deviation is more preferably 0.6 or less, still more preferably 0.4 or less. The lower limit of the standard deviation is not designated, but making it 0.05 or less is technically difficult. What affects the bendability is, in particular, the variation in micro hardness of the soft surface layer in the direction vertical to the sheet thickness. Even if there is a moderate gradient of hardness inside the soft surface layer in the sheet thickness direction, the advantageous effect of the present invention is not impaired. Therefore, the nano-hardness standard deviation has to be measured at a certain position in the sheet thickness direction at positions vertical to the sheet thickness direction. In the present invention, “the nano-hardness standard deviation of the soft surface layer” means the standard deviation obtained by measuring the nano-hardnesses of a total of 100 locations at the 1/2 position of thickness of the soft surface layer defined above at 3 μm intervals on a line vertical to the sheet thickness direction and parallel to the rolling direction using a Hysitron tribo-900 under conditions of an indentation depth of 80 nm by a Berkovich shaped diamond indenter.


To further improve the bendability of the high strength steel sheet, the average hardness change in the sheet thickness direction of the hardness transition zone is preferably 5000 (ΔHv/mm) or less. In the present invention, the “hardness transition zone” is defined as follows:


First, at certain intervals in the sheet thickness direction from the 1/2 position of sheet thickness toward the surface (for example, every 5% of sheet thickness. If necessary, every 1% or 0.5%), the Vickers hardness at a certain position in the sheet thickness direction is measured by an indentation load of 100 g, then the Vickers hardnesses at a total of at least three points, for example, five points or 10 points, are measured in the same way by an indentation load of 100 g on a line from that position in the direction vertical to sheet thickness and parallel to the rolling direction. The average value of these is deemed the average Vickers hardness at that position in the sheet thickness direction. The intervals between the measurement points aligned in the sheet thickness direction and rolling direction are preferably four times or more the indents when possible. When the average Vickers hardness at a certain position in the sheet thickness direction becomes 0.95 time or less the similarly measured average Vickers hardness at the 1/2 position of sheet thickness, the region from that position to the previously defined soft surface layer is defined as the hardness transition zone.


The average hardness change in the sheet thickness direction of the hardness transition zone (ΔHv/mm) is defined by the following formula:





Average hardness change (ΔHv/mm)=(Maximum average hardness in Vickers hardnesses of hardness transition zone)−(Minimum average hardness in Vickers hardnesses of hardness transition zone)/Thickness of hardness transition zone


Here, the “maximum average hardness of the Vickers hardness of the hardness transition zone” is the largest value among the average Vickers hardnesses at different positions in the sheet thickness direction in the hardness transition zone, while the “minimum average hardness of the Vickers hardness of the hardness transition zone” is the smallest value among the average Vickers hardnesses at different positions in the sheet thickness direction in the hardness transition zone.


If the average hardness change in the sheet thickness direction of the hardness transition zone is larger than 5000 (ΔHv/mm), sometimes the bendability will fall. Preferably, it is 4000 (ΔHv/mm) or less, more preferably 3000 (ΔHv/mm) or less, most preferably 2000 (ΔHv/mm) or less. The thickness of the hardness transition zone is not prescribed. However, if the ratio of the hardness transition zone in the sheet thickness is large, since the tensile strength will fall, the hardness transition zone is preferably 20% or less of the sheet thickness at one surface. More preferably, it is 10% or less.


To prevent deterioration of the bending load of the high strength steel sheet, the average Vickers hardness of the soft surface layer has to be more than 0.60 time the average Vickers hardness of the 1/2 position in sheet thickness. 110.60 time or less, at the time of bending, the soft surface layer will greatly deform and the middle part in sheet thickness will lean to the outside in the bend so fracture will occur early, therefore the bending load will remarkably deteriorate. The “bending load” referred to here indicates the maximum load obtained when taking a 60 mm×60 mm test piece from the steel sheet and conducting a bending test based on the standard 238-100 of the German Association of the Automotive Industry (VDA) under conditions of a punch curvature of 0.4 mm, a roll size of 30 mm, a distance between rolls of 2×sheet thickness+0.5 (mm), and a maximum indentation stroke of 11 mm.



FIG. 1 shows one example of the distribution of hardness for high strength steel sheet according to a preferred embodiment of the present invention. It shows the distribution of hardness of a thickness 1 mm steel sheet from the surface to 1/2 position of sheet thickness. The abscissa shows the position in the sheet thickness direction (mm). The surface is 0 mm, while the 1/2 position of sheet thickness is 0.5 mm. The ordinate shows the average of five points of the Vickers hardness at different positions in the sheet thickness direction. The Vickers hardness of the 1/2 position of sheet thickness is 430 Hv. The surface side from the point where it becomes 0.90 time or less is the soft surface layer, while the range between the point where it becomes 0.95 time or less and the soft surface layer becomes the hardness transition zone.


To improve the ductility of the high strength steel sheet, the middle part in sheet thickness preferably includes, by area percent, 10% or more of retained austenite. This is so that the ductility is improved by the transformation induced plasticity of the retained austenite. With an area percent of retained austenite of 10% or more, a 15% or more ductility is obtained. If using this effect of retained austenite, even if soft ferrite is not included, a 15% or more ductility can be secured, so the middle part in sheet thickness can be higher in strength and both high strength and high ductility can be achieved. The “ductility” referred to here indicates the total elongation obtained by obtaining a Japan Industrial Standard JIS No. 5 test piece from the steel sheet perpendicular to the rolling direction and conducting a tensile test based on JIS Z2241.


Next, the chemical composition of the middle part in sheet thickness desirable for obtaining the advantageous effect of the present invention will be explained. The “%” relating to the content of elements means “mass %” unless otherwise indicated. In the middle part in sheet thickness, near the boundary with the soft surface layer, due to the diffusion of alloy elements with the soft surface layer, sometimes the chemical composition will differ from a position sufficiently far from the boundary. For example, when the high strength steel sheet of the present invention includes the above-mentioned hardness transition zone, at the middle part in sheet thickness, sometimes the chemical composition will differ between the vicinity of the boundary with the hardness transition zone and a position sufficiently far from the boundary. In such a case, the chemical composition measured near the 1/2 position of sheet thickness is determined as follows:


“C: 0.05 to 0.8%”


C raises the strength of steel sheet and is added so as to raise the strength of the high strength steel sheet. However, if the C content is more than 0.8%, the toughness becomes insufficient. Further, if the C content is less than 0.05%, the strength becomes insufficient. The C content is preferably 0.6% or less in range, more preferably is 0.5% or less in range.


“Si: 0.01 to 2.50%”


Si is a ferrite stabilizing element. It increases the Ac3 transformation point, so it is possible to form a large amount of ferrite at a broad range of annealing temperature. This is added from the viewpoint of improvement of the controllability of structures. To obtain such an effect, the Si content has to be 0.01% or more. On the other hand, from the viewpoint of securing the ductility, if the Si content is less than 0.30%, a large amount of coarse iron-based carbides are formed, the percentage of retained austenite structures in the inner microstructures cannot be 10% or more, and sometimes the elongation ends up falling. From this viewpoint, the lower limit value of Si is preferably 0.30% or more, more preferably 0.50% or more. In addition, Si is an element necessary for suppressing coarsening of the iron-based carbides at the middle part in sheet thickness and raising the strength and formability. Further, as a solution strengthening element, Si has to be added to contribute to the higher strength of the steel sheet. From these viewpoints, the lower limit value of Si is preferably 1% or more, more preferably 1.2% or more. However, if the Si content is more than 2.50%, since the middle part in sheet thickness becomes brittle and the ductility deteriorates, the upper limit is 2.50%. From the viewpoint of securing ductility, the Si content is preferably 2.20% or less, more preferably 2.00% or less.


“Mn: 0.010 to 8.0%”


Mn is added to raise the strength of the high strength steel sheet. To obtain such an effect, the Mn content has to be 0.010% or more. However, if the Mn content exceeds 8.0%, the distribution of the hardness of the steel sheet surface layer caused by segregation of Mn becomes greater. From this viewpoint, the content is preferably 5.0% or less, more preferably 4.0%, still more preferably 3.0% or less.


“P: 0.1% or less”


P tends to segregate at the middle part in sheet thickness of the steel sheet and causes a weld zone to become brittle. If more than 0.1%, the embrittlement of the weld zone becomes remarkable, so the suitable range was limited to 0.1% or less. The lower limit of P content is not prescribed, but making the content less than 0.001% is economically disadvantageous.


“S: 0.05% or less”


S has a detrimental effect on the weldability and also the manufacturability at the time of casting and hot rolling. Due to this, the upper limit value is 0.05% or less. The lower limit of the S content is not prescribed, but making the content less than 0.0001% is economically disadvantageous.


“Al: 0 to 3%”


Al acts as a deoxidizer and is preferably added in the deoxidation step. To obtain such an effect, the Al content has to be 0.01% or more. On the other hand, if the Al content is more than 3%, the danger of slab cracking at the time of continuous casting rises.


“N: 0.01% or less”


Since N forms coarse nitrides and causes the bendability to deteriorate, the addition amount has to be kept down. If N is more than 0.01%, since this tendency becomes remarkable, the range of N content is 0.01% or less. In addition, N causes the formation of blowholes at the time of welding, and so should be small in content. Even if the lower limit value of the N content is not particularly determined, the effect of the present invention is exhibited, but making the N content less than 0.0005% invites a large increase in manufacturing costs, and therefore this is the substantive lower limit value.


“At least one element selected from the group comprised of Cr: 0.01 to 3%, Mo: 0.01 to 1%, and B: 0.0001 to 0.01%”


Cr, Mo, and B are elements contributing to improvement of strength and can be used in place of part of Mn. Cr, Mo, and B, alone or in combinations of two or more, are preferably respectively included in 0.01% or more, 0.01% or more, and 0.0001% or more. On the other hand, if the contents of the elements are too great, the pickling ability, weldability, hot workability, etc., sometimes deteriorate, so the contents of Cr, Mo, and B are preferably respectively 3% or less, 1% or less, and 0.01% or less.


“At least one element selected from the group comprised of Ti: 0.01 to 0.2%, Nb: 0.01 to 0.2%, and V: 0.01 to 0.2%”


Ti, Nb, and V are strengthening elements. They contribute to the rise of strength of the steel sheet by precipitation strengthening, strengthening of crystal grains by suppression of growth of ferrite crystal grains, and dislocation strengthening through suppression of recrystallization. When added for this purpose, 0.01% or more is preferably added. However, if the respective contents are more than 0.2%, the precipitation of carbonitrides increases and the formability deteriorates.


“At least one element selected from the group comprised of Cu: 0.01 to 1% and Ni: 0.01 to 1%”


Cu and Ni are elements contributing to improvement of strength and can be used in place of part of Mn. Cu and Ni, alone or together, are preferably respectively included in 0.01% or more. On the other hand, if the contents of the elements are too great, the pickling ability, weldability, hot workability, etc., sometimes deteriorate, so the contents of Cr and Ni are preferably respectively 1.0% or less.


Further, even if unavoidably adding the following elements to the middle part in sheet thickness, the effect of the present invention is not impaired. That is, O: 0.001 to 0.02%, W: 0.001 to 0.1%, Ta: 0.001 to 0.1%, Sn: 0.001 to 0.05%, Sb: 0.001 to 0.05%, As: 0.001 to 0.05%, Mg: 0.0001 to 0.05%, Ca: 0.001 to 0.05%, Zr: 0.001 to 0.05%, and REM (rare earth metals) such as Y: 0.001 to 0.05%, La: 0.001 to 0.05% and Ce: 0.001 to 0.05%.


The steel sheet in the present invention sometimes differs in chemical composition between the soft surface layer and the middle part in sheet thickness. While explained later, the important point in the present invention is that the surface layer is substantially low temperature transformed structures (bainite, martensite, etc.) and ferrite and pearlite transformation is suppressed to reduce the variation of hardness. In such a case, the preferable chemical composition at the soft surface layer is as follows:


“C:0.30 time or more and 0.90 time or less the C content of middle part in sheet thickness and 0.72% or less”


C raises the strength of steel sheet and is added for raising the strength of the high strength steel sheet. The C content of the soft surface layer is preferably 0.90 time or less the C content of the middle part in sheet thickness. This is to lower the hardness of the soft surface layer from the hardness of the middle part in sheet thickness. If larger than 0.90 time, sometimes the average Vickers hardness of the soft surface layer will not become 0.90 time or less the average Vickers hardness of the 1/2 position in sheet thickness. More preferably, the C content of the soft surface layer is 0.80 time or less the C content of the middle part in sheet thickness, more preferably 0.70 time or less. The C content of the soft surface layer has to be 0.30 time or more the C content of the middle part in sheet thickness. If lower than 0.30 time, sometimes the average Vickers hardness of the soft surface layer will not become more than 0.60 time the average Vickers hardness of the 1/2 position in sheet thickness. If the C content of the soft surface layer is 0.90 time or less the C content of the middle part in sheet thickness, since the preferable C content of the middle part in sheet thickness is 0.8% or less, the preferable C content of the soft surface layer becomes 0.72% or less. Preferably the content is 0.5% or less, more preferably 0.3% or less, most preferably 0.1% or less. The lower limit of the C content is not particularly prescribed. If using industrial grade ultralow C steel, about 0.001% is the substantive lower limit, but from the viewpoint of the solid solution C amount, the Ti, Nb, etc., may be used to completely remove the solid solution C and use the steel as “interstitial free steel”.


“Si: 0.01 to 2.5%”


Si is an element suppressing temper softening of martensite and can keep the strength from dropping due to tempering by its addition. To obtain such effects, the Si content has to be 0.01% or more. However, addition of more than 2.5% causes deterioration of the toughness, so the content is 2.5% or less.


“Mn: 0.01 to 8.0%”


Mn is added to raise the strength of the high strength steel sheet. To obtain such an effect, the Mn content has to be 0.01% or more. However, if the Mn content is more than 8.0%, the distribution of hardness of the steel sheet surface layer caused by segregation of Mn becomes greater. From this viewpoint, the content is preferably 5% or less, more preferably 3% or less.


In addition, the total of the Mn content, Cr content, and Mo content of the soft surface layer is preferably 0.3 time or more the total of the Mn content, Cr content, and Mo content of the middle part in sheet thickness. This will be explained later, but the soft surface layer reduces the variation of hardness by making the majority of the structures low temperature transformed structures (bainite and martensite etc.). If the total of the Mn content, Cr content, and Mo content for improving the hardenability is smaller than 0.3 time the total of the Mn content, Cr content, and Mo content of the middle part in sheet thickness, ferrite transformation easily occurs and variation of hardness is caused. More preferably, the total is 0.5 time or more, more preferably 0.7 time or more. The upper limit values of these are not prescribed.


“P: 0.1% or less”


P makes the weld zone brittle. If more than 0.1%, the embrittlement of the weld zone becomes remarkable, so the suitable range was limited to 0.1% or less. The lower limit of the P content is not prescribed, but making the content less than 0.001% is economically disadvantageous.


“S: 0.05% or less”


S has a detrimental effect on the weldability and the manufacturability at the time of casting and the time of hot rolling. Due to this, the upper limit value is 0.05% or less. The lower limit of the S content is not prescribed, but making the content less than 0.0001% is economically disadvantageous.


“Al: 0 to 3%”


Al acts as a deoxidizer and preferably is added in the deoxidation step. To obtain such an effect, the Al content has to be 0.01% or more. On the other hand, if the Al content is more than 3%, the danger of slab cracking at the time of continuous casting rises.


“N: 0.01% or less”


N forms coarse nitrides and causes the bendability to deteriorate, so the amount added has to be kept down. If N is more than 0.01%, since this tendency becomes remarkable, the range of the N content is 0.01% or less. In addition N becomes a cause of formation of blowholes at the time of welding, so the smaller the content the better. Even with the lower limit of the N content not particularly determined, the effect of the present invention is exhibited, but making the N content less than 0.0005% invites a large increase in manufacturing costs, so this is substantively the lower limit value.


“At least one element selected from the group comprising Cr: 0.01 to 3%, Mo: 0.01 to 1%, and B: 0.0001 to 0.01%”


Cr, Mo, and B are elements contributing to improvement of strength and can be used in place of part of Mn. Cr, Mo, and B, alone or in combinations of two or more, are preferably respectively included in 0.01% or more, 0.01% or more, and 0.0001% or more. On the other hand, if the contents of the elements are too great, since the pickling ability, weldability, hot workability, etc., sometimes deteriorate, the Cr, Mo, and B contents are preferably respectively 3% or less, 1% or less, and 0.01% or less. Further, there is a preferable range for the total of Cr and Mo with Mn. This is as explained above.


Further, the B content of the soft surface layer is preferably 0.3 time or more the B content of the middle part in sheet thickness. If the B content for improving the hardenability is smaller than 0.3 time the B content of the middle part in sheet thickness, ferrite transformation easily occurs and variation of hardness is caused. More preferably, it is 0.5 time or more, still more preferably 0.7 time or more. No upper limit value is prescribed.


“At least one type of element selected from the group comprising Ti: 0.01 to 0.2%, Nb: 0.01 to 0.2%, and V: 0.01 to 0.2%”


Ti, Nb, and V are strengthening elements. They contribute to the rise of strength of the steel sheet by precipitation strengthening, strengthening of crystal grains by suppression of growth of ferrite crystal grains, and dislocation strengthening through suppression of recrystallization. When added for this purpose, 0.01% or more is preferably added. However, if the respective contents are more than 0.2%, the precipitation of carbonitrides increases and the formability deteriorates.


“At least one element selected from the group comprised of Cu: 0.01 to 1% and Ni: 0.01 to 1%”


Cu and Ni are elements contributing to improvement of strength and can be used in place of part of Mn. Cu and Ni, alone or together, are preferably respectively included in 0.01% or more. On the other hand, if the contents of the elements are too great, the pickling ability, weldability, hot workability, etc., sometimes deteriorate, so the contents of Cu and Ni are preferably respectively 1.0% or less.


Further, the total of the Cu content and Ni content of the soft surface layer is preferably 0.3 time or more the total of the Cu content and Ni content of the middle part in sheet thickness. If the total of the Cu content and Ni content for improving the hardenability is smaller than 0.3 time the total of the Cu content and Ni content of the middle part in sheet thickness, ferrite transformation easily occurs and a variation of hardness is caused. More preferably, it is 0.5 time or more, still more preferably 0.7 time or more. No upper limit value is prescribed.


Furthermore, even if intentionally or unavoidably adding the following elements to the soft surface layer, the effect of the present invention is not impaired. That is, O: 0.001 to 0.02%, W: 0.001 to 0.1%, Ta: 0.001 to 0.1%, Sn: 0.001 to 0.05%, Sb: 0.001 to 0.05%, As: 0.001 to 0.05%, Mg: 0.0001 to 0.05%, Ca: 0.001 to 0.05%, Zr: 0.001 to 0.05%, and Y: 0.001 to 0.05%, La: 0.001 to 0.05%, Ce: 0.001 to 0.05%, and other REM (rare earth metal).


The effect of the present invention, i.e., the excellent bendability and/or ductility, can similarly be achieved even if treating the surface of the soft surface layer by hot dip galvanizing, hot dip galvannealing, electrogalvanizing, etc.


Next, the mode of the method of production for obtaining the high strength steel sheet of the present invention will be explained. The following explanation aims at a simple illustration of the method of production for obtaining the high strength steel sheet of the present invention. It is not intended to limit the strength steel sheet of the present invention to double-layer steel sheet comprised of two steel sheets stacked together as explained below. For example, it is also possible to decarburize a single-layer steel sheet to soften the surface layer part and thereby produce a high strength steel sheet comprised of a soft surface layer and a middle part in sheet thickness.


One important point in the present invention is the point of reducing the variation of hardness of the surface layer. The variation of hardness of the surface layer becomes larger when the surface layer has both ferrite, pearlite, or other relatively soft structures and low temperature transformed structures (bainite and martensite) present. In the following method of production, in the present invention, the method of making the surface layer substantially low temperature transformed structures will be explained.


The degreased matrix steel sheet satisfying the above constituents of the middle part in sheet thickness has the surface layer-use steel sheet superposed on one or both surfaces.


By hot rolling, cold rolling, continuously annealing, continuously hot dip coating, and otherwise treating the above-mentioned multilayer member (double-layer steel sheet), the high strength steel sheet according to the present invention, more specifically a hot rolled steel sheet, cold rolled steel sheet, and plated steel sheet, can be obtained.


For example, the method for producing hot rolled steel sheet among the high strength steel sheets encompassed by the present invention is characterized by comprising:


superposing on one or both surfaces of a matrix steel sheet having a chemical composition explained above and forming a middle part in sheet thickness a surface layer-use steel sheet having a chemical composition similarly explained above and forming a soft surface layer to form a double-layer steel sheet,


heating the double-layer steel sheet to a heating temperature of 1100° C. or more and 1350° C. or less, preferably more than 1150° C. and 1350° C. or less, then hot rolling it, wherein the hot rolling comprises rough rolling and finish rolling of a finishing temperature of 800 to 980° C., the rough rolling is performed two times under conditions of a rough rolling temperature of 1100° C. or more, a sheet thickness reduction rate per pass of 5% or more and less than 50%, and a time between passes of 3 seconds or more, and


cooling the hot rolled double-layer steel sheet in a cooling process from 750° C. to 550° C. by an average cooling rate of 2.5° C./s or more, then coiling it at a coiling temperature of 550° C. or less.


If making an element diffuse between the matrix steel sheet and surface layer-use steel sheet and forming between the two a hardness transition zone with an average hardness change in the sheet thickness direction of 5000 (ΔHv/mm) or less, in the hot rolling step, it is preferable to heat the double-layer steel sheet by a heating temperature of 1100° C. or more and 1350° C. or less for 2 hours, more preferably to heat it at more than 1150° C. and 1350° C. or less for 2 hours or more.


To make the retained austenite of the middle part in sheet thickness in the high strength steel sheet an area percent of 10% or more to improve the ductility of the high strength steel sheet, instead of the step after the hot rolling prescribed above, it is preferable to include holding the hot rolled double-layer steel sheet in the cooling process at a temperature of 700° C. to 500° C. for 3 seconds or more, then coiling it at a temperature of the martensite transformation start temperature Ms to the bainite transformation start temperature Bs of the matrix steel sheet.


Here,


Bs (° C.)=820−290C/(1−Sf)−37Si−90Mn−65Cr−50Ni+70A1


Ms (° C.)=541−474C/(1−Sf)−15Si−35Mn−17Cr−17Ni+19A1


where, C, Si, Mn, Cr, Ni, and Al are the contents (mass %) of the elements of the matrix steel sheet, while Sf is the area percent of ferrite in the matrix steel sheet.


If explaining the steps in more detail, if obtaining hot rolled steel sheet, first, the double-layer steel sheet prepared by the above method is heated by a heating temperature of 1100° C. or more, preferably more than 1150° C. and 1350° C. or less. To suppress anisotropy of the crystal orientations due to casting, the heating temperature of the slab is preferably 1100° C. or more. On the other hand, since heating a slab to more than 1350° C. requires input of a large amount of energy and invites a large increase in manufacturing costs, the heating temperature is 1350° C. or less. Further, to control the nano-hardness standard deviation of the soft surface layer to 0.8 or less and, further, when there is a hardness transition zone, give that a steady hardness change, the concentrations of the alloy elements, in particular the C atoms, have to be controlled so as to be steadily distributed. The distribution of the C concentration is obtained by diffusion of the C atoms. The frequency of diffusion of C atoms increases the higher the temperature. Therefore, to control the concentration of C, control from the hot rolling heating to the rough rolling becomes important. In hot rolling heating, to promote the diffusion of C atoms, the heating temperature has to be higher. Preferably, it is 1100° C. or more and 1350° C. or less, more preferably more than 1150° C. and 1350° C. or less. In hot rolling heating, the changes of (i) and (ii) shown in FIG. 2 occur. (i) shows the diffusion of C atoms from the middle part in sheet thickness to the soft surface layer, while (ii) shows the decarburization reaction of C being disassociated from the soft surface layer to the outside. The distribution of the concentration of C arises due to the balance between the diffusion of C atoms and disassociation reaction of this (i) and (ii). If less than 1100° C., since the reaction of (i) is insufficient, the preferable distribution of concentration of C is not obtained. On the other hand, if more than 1350° C., since the reaction of (ii) excessively occurs, similarly the preferred distribution of concentration is not obtained.


Furthermore, to obtain a furthermore suitable distribution of concentration of C after controlling the distribution to the preferable distribution of concentration of C by adjustment of the hot rolling heating temperature, pass control in the rough rolling is extremely important. The rough rolling is performed two times or more under conditions of a rough rolling temperature of 1100° C. or more, a sheet thickness reduction rate per pass of 5% or more and less than 50%, and a time between passes of 3 seconds or more. This is so as to promote the diffusion of C atoms of (i) in FIG. 2 by the strain introduced in the rough rolling. If using an ordinary method for rough rolling and finish rolling a slab controlled to a preferable state of concentration of C by hot rolling heating, the sheet thickness would be reduced without the C atoms being sufficiently diffused inside the soft surface layer. Therefore, if producing hot rolled steel sheet of a thickness of several mm by hot rolling by an ordinary method from a slab having a thickness of more than 200 mm, the result would be a steel sheet with a concentration of C rapidly changing at the soft surface layer and a steady hardness change could no longer be obtained. The method discovered for solving this is the above pass control of rough rolling. The diffusion of C atoms is greatly affected by not only temperature, but also strain (dislocation density). In particular, compared with lattice diffusion, with dislocation diffusion, the diffusion frequency rises 10 times or more higher, so steps are required for making the sheet thickness thinner by rolling while leaving the dislocation density. The curve 1 of FIG. 3 shows the change in dislocation density after a rolling pass when the sheet thickness reduction rate per pass in rough rolling is small. It is learned that strain remains over a long period of time. By leaving strain at the soft surface layer over a long period of time in this way, sufficient diffusion of C atoms inside the soft surface layer occurs and the optimal distribution of concentration of C can be obtained. On the other hand, curve 2 shows the change in the dislocation density when the sheet thickness reduction rate is large. If the amount of strain introduced by rolling becomes higher, recovery is easily promoted and the dislocation density rapidly falls. For this reason, to obtain the optimal distribution of concentration of C, it is necessary to prevent a change in the dislocation density such as shown in the curve 2. From such a viewpoint, the upper limit of the sheet thickness reduction rate per pass becomes less than 50%. To promote the diffusion of C atoms at the soft surface layer, securing certain amounts of dislocation density and holding time becomes necessary, so the lower limit of the sheet thickness reduction rate becomes 5% and a time between passes of 3 seconds or more must be secured.


Further, when forming a hardness transition zone, the heating time of the slab is 2 hours or more. This is so as to cause elements to diffuse between the matrix steel sheet and the surface layer-use steel sheet during slab heating and reduce the average hardness change of the hardness transition zone formed between the two. If the heating time is shorter than 2 hours, the average hardness change of the hardness transition zone will not become sufficiently small. The upper limit of the heating time is not prescribed, but heating for 8 hours or more requires a large amount of heating energy and is not preferable from the cost aspect.


After heating the slab, it is hot rolled. If the end temperature of the hot rolling (finishing temperature) is less than 800° C. the rolling reaction force will become higher and it will become difficult to stably obtain the designated sheet thickness. For this reason, the end temperature of the hot rolling is 800° C. or more. On the other hand, making the end temperature of the hot rolling more than 980° C. requires an apparatus for heating the steel sheet from the end of heating of the slab to the end of the hot rolling. A high cost is required. Therefore, the end temperature of the hot rolling is 980° C. or less.


After that, in the cooling process, the sheet is cooled from 750° C. to 550° C. by an average cooling rate of 2.5° C./s or more. This is an important condition in the present invention. This step is necessary for making the majority of the soft surface layer low temperature transformed structures and reducing the variation of hardness. If the average cooling rate is slower than 2.5° C./s, ferrite transformation and pearlite transformation occur at the soft surface layer and cause variation of hardness. More preferably, the rate is 5° C./s or more, still more preferably 10° C./s or more. With a temperature higher than 750° C., ferrite transformation and pearlite transformation become less likely to occur, and therefore the average cooling rate is not prescribed. With a temperature lower than 550° C., the structures transform to low temperature transformed structures, and therefore the average cooling rate is not prescribed.


The coiling temperature is 550° C. or less. With a temperature higher than 550° C., ferrite transformation and pearlite transformation occur at the soft surface layer and cause variation of hardness. More preferably, the temperature is 500° C. or less, still more preferably 300° C. or less.


On the other hand, to make the retained austenite of the middle part in sheet thickness at the high strength steel sheet an area percent of 10% or more to improve the ductility of the high strength steel sheet, after the above hot rolling, in the cooling process, the sheet is held at a temperature between 700° C. to 500° C. for 3 seconds or more. This is an important condition in the present invention and is a step required for causing only the soft layer of the surface layer to transform to ferrite and for reducing the variation of hardness. If the temperature is 700° C. or more, since the ferrite transformation is delayed, the surface layer cannot be ferrite. If 500° C. or less, part of the surface layer becomes low temperature transformed structures. If there are a plurality of structures like ferrite and low temperature transformed structures, since this causes variation of hardness of the surface layer, the holding temperature is 500° C. or more. The holding time is 3 seconds or more. To make the ferrite transformation of the surface layer proceed sufficiently, the sheet has to be held for 3 seconds or more. More preferably the holding time is 5 seconds or more, more preferably 10 seconds or more.


The coiling temperature is the temperature of the bainite transformation temperature region of the matrix steel sheet, i.e., the temperature of the martensite transformation start temperature Ms to the bainite transformation start temperature Bs of the matrix steel sheet. This is so as to cause the formation of bainite or martensite in the matrix steel sheet to obtain high strength steel and further to stabilize the retained austenite. In this way, by changing the timings of transformation of the matrix steel sheet and the surface layer-use steel sheet, structures with small variations in hardness are obtained in the surface layer. This is one of the features of the present invention. In the present invention, the martensite transformation start temperature Ms and bainite transformation start temperature Bs are calculated by the following formulas:


Bs (° C.)=820−290C/(1−Sf)−37Si−90Mn−65Cr−50Ni+70A1


Ms (° C.)=541−474C/(1−Sf)−15Si−35Mn−17Cr−17Ni+19A1


where, C, Si, Mn, Cr, Ni, and Al are the contents (mass %) of the elements of the matrix steel sheet, while Sf is the area percent of ferrite in the matrix steel sheet.


It is difficult to find the area percent of ferrite during the manufacture of steel sheet, so in the present invention, in calculating Bs and Ms, a sample of the cold rolled sheet before entering the annealing step is taken and annealed by the same temperature history as the annealing step. The area percent of the ferrite found is used.


Next, the method for obtaining cold rolled steel sheet among the high strength steel sheets encompassed by the present invention will be explained. The method for producing the cold rolled steel sheet is characterized by comprising:


superposing on one or both surfaces of a matrix steel sheet having a chemical composition explained above and forming a middle part in sheet thickness a surface layer-use steel sheet having a chemical composition similarly explained above and forming a soft surface layer to form a double-layer steel sheet,


heating the double-layer steel sheet by a heating temperature of 1100° C. or more and 1350° C. or less, more preferably more than 1150° C. and 1350° C. or less, then hot rolling and cold rolling it, wherein the hot rolling comprises rough rolling and finish rolling at a finishing temperature of 800 to 980° C., the rough rolling is performed two times or more under conditions of a rough rolling temperature of 1100° C. or more, a sheet thickness reduction rate per pass of 5% or more and less than 50%, and a time between passes of 3 seconds or more, and


holding the rolled double-layer steel sheet at a temperature of the Ac3 point of the surface layer-use steel sheet minus 50° C. or more and the Ac3 point of the matrix steel sheet minus 50° C. or more and 900° C. or less for 5 seconds or more, then cooling from 750° C. to 550° C. or less by an average cooling rate of 2.5° C./s or more,


where





Ac3=910−203√C+44.7Si−30Mn+700P−20Cu−15.2Ni−11Cr+31.5Mo+400Ti+104V+400A1  (formula 1)


where C, Si, Mn, P, Cu, Ni, Cr Mo, Ti, V, and Al are contents (mass %) of the elements.


Further, if making elements diffuse between the matrix steel sheet and the surface layer-use steel sheet and forming between the two a hardness transition zone with an average hardness change in the sheet thickness direction of 5000 (ΔHv/mm) or less, preferably the above double-layer steel sheet is heated to the heating temperature of 1100° C. or more and 1350° C. or less or more than 1150° C. and 1350° C. or less for 2 hours or more then is hot rolled and cold rolled.


Further, the method preferably includes making the retained austenite of the middle part in sheet thickness in the high strength steel sheet an area percent of 10% or more to improve the ductility of the high strength steel sheet and annealing the rolled double-layer steel sheet by running it through a continuous annealing line instead of the steps after cold rolling prescribed above. The annealing at the continuous annealing line preferably includes, first, holding the double-layer steel sheet at a heating temperature of 700° C. or more and 900° C. or less for 5 seconds or more,


then, optionally, preliminarily cooling the double-layer steel sheet so that it remains from the heating temperature to a preliminary cooling stop temperature of the Bs point of the matrix steel sheet to less than the Ac3 point minus 20° C. for 5 seconds or more and less than 400 seconds,


then cooling the double-layer steel sheet to the cooling stop temperature of the Ms of the matrix steel sheet minus 100° C. to less than Bs by an average cooling rate of 10° C./s or more, and


then making the double-layer steel sheet stop in the temperature region of the Ms of the matrix steel sheet minus 100° C. or more for 30 seconds to 600 seconds.





Ac3 (° C.)=910−203√C+44.7Si−30Mn+700P−20Cu−15.2Ni−11Cr+31.5Mo+400Ti+104V+400A1  (formula 1)





Bs (° C.)=820−290C/(1−Sf)−37Si−90Mn−65Cr−50Ni+70A1  (formula 2)





Ms (° C.)=541−474C/(1−Sf)−15Si−35Mn−17Cr−17Ni+19A1  (formula 3)


where, C, Si, Mn, P, Cu, Ni, Cr, Mo, Ti, V, and Al are the contents (mass %) of the elements of the matrix steel sheet, while Sf is the area percent of ferrite in the matrix steel sheet.


Explaining the steps in more detail, first, the double-layer steel sheet fabricated by the above method, as explained in the method for producing hot rolled steel sheet, is heated to a heating temperature of 1100° C. or more and 1350° C. or less or more than 1150° C. and 1350° C. or less, then is hot rolled and, for example, is coiled at a coiling temperature of 20° C. or more and 700° C. or less. Next, the thus produced hot rolled steel sheet is pickled. The pickling is for removing the oxides on the surface of the hot rolled steel sheet and may be performed one time or may he performed divided into several times. When forming a hardness transition zone, preferably, first, the double-layer steel sheet is heated to a heating temperature of 1100° C. or more 1350° C. or less or more than 1150° C. and 1350° C. or less for 2 hours or more. This is so as to make elements diffuse between the matrix steel sheet and the surface layer-use steel sheet during heating and to make the average hardness changeof the hardness transition zone formed between the two smaller. If the heating time is shorter than 2 hours, the average hardness change of the hardness transition zone will not become sufficiently small. Next, the thus produced hot rolled steel sheet is pickled. The pickling is for removing the oxides on the surface of the hot rolled steel sheet and may be performed one time or may be performed divided into several times.


In the cold rolling, if the total of the rolling reduction is more than 85%, the ductility of the matrix steel sheet is lost and during cold rolling, the danger of the matrix steel sheet fracturing rises, so the total of the rolling reduction is preferably 85% or less. On the other hand, to sufficiently proceed with recrystallization of the soft layer in the annealing step, the total of the rolling reduction is preferably 20% or more, more preferably 30% or more. For the purpose of lowering the cold rolling load before cold rolling, the sheet may be annealed at a temperature of 700° C. or less.


Next, the annealing will be explained. In the annealing as well, to reduce the variation of hardness of the soft surface layer, it is important to make the majority of the structures at the soft surface layer low temperature transformed structures and suppress ferrite transformation and pearlite transformation. If the chemical composition of the surface layer-use steel sheet satisfies the above suitable range, the entirety of the soft surface layer is low temperature transformed structures and there is no concern of the average Vickers hardness of the soft surface layer becoming higher than 0.90 time the average Vickers hardness of the 1/2 position in sheet thickness.


The sheet is held at a temperature of the Ac3 point of the surface layer-use steel sheet minus 50° C. or more and the Ac3 point of the matrix steel sheet minus 50° C. or more and 900° C. or less for 5 seconds or more. The reason for making the temperature the Ac3 point of the matrix steel sheet minus 50° C. or more is that by heating the matrix steel sheet to the dual-phase region of ferrite and austenite or the single-phase region of austenite, subsequent heat treatment enables transformed structures to be obtained and the necessary strength to be obtained. With a temperature lower than this, the strength remarkably falls. The reason for making the temperature the Ac3 point of the surface layer-use steel sheet minus 50° C. or more is that by heating the surface layer to the dual-phase region of ferrite and austenite or the single-phase region of austenite, subsequent heat treatment enables the majority of the sheet to be low temperature transformed structures and the variation of hardness to be reduced. With a temperature lower than this, the variation of hardness becomes greater. If heating to 900° C. or more, the former γ grain size of the hard layer becomes coarser and the toughness deteriorates, so this is not preferable.


After that, the sheet is cooled from 750° C. to 550° C. or less by an average cooling rate of 2.5° C./s or more. This is an important condition in the present invention. The step is necessary for making the majority of the soft surface layer low temperature transformed structures and reducing the variation of hardness. If the average cooling rate is slower than 2.5° C./s, ferrite transformation and pearlite transformation occur at the soft surface layer and cause a variation of hardness. More preferably, the rate is 5° C./s or more, more preferably 10° C./s or more. With a temperature higher than 750° C., it is difficult for ferrite transformation or pearlite transformation to occur, so the average cooling rate is not prescribed. With a temperature lower than 550° C., the structures transform to low temperature transformed structures, so the average cooling rate is not prescribed.


At 550° C. or less, the sheet may be cooled down to room temperature by a certain cooling rate. By holding this at a temperature of 200° C. to 550° C. or so, the bainite transformation can be promoted and the martensite can be tempered. However, if holding at 300° C. to 550° C. for a long time, there is a possibility of the strength falling, so if holding at this temperature, the holding time is preferably 600 seconds or less.


To make the retained austenite at the middle part in sheet thickness in the high strength steel sheet an area percent of 10% or more and improve the ductility of the high strength steel sheet, instead of the annealing and cooling explained above, the following annealing and cooling are preferably performed. First, in the annealing, the sheet is heated to 700° C. or more and 900° C. or less and held there for 5 seconds or more. The reason for making the temperature 700° C. or more is to make the recrystallization of the softened layer sufficiently proceed so as to lower the nonrecrystallized fraction and reduce the variation of hardness. With a temperature lower than 700° C., the variation of hardness of the softened layer becomes greater. If heating to 900° C. or more, the former γ grain size of the hard layer coarsens and the toughness deteriorates, so this is not preferred. The sheet has to be held at the heating temperature for 5 seconds or more. If the holding time is 5 seconds or less, the austenite transformation of the matrix steel sheet does not sufficiently proceed and the strength remarkably drops. Further, the softened layer becomes insufficiently recrystallized and the variation of hardness of the surface layer becomes greater. From these viewpoints, the holding time is preferably 10 seconds or more. Still more preferably it is 20 seconds or more.


The annealing, for example, is performed by running the rolled double-layer steel sheet through a continuous annealing line. Here, “annealing through a continuous annealing line” includes, first, holding the double-layer steel sheet at a heating temperature of 700° C. or more and 900° C. or less for 5 seconds or more, then optionally preliminarily cooling the double-layer steel sheet from the heating temperature so that it remains at a preliminary cooling stop temperature of the Bs point of the matrix steel sheet to less than the Ac3 point minus 20° C. for 5 seconds or more and less than 400 seconds. Such a preliminary cooling step may be performed in accordance with need. A subsequent cooling step may also be performed without the preliminary cooling step.


After the optional preliminary cooling step, the annealing on the continuous annealing line includes cooling the double-layer steel sheet until the cooling stop temperature of the Ms of the matrix steel sheet minus 100° C. to less than Bs by an average cooling rate of 10° C./s or more and next making the double-layer steel sheet stop in a temperature region of Ms of the matrix steel sheet minus 100° C. or more, more preferably a temperature region of 300° C. or more and 500° C. or less, for 30 seconds or more and 600 seconds or less. While stopping, the sheet may if necessary be heated and cooled any number of times. To stabilize the retained austenite, this stopping time is important. With the necessary stopping time of less than 30 seconds, it is difficult to obtain 10% or more of retained austenite. On the other hand, if 600 seconds or more, due to the progression of softening in the structures as a whole, sufficient strength becomes difficult to obtain. In the present invention, Ac3, Bs, and Ms are calculated by the following formulas:





Ac3 (° C.)=910−203−√C+44.7Si−30Mn+700P−20Cu−15.2Ni−11Cr+31.5Mo+400Ti+104V+400A1  (formula 1)





Bs (° C.)=820−290C/(1−S0−375i−90Mn−65Cr−50Ni+70A1





Ms (° C.)=541−474C/(1−Sf)−15Si−35Mn−17Cr−17Ni+19A1


where, C, Si, Mn, P, Cu, Ni, Cr, Mo, Ti, V, and Al are the contents (mass %) of the elements of the matrix steel sheet, while Sf is the area percent of ferrite in the matrix steel sheet.


It is difficult to find the area percent of ferrite in steel sheet during production, so in the present invention, in calculating Bs and Ms, a sample of the cold rolled sheet before entering the annealing step is taken and annealed by the same temperature history as the annealing step. The area percent of the ferrite found is used.


After that, when performing hot dip galvanization, the plating bath temperature need only be a condition applied in the past. For example, the condition of 440° C. to 550° C. may be applied. Further, after performing the hot dip galvanization, when heating the steel sheet for alloying to prepare hot dip galvannealed steel sheet, the heating temperature of the alloying in that case need only be a condition applied in the past. For example, the condition of 400° C. to 600° C. may be applied. The heating system of alloying is not particularly limited. It is possible to use direct heating by combustion gas, induction heating, direct electrical heating, or another heating system corresponding to the hot dip coating facility from the past.


After the alloying treatment, the steel sheet is cooled to 200° C. or less and if necessary is subjected to skin pass rolling.


When producing electrogalvanized steel sheet, for example, there is the method of performing, as pretreatment for plating, alkali degreasing, rinsing, pickling, and rinsing again, then electrolytically treating the pretreated steel sheet using a solution circulating type electroplating apparatus and using a plating bath comprised of zinc sulfate, sodium sulfate, and sulfuric acid by a current density of 100 A/dm2 or so until reaching a predetermined plating thickness.


Finally, the preferable constituents of the surface layer-use steel sheet will be shown. The steel sheet in the present invention sometimes differs in chemical composition between the soft surface layer and the middle part in sheet thickness. In such a case, the preferable chemical composition in the surface layer-use steel sheet forming the soft surface layer is as follows:


The C content of the surface layer-use steel sheet is preferably 0.30 time or more and 0.90 time or less the C content of the matrix steel sheet. This is so as to lower the hardness of the surface layer-use steel sheet from the hardness of the matrix steel sheet. If greater than 0.90 time, in the finally obtained high strength steel sheet, sometimes the average Vickers hardness of the soft surface layer will not become 0.90 time the average Vickers hardness of the 1/2 position in sheet thickness or less. More preferably, the C content of the surface layer-use steel sheet is 0.85 time or less the C content of the matrix steel sheet, still more preferably 0.80 time or less.


The total of the Mn content, Cr content, and Mo content of the surface layer-use steel sheet is preferably 0.3 time or more the total of the Mn content, Cr content, and Mo content of the matrix steel sheet. If the total of the Mn content, Cr content, and Mo content for raising the hardenability is smaller than 0.3 time the total of the Mn content, Cr content, and Mo content of the matrix steel sheet, it is difficult to form low temperature transformed structures and variation of hardness is caused. More preferably, the total is 0.5 time or more, still more preferably 0.7 time or more.


The B content of the surface layer-use steel sheet is preferably 0.3 time or more the B content of the matrix steel sheet. If the B content for improving the hardenability is smaller than 0.3 time the matrix steel sheet, it is difficult to form low temperature transformed structures and variation of hardness is caused. More preferably, the B content is 0.5 time or more, still more preferably 0.7 time or more.


The total of the Cu content and Ni content of the surface layer-use steel sheet is preferably 0.3 time or more the total of the Cu content and Ni content of the matrix steel sheet. If the total of the Cu content and Ni content for improving the hardenability is smaller than 0.3 time the total of the Cu content and Ni content of the matrix steel sheet, it is difficult to form low temperature transformed structures and variation of hardness is caused. More preferably, the total is 0.5 time or more, still more preferably 0.7 time or more.


The surface layer-use steel sheet may contain, in addition to the above elements, Si, P, S, Al, N, Cr, B, Ti, Nb, V, Cu, Ni, 0, W, Ta, Sn, Sb, As, Mg, Ca, Y, Zr, La, and Ce. The preferable ranges of composition of the above elements are similar to the preferable ranges of the middle part in sheet thickness.


Next, the method of identification of the steel structures according to the present invention will be explained. Steel structures can be identified by observing the cross-section of the steel sheet parallel to the rolling direction and thickness direction and/or the cross-section vertical to the rolling direction by a power of 500× to 10000×. For example, a sample of the steel sheet is cut out, then the surface polished to a mirror finish by machine polishing, then a Nital reagent is used to reveal the steel structures. After that, the steel structures at the region of a depth from the surface of about 1/2 of the thickness of the steel sheet are examined using a scanning electron microscope (SEM). Due to this, it is possible to measure the area percent of ferrite of the matrix steel sheet. Further, in the present invention, the area percent of the retained austenite at the middle part in sheet thickness is determined as follows by X-ray measurement. First, the part from the surface of the steel sheet down to 1/2 of the thickness of the steel sheet is ground away by mechanical polishing and chemical polishing. The chemically polished surface is measured using MoKα (rays as the characteristic X rays. Further, from the integrated intensity ratio of the diffraction peaks of (200) and (211) of the body centered cubic lattice (bcc) phases and (200), (220), and (311) of the face centered cubic lattice (fcc) phases, the following formula is used to calculate the area percent of retained austenite at the middle part in sheet thickness:






Sγ(1200f+I220f+I311f)/(I200b+I211b)×100


(Sγ indicates the area percent of retained austenite at the middle part in sheet thickness, I200f, I220f, and I311f indicate the intensities of the diffraction peaks of (200), (220), and (311) of the fcc phases, and I200b and I211b indicate the intensities of the diffraction peaks of (200) and (211) of the bcc phases.)


EXAMPLES

In the examples, the finished products obtained were tested by a Vickers hardness test, nano-hardness test, tensile test, V-bending test, and bending load test.


The average Vickers hardness was determined as follows: First, at intervals of 5% of sheet thickness in the sheet thickness direction from the 1/2 position of sheet thickness toward the surface, the Vickers hardnesses at certain positions in the sheet thickness direction were measured by an indentation load of 100 g. Next, the Vickers hardnesses of a total of five points were measured by an indentation load of 100 g in the same way from that position in the direction vertical to sheet thickness on a line parallel to the rolling direction. The average value of these was determined as the average Vickers hardness at that position in the sheet thickness direction. The intervals of the measurement points aligned in the sheet thickness direction and rolling direction were distances of 4 times or more the indents. When the average Vickers hardness at a certain sheet thickness direction position becomes 0.90 time or less the average Vickers hardness at the similarly measured 1/2 position of sheet thickness, the surface side from that position is defined as the “soft surface layer”. The average Vickers hardness of the soft surface layer as a whole was found by measuring the Vickers hardness randomly at 10 points in the thus defined soft surface layer and obtaining the average of these.


Further, the method prescribed in the Description was used to find the thickness of the soft surface layer and determine the ratio to the sheet thickness. Similarly, the method prescribed in the Description was used to determine the value of the average hardness change in the sheet thickness direction of the hardness transition zone.


The nano-hardness of the soft surface layer was measured at the 1/2 position of thickness of the soft surface layer from the surface at 100 points in the direction vertical to sheet thickness. The standard deviation of these values was determined as the nano-hardness standard deviation of the soft surface layer.


The tensile strength TS and elongation (%) were measured in accordance with JIS Z 2241 by preparing a No. 5 test piece described in JIS Z 2201 having a long axis in a direction perpendicular to the rolling direction.


Further, the limit curvature radius R is found by preparing a No. I test piece described in JIS Z2204 so that the direction vertical to the rolling direction becomes the longitudinal direction) (bending ridgeline matching rolling direction). A V-bending test was performed based on JIS Z2248. A sample having a soft surface layer at only one surface was bent so that the surface having the soft surface layer became the outside of the bend. The angle of the die and punch was 60° while the radius of the front end of the punch was changed by units of 0.5 mm in the bending test. The radius of the front end of the punch at which bending was possible without cracks being caused was found as the “limit curvature radius R”.


Further, the bending load test was performed by obtaining a 60 mm×60 mm test piece from the steel sheet, performing a bending test based on the standard 238-100 of the German


Association of the Automotive Industry (VDA) under conditions of a punch curvature of 0.4 mm, a roll size of 30 mm, a distance between rolls of 2×sheet thickness+0.5 (mm), and a maximum indentation stroke of 11 mm and measuring the maximum load (N) at that time. In this example, a sheet with a bending load (N) of more than 3000 times the sheet thickness (mm) was deemed “passing”.


Example A

A continuously cast slab of a thickness of 20 mm having each of the chemical compositions shown in Table 1 (matrix steel sheet) was ground at its surfaces to remove surface oxides, then was superposed with a surface layer-use steel sheet having the chemical composition shown in Table 1 at one surface or both surfaces by arc welding. The ratio of the thickness of the surface layer-use steel sheet to the sheet thickness was as shown in “ratio of surface layer-use steel sheet (one side) (%)” of Table 1. This was hot rolled under conditions of a heating temperature, finishing temperature, and coiling temperature shown in Table 2 to obtain a multilayer hot rolled steel sheet. In the case of a test material having the hot rolled steel sheet as the finished product, the holding time at 700° C. to 500° C. in the hot rolling was intentionally controlled to the value shown in Table 2. If having a cold rolled steel sheet as the finished product, after that, the sheet was pickled, cold rolled by 50%, and annealed under the conditions shown in Table 2.


When the obtained products were measured for chemical compositions at positions of 2% of the sheet thickness from the surface layer and for chemical compositions at 1/2 positions of sheet thickness, there were substantially no changes from the chemical compositions of the matrix steel sheets and steel sheets for surface layer use shown in Table 1.










TABLE 1







Steel
Matrix steel sheet (mass %)






















type
C
Si
Mn
S
P
Al
N
Cr
Mo
B
Ti
Nb
V
Cu
Ni





a
0.310
1.10
2.10
0.001
0.001


b
0.510
2.00
2.00
0.002
0.001


c
0.790
0.90
0.50
0.001
0.001


d
0.310
2.42
2.00
0.002
0.002


e
0.400
0.10
8.00
0.002
0.002


f
0.400
0.10
2.00
0.002
0.002


1.00
1.00
0.002


g
0.490
0.50
3.10
0.001
0.001





0.100
0.100
0.10


h
0.510
0.60
3.00
0.001
0.001








0.10
0.10


i
0.300
0.60
3.10
0.001
0.001


j
0.290
0.60
1.00
0.001
0.001


k
0.310
0.60
0.30
0.001
0.001




0.001


l
0.300
0.60
0.30
0.001
0.001









0.10











Steel
Surface layer-use steel sheet (mass %)






















type
C
Si
Mn
S
P
Al
N
Cr
Mo
B
Ti
Nb
V
Cu
Ni





a
0.200
1.05
1.5
0.001
0.002


b
0.400
0.05
1.6
0.002
0.001


c
0.400
0.95
0.3
0.002
0.002


d
0.250
1.55
1.3
0.001
0.001


e
0.330
1.50
6.0
0.002
0.010


f
0.300
0.50
1.5
0.002
0.010


0.40
0.40
0.001


g
0.400
1.45
2.0
0.002
0.010





0.450
0.450
0.40


h
0.360
1.50
2.1
0.001
0.010








0.06
0.06


i
0.350
0.45
2.0
0.001
0.001


j
0.200
0.45
0.1
0.002
0.001


k
0.200
0.45
0.3
0.002
0.001


l
0.250
0.55
0.3
0.001
0.001















Ratio of surface layer-use steel sheet to matrix steel sheet
Ratio of surface layer-use
Matrix steel
Surface layer-use














Steel type
C
Mn + Cr + Mo
B
Cu + Ni
steel sheet (one side) (%)
sheet Ac3 (° C.)
steel sheet Ac3 (° C.)





a
0.6
0.7


25
783
821


b
0.8
0.8


15
794
736


c
0.5
0.6


15
755
815


d
0.8
0.7


15
845
839


e
0.8
0.8


15
546
680


f
0.8
0.6
0.33

15
747
784


g
0.8
0.6


15
668
648


h
0.7
0.7

0.6
15
698
790


i
1.2
0.6


15
733
750


j
0.7
0.1


15
798
836


k
0.6
1.0
0.00

15
815
830


l
0.8
1.0

0  
15
815
824





* Empty fields show elements not intentionally added
















TABLE 2









Hot rolling conditions
Annealing conditions

























Heating
Rough
Sheet thickness
Time

Finishing
750° C. to 550° C.
Coiling
Heating

750° C. to 550° C.




Steel

temp.
rolling
reduction rate
between
Rolling
temp.
average cooling
temp.
temp.
Holding
average cooling


Class
No.
type
Steel sheet
(° C.)
temp. (° C.)
per pass (%)
passes (s)
operations
(° C.)
rate (° C./s)
(° C.)
(° C.)
time (s)
rate (° C./s)





Inv. ex.
1
a
Hot rolled steel sheet
1250
1160
20
5
5
900
 5
450





Inv. ex.
2
a
Cold rolled steel sheet
1250
1130
30
3
2
900

450
850
120
10


Inv. ex.
3
b
Hot rolled steel sheet
1200
1140
23
5
5
890
 5
180





Comp. ex.
4
b
Hot rolled steel sheet
1200
1160
22
5
3
890
 1
200





Inv. ex.
5
b
Cold rolled steel sheet
1150
1140
35
8
5
930

600
830
130
15


Comp. ex.
6
b
Cold rolled steel sheet
1150
1130
11
8
5
930

550
650
 10
20


Comp. ex.
7
b
Cold rolled steel sheet
1150
1100
39
7
4
930

550
750
 5
 1


Inv. ex.
8
b
Cold rolled steel sheet
1150
1120
23
9
4
930

550
820
 10
30


Comp. ex.
9
b
Cold rolled steel sheet
1150
1110
39
3
5
930

650
830
 2
200 


Inv. ex.
10
b
Hot dip galvanized steel sheet
1100
1100
41
5
3
920

600
830
120
20


Inv. ex.
11
b
Hot dip galvannealed steel sheet
1100
1100
15
9
4
920

600
830
120
20


Inv. ex.
12
b
Electrogalvanized steel sheet
1100
1100
43
3
3
920

600
830
120
20


Inv. ex.
13
c
Hot rolled steel sheet
1250
1190
34
4
3
900
10
300





Inv. ex.
14
c
Cold rolled steel sheet
1100
1100
27
9
5
930

600
880
 10
 3


Inv. ex.
15
d
Hot rolled steel sheet
1150
1140
36
7
4
930
20
200





Inv. ex.
16
d
Cold rolled steel sheet
1100
1100
31
6
4
930

600
880
 30
 6


Inv. ex.
17
e
Hot rolled steel sheet
1350
1140
44
5
4
930
30
100





Inv. ex.
18
e
Cold rolled steel sheet
1350
1130
44
7
2
920

600
890
 60
10


Inv. ex.
19
f
Hot rolled steel sheet
1100
1100
13
4
3
920
40
150





Inv. ex.
20
f
Cold rolled steel sheet
1100
1100
21
6
4
920

650
880
 90
15


Inv. ex.
21
g
Hot rolled steel sheet
1150
1100
45
5
2
920
30
50





Inv. ex.
22
g
Cold rolled steel sheet
1100
1100
36
7
5
930

650
880
150
30


Inv. ex.
23
h
Hot rolled steel sheet
1150
1140
19
8
5
930
30
400





Inv. ex.
24
h
Cold rolled steel sheet
1100
1100
45
7
3
920

650
890
250
55


Comp. ex.
25
i
Hot rolled steel sheet
1150
1120
41
9
2
920
30
150





Comp. ex.
26
i
Cold rolled steel sheet
1100
1100
25
3
4
920

600
890
300
50


Comp. ex.
27
j
Hot rolled steel sheet
1150
1100
4
4
8
930
20
250





Comp. ex.
28
j
Cold rolled steel sheet
1100
1100
25
2
3
930

600
890
230
20


Inv. ex.
29
c
Hot rolled steel sheet
1200
1160
14
10
2
910
20
200





Inv. ex.
30
c
Cold rolled steel sheet
1200
1180
22
7
2
920

600
890
 20
 8


Inv. ex.
31
d
Hot rolled steel sheet
1200
1110
23
8
5
910
20
100





Inv. ex.
32
d
Cold rolled steel sheet
1200
1140
20
3
4
920

600
890
 30
 6


Inv. ex.
33
e
Hot rolled steel sheet
1200
1130
45
8
3
910
20
100





Inv. ex.
34
e
Cold rolled steel sheet
1200
1140
41
8
3
920

600
890
 60
15


Inv. ex.
35
f
Hot rolled steel sheet
1200
1160
19
8
2
910
40
100





Inv. ex.
36
f
Cold rolled steel sheet
1200
1140
14
10
5
920

600
880
 60
20


Comp. ex.
37
a
Cold rolled steel sheet
1250
1000
35
10
3
900

450
850
120
10


Comp. ex.
38
a
Cold rolled steel sheet
1250
1200
4
5
8
900

450
850
120
10


Comp. ex.
39
a
Cold rolled steel sheet
1250
1200
65
5
1
900

450
850
120
10


Comp. ex.
40
a
Cold rolled steel sheet
1250
1200
35
2
4
900

450
850
120
10


Comp. ex.
41
a
Cold rolled steel sheet
1250
1200
30
4
1
900

450
850
120
10













Hardness














B

Soft surface
Ratio of soft
















A
Soft surface

layer
surface layer
Mechanical properties























Sheet thickness ½
layer average

nano-hardness
(one side) to
Tensile


Sheet






average Vickers
Vickers

standard
sheet thickness
strength
Limit bending
Bending
thickness



Class
No.
hardness (Hv)
hardness (Hv)
B/A
deviation
(%)
(MPa)
radius R (mm)
load (N)
(mm)
Softened part







Inv. ex.
1
590
400
0.68
0.4
23
1710
1
22100
2.4
Both surfaces



Inv. ex.
2
600
390
0.65
0.4
23
1700
1
8000
1.2
Both surfaces



Inv. ex.
3
700
600
0.86
0.5
13
1960
1
34300
2.4
Both surfaces



Comp. ex.
4
700
400
0.57
0.9
13
1650
2.5
22900
2.4
Both surfaces



Inv. ex.
5
700
580
0.83
0.4
13
1950
1.5
8500
1.2
Both surfaces



Comp. ex.
6
590
350
0.59
0.9
13
1600
2.5
9700
1.2
Both surfaces



Comp. ex.
7
650
400
0.62
0.9
13
1570
2.5
10800
1.2
Both surfaces



Inv. ex.
8
710
590
0.83
0.5
13
1960
1.5
8600
1.2
Both surfaces



Comp. ex.
9
580
330
0.57
0.9
13
1560
2.5
6500
1.2
Both surfaces



Inv. ex.
10
690
570
0.83
0.4
13
1880
1
6900
1.2
Both surfaces



Inv. ex.
11
690
580
0.84
0.5
13
1880
1
11700
1.2
Both surfaces



Inv. ex.
12
700
570
0.81
0.5
13
1890
1
9200
1.2
Both surfaces



Inv. ex.
13
750
500
0.67
0.5
13
2450
1.5
51500
2.4
Both surfaces



Inv. ex.
14
730
490
0.67
0.5
13
2330
1.5
7100
1.2
Both surfaces



Inv. ex.
15
600
520
0.87
0.4
13
1870
1
39900
2.6
Both surfaces



Inv. ex.
16
590
500
0.85
0.5
13
1850
1
9000
1.2
Both surfaces



Inv. ex.
17
680
530
0.78
0.5
13
1990
1
30200
2.8
Both surfaces



Inv. ex.
18
660
530
0.80
0.5
13
1990
1
17900
1.6
Both surfaces



Inv. ex.
19
680
500
0.74
0.4
13
2010
1.5
23300
2
Both surfaces



Inv. ex.
20
680
470
0.69
0.4
13
2000
1.5
9000
1
Both surfaces



Inv. ex.
21
730
660
0.90
0.6
13
2330
1.5
24300
2.4
Both surfaces



Inv. ex.
22
720
650
0.90
0.6
13
2320
1.5
12600
1.6
Both surfaces



Inv. ex.
23
770
550
0.71
0.7
13
2320
1.5
37700
2.8
Both surfaces



Inv. ex.
24
750
560
0.75
0.7
13
2330
1.5
6200
0.8
Both surfaces














Hardness














B

Soft surface
Ratio of soft
















A
Soft surface

layer
surface layer
Mechanical properties























Sheet thickness ½
layer average

nano-hardness
part (one side) to
Tensile


Sheet






average Vickers
Vickers

standard
sheet thickness
strength
Limit bending
Bending
thickness



Class
No.
hardness (Hv)
hardness (Hv)
B/A
deviation
(%)
(MPa)
radius R (mm)
load (N)
(mm)
Softened part







Comp. ex.
25
590
690
1.17
0.9
13
2150
2.5
39200
2.4
Both surfaces



Comp. ex.
26
590
680
1.15
0.9
13
2150
2.5
12600
1.6
Both surfaces



Comp. ex.
27
590
450
0.76
0.9
13
1960
2.5
22100
2.4
Both surfaces



Comp. ex.
28
590
440
0.75
0.9
13
1950
2.5
9500
1.6
Both surfaces



Inv. ex.
29
750
500
0.67
0.5
13
2520
1.5
52000
2.4
One surface



Inv. ex.
30
740
500
0.68
0.5
13
2470
1.5
21000
1.6
One surface



Inv. ex.
31
610
520
0.85
0.4
13
1980
1
22200
2.4
One surface



Inv. ex.
32
590
510
0.86
0.5
13
1970
1
12800
1.6
One surface



Inv. ex.
33
680
520
0.76
0.5
13
2060
1
28700
2.4
One surface



Inv. ex.
34
670
530
0.79
0.5
13
2050
1
12900
1.6
One surface



Inv. ex.
35
690
520
0.75
0.4
13
2100
1.5
24900
2.4
One surface



Inv. ex.
36
680
490
0.72
0.4
13
2080
1.5
12900
1.6
One surface



Comp. ex.
37
590
370
0.63
0.9
10
1730
2.5
2800
1.2
Both surfaces



Comp. ex.
38
590
370
0.63
0.9
10
1720
2.5
3300
1.2
Both surfaces



Comp. ex.
39
590
370
0.63
0.9
10
1740
3
3100
1.2
Both surfaces



Comp. ex.
40
590
370
0.63
0.9
10
1710
2.5
1600
1.2
Both surfaces



Comp. ex.
41
590
370
0.63
0.9
10
1720
2.5
3300
1.2
Both surfaces










If referring to Table 2, for example, in the steel sheets of Comparative Examples 7, 27, and 28, it is learned that the requirement of the average Vickers hardness of the soft surface layer being more than 0.60 time and 0.90 time or less the average Vickers hardness of the 1/2 position in sheet thickness was satisfied, but the nano-hardness standard deviation of the soft surface layer was 0.9, i.e., the requirement of being 0.8 or less was not satisfied. As a result, in the steel sheets of these comparative examples, the limit curvature radius R was 2.5 mm. In contrast to this, in the steel sheets in the invention examples of the present invention satisfying the two requirements, the limit curvature radius R was less than 2 mm, in particular, was 1.5 mm or 1 mm. For this reason, it was learned that by suppressing the variation of hardness of the soft surface layer to within a specific range, it is possible to remarkably improve the bendability of the steel sheet compared with steel sheet just combining a middle part in sheet thickness and a soft surface layer softer than the same.


Further, if referring to the hot rolled steel sheet of Comparative Example 4, if making the holding time at 750° C. to 550° C. in the cooling process after hot rolling 1 second, the average Vickers hardness of the soft surface layer was 0.57 time the average Vickers hardness of the 1/2 position in sheet thickness, the nano-hardness standard deviation of the soft surface layer was 0.9, and the limit curvature radius R was 2.5 mm. In contrast to this, in the hot rolled steel sheet of Invention Example 3 prepared in the same way as Comparative Example 4 except for making the holding time 5 seconds and the coiling temperature 180° C., the average Vickers hardness of the soft surface layer was 0.86 time the average Vickers hardness of the 1/2 position in sheet thickness, the nano-hardness standard deviation of the soft surface layer was 0.5, and the limit curvature radius R was 1 mm.


Further, if referring to the cold rolled steel sheets of Invention Examples 5 and 8, it was learned that by holding at the Ac3 point of the surface layer-use steel sheet minus 50° C. or more and the Ac3 point of the matrix steel sheet minus 50° C. or more and a temperature of 900° C. or less for 5 seconds or more and suitably selecting the temperature, the holding time, and the average cooling rate at the time of annealing so as to satisfy the requirement of cooling from 750° C. to 550° C. or less by an average cooling rate of 2.5° C./s or more, it is possible to suppress variation of hardness of the soft surface layer (nano-hardness standard deviation of soft surface layer: 0.4 or 0.5) and as a result to remarkably improve the bendability of the cold rolled steel sheet (limit curvature radius R of 1.5 mm). On the other hand, in the cold rolled steel sheets of Comparative Examples 6, 7, and 9 not satisfying the above requirement, the nano-hardness standard deviation of the soft surface layer was 0.9 and the limit curvature radius R was 2.5 mm.


Further, in steel sheet manufactured by hot rolling without rough rolling being performed two times or more under conditions of a rough rolling temperature of 1100° C. or more, a sheet thickness reduction rate per pass of 5% to less than 50%, and a time between passes of 3 seconds or more, the limit curvature radius R was high and/or the bending load was low and a sufficient bendability could not be achieved.


Example B
Formation of Hardness Transition Zone

A continuously cast slab of a thickness of 20 mm having each of the chemical compositions shown in Table 3 (matrix steel sheet) was ground at its surfaces to remove surface oxides, then was superposed with surface layer-use steel sheet having the chemical compositions shown in Table 1 at one surface or both surfaces by arc welding. The ratio of the thickness of the surface layer-use steel sheet to the sheet thickness was as shown in “ratio of surface layer-use steel sheet (one side) (%)” of Table 3. This was hot rolled under conditions of a heating temperature, heating time, finishing temperature, and coiling temperature shown in Table 4 to obtain a multilayer hot rolled steel sheet. In the case of a test material having the hot rolled steel sheet as the finished product, the average cooling rate of hot rolling from 750° C. to 550° C. was intentionally controlled to the value shown in Table 4. If having a cold rolled steel sheet as the finished product, after that, the sheet was pickled, cold rolled by 50%, and annealed under the conditions shown in Table 4.


When the obtained products were measured for chemical compositions at positions of 2% of the sheet thickness from the surface layer and chemical compositions at 1/2 positions of sheet thickness, there were substantially no changes from the chemical compositions of the matrix steel sheets and steel sheets for surface layer use shown in Table 3.










TABLE 3







Steel
Matrix steel sheet (mass %)






















type
C
Si
Mn
S
P
Al
N
Cr
Mo
B
Ti
Nb
V
Cu
Ni





a′
0.310
1.10
2.10
0.001
0.001


b′
0.510
2.00
2.00
0.002
0.001


c′
0.790
0.90
0.50
0.001
0.001


d′
0.310
2.42
2.00
0.002
0.002


e′
0.400
0.10
8.00
0.002
0.002


f′
0.400
0.10
2.00
0.002
0.002


1.00
1.00
0.002


g′
0.490
0.50
3.10
0.001
0.001





0.100
0.100
0.10


h′
0.510
0.60
3.00
0.001
0.001








0.10
0.10


i′
0.300
0.60
3.10
0.001
0.001


j′
0.290
0.60
1.00
0.001
0.001


k′
0.310
0.60
0.30
0.001
0.001




0.001


l′
0.300
0.60
0.30
0.001
0.001









0.10











Steel
Surface layer-use steel sheet (mass %)






















type
C
Si
Mn
S
P
Al
N
Cr
Mo
B
Ti
Nb
V
Cu
Ni





a′
0.200
1.05
1.5
0.001
0.002


b′
0.400
0.05
1.6
0.002
0.001


c′
0.400
0.95
0.3
0.002
0.002


d′
0.250
1.55
1.3
0.001
0.001


e′
0.330
1.50
6.0
0.002
0.010


f′
0.300
0.50
1.5
0.002
0.010


0.40
0.40
0.001


g′
0.400
1.45
2.0
0.002
0.010





0.450
0.450
0.40


h′
0.360
1.50
2.1
0.001
0.010








0.06
0.06


i′
0.350
0.45
2.0
0.001
0.001


j′
0.200
0.45
0.1
0.002
0.001


k′
0.200
0.45
0.3
0.002
0.001


l′
0.250
0.55
0.3
0.001
0.001















Ratio of matrix steel sheet to surface layer-use steel sheet
Ratio of surface layer-use
Matrix steel
Surface layer-use














Steel type
C
Mn + Cr + Mo
B
Cu + Ni
steel sheet (one side) (%)
sheet Ac3 (° C.)
steel sheet Ac3 (° C.)





a′
0.6
0.7


25
783
821


b′
0.8
0.8


15
794
736


c′
0.5
0.6


15
755
815


d′
0.8
0.7


15
845
839


e′
0.8
0.8


15
546
680


f′
0.8
0.6
0.33

15
747
784


g′
0.8
0.6


15
668
648


h′
0.7
0.7

0.6
15
698
790


i′
1.2
0.6


15
733
750


j′
0.7
0.1


15
798
836


k′
0.6
1.0
0.00

15
815
830


l′
0.8
1.0

0  
15
815
824





* Empty fields show elements not intentionally added.
















TABLE 4









Hot rolling conditions
Annealing conditions


























Heating
Heating
Rough
Sheet thickness
Time

Finishing
750° C. to 550° C.
Coiling
Heating

750° C. to 550° C.




Steel

temp.
time
rolling
reduction rate
between
Rolling
temp.
average cooling
temp.
temp.
Holding
average cooling


Class
No.
type
Steel sheet
(° C.)
(min)
temp. (° C.)
per pass (%)
passes (s)
operations
(° C.)
rate (° C./s)
(° C.)
(° C.)
time (s)
rate (° C./s)





Inv. ex.
101
a′
Hot rolled steel sheet
1250
120
1160
20
5
5
900
 5
450





Inv. ex.
102
a′
Cold rolled steel sheet
1250
120
1130
30
3
2
900

450
850
120
10


Inv. ex.
103
b′
Hot rolled steel sheet
1200
150
1140
23
5
5
890
 5
180





Comp. ex.
104
b′
Hot rolled steel sheet
1200
150
1160
22
5
3
890
 1
200





Inv. ex.
105
b′
Cold rolled steel sheet
1150
150
1140
35
8
5
930

600
830
130
15


Comp. ex.
106
b′
Cold rolled steel sheet
1150
150
1130
11
8
5
930

550
650
 10
20


Comp. ex.
107
b′
Cold rolled steel sheet
1150
150
1100
39
7
4
930

550
750
 5
 1


Inv. ex.
108
b′
Cold rolled steel sheet
1150
150
1120
23
9
4
930

550
820
 10
30


Comp. ex.
109
b′
Cold rolled steel sheet
1150
150
1110
39
3
5
930

650
830
 2
200 


Inv. ex.
110
b′
Cold rolled steel sheet
1150
100
1110
22
7
2
930

650
830
 10
200 


Inv. ex.
111
b′
Hot dip galvanized steel sheet
1100
150
1100
41
5
3
920

600
830
120
20


Inv. ex.
112
b′
Hot dip galvannealed steel sheet
1100
150
1100
15
9
4
920

600
830
120
20


Inv. ex.
113
b′
Electrogalvanized steel sheet
1100
150
1100
43
3
3
920

600
830
120
20


Inv. ex.
114
c′
Hot rolled steel sheet
1250
150
1190
34
4
3
900
10
300





Inv. ex.
115
c′
Cold rolled steel sheet
1100
150
1100
27
9
5
930

600
880
 10
 3


Inv. ex.
116
d′
Hot rolled steel sheet
1150
150
1140
36
7
4
930
20
200





Inv. ex.
117
d′
Cold rolled steel sheet
1100
300
1100
31
6
4
930

600
880
 30
 6


Inv. ex.
118
e′
Hot rolled steel sheet
1350
300
1140
44
5
4
930
30
100





Inv. ex.
119
e′
Cold rolled steel sheet
1350
300
1130
44
7
2
920

600
890
 60
10


Inv. ex.
120
f′
Hot rolled steel sheet
1100
300
1100
13
4
3
920
40
150





Inv. ex.
121
f′
Cold rolled steel sheet
1100
300
1100
21
6
4
920

650
880
 90
15


Inv. ex.
122
g′
Hot rolled steel sheet
1150
300
1100
45
5
2
920
30
50





Inv. ex.
123
g′
Cold rolled steel sheet
1100
300
1100
36
7
5
930

650
880
150
30


Inv. ex.
124
h′
Hot rolled steel sheet
1150
300
1140
19
8
5
930
30
400





Inv. ex.
125
h′
Cold rolled steel sheet
1100
300
1100
45
7
3
920

650
890
250
55


Comp. ex.
126
i′
Hot rolled steel sheet
1150
300
1120
41
9
2
920
30
150





Comp. ex.
127
i′
Cold rolled steel sheet
1100
300
1100
25
3
4
920

600
890
300
50


Comp. ex.
128
j′
Hot rolled steel sheet
1150
300
1100
4
4
8
930
20
250





Comp. ex.
129
j′
Cold rolled steel sheet
1100
300
1100
25
2
3
930

600
890
230
20


Inv. ex.
130
c′
Hot rolled steel sheet
1200
200
1160
14
10
2
910
20
200





Inv. ex.
131
c′
Cold rolled steel sheet
1200
200
1180
22
7
2
920

600
890
 20
 8


Inv. ex.
132
d′
Hot rolled steel sheet
1200
200
1110
23
8
5
910
20
100





Inv. ex.
133
d′
Cold rolled steel sheet
1200
200
1140
20
3
4
920

600
890
 30
 6


Inv. ex.
134
e′
Hot rolled steel sheet
1200
200
1130
45
8
3
910
20
100





Inv. ex.
135
e′
Cold rolled steel sheet
1200
150
1140
41
8
3
920

600
890
 60
15


Inv. ex.
136
f′
Hot rolled steel sheet
1200
150
1160
19
8
2
910
40
100





Inv. ex.
137
f′
Cold rolled steel sheet
1200
150
1140
14
10
5
920

600
880
 60
20


Comp. ex.
138
a′
Cold rolled steel sheet
1250
120
1000
35
10
3
900

450
850
120
10


Comp. ex.
139
a′
Cold rolled steel sheet
1250
120
1200
4
5
8
900

450
850
120
10


Comp. ex.
140
a′
Cold rolled steel sheet
1250
120
1200
65
5
1
900

450
850
120
10


Comp. ex.
141
a′
Cold rolled steel sheet
1250
120
1200
35
2
4
900

450
850
120
10


Comp. ex.
142
a′
Cold rolled steel sheet
1250
120
1200
30
4
1
900

450
850
120
10













Hardness















B

Soft surface

Ratio of soft

















A
Soft surface

layer
Average hardness
surface layer
Mechanical properties






















Sheet thickness ½
layer average

nano-hardness
change of hardness
(one side) to
Tensile

Bending
Sheet





average Vickers
Vickers

standard
transition zone
sheet thickness
strength
Limit bending
load
thickness


Class
No.
hardness (Hv)
hardness (Hv)
B/A
deviation
(ΔHv/mm)
(%)
(MPa)
radius R (mm)
(N)
(mm)
Softened part





Inv. ex.
101
580
380
0.66
0.4
833
20
1700
1
29900
2.4
Both surfaces


Inv. ex.
102
590
370
0.63
0.4
917
20
1690
1
9300
1.2
Both surfaces


Inv. ex.
103
690
600
0.87
0.5
621
10
1960
1
31200
2.4
Both surfaces


Comp. ex.
104
690
390
0.57
0.9
1250
10
1680
2.5
20600
2.4
Both surfaces


Inv. ex.
105
700
570
0.81
0.4
1000
10
1930
1
6400
1.2
Both surfaces


Comp. ex.
106
590
330
0.56
0.9
2000
10
1600
2.5
8100
1.2
Both surfaces


Comp. ex.
107
650
410
0.63
0.9
2083
10
1580
2.5
9200
1.2
Both surfaces


Inv. ex.
108
700
580
0.83
0.5
1000
10
1940
1
9000
1.2
Both surfaces


Comp. ex.
109
580
320
0.55
0.9
2083
10
1560
2.5
7000
1.2
Both surfaces


Inv. ex.
110
680
550
0.81
0.5
5015
14
1560
1.5
6900
1.2
Both surfaces


Inv. ex.
111
680
570
0.84
0.4
1000
10
1870
1
8600
1.2
Both surfaces


Inv. ex.
112
690
570
0.83
0.5
917
10
1870
1
8600
1.2
Both surfaces


Inv. ex.
113
690
570
0.83
0.5
1083
10
1880
1
8200
1.2
Both surfaces


Inv. ex.
114
740
490
0.66
0.5
1041
10
2450
1
37900
2.4
Both surfaces


Inv. ex.
115
730
480
0.66
0.5
2000
10
2330
1
14300
1.2
Both surfaces


Inv. ex.
116
590
510
0.86
0.4
385
10
1860
1
32200
2.6
Both surfaces


Inv. ex.
117
580
500
0.86
0.5
672
10
1850
1
6700
1.2
Both surfaces


Inv. ex.
118
660
520
0.79
0.5
500
10
1970
1
25800
2.8
Both surfaces


Inv. ex.
119
640
520
0.81
0.5
750
10
1960
1
12200
1.6
Both surfaces


Inv. ex.
120
670
490
0.73
0.4
905
10
2010
1
28800
2
Both surfaces


Inv. ex.
121
680
460
0.68
0.4
2210
10
1990
1
6300
1
Both surfaces


Inv. ex.
122
710
670
0.94
0.6
168
10
2300
1
27400
2.4
Both surfaces


Inv. ex.
123
710
650
0.92
0.6
376
10
2290
1
20800
1.6
Both surfaces


Inv. ex.
124
760
550
0.72
0.7
793
10
2320
1
43500
2.8
Both surfaces


Inv. ex.
125
740
550
0.74
0.7
2375
10
2320
1
4100
0.8
Both surfaces


Comp. ex.
126
590
680
1.15
0.9

10
2140
2.5
24200
2.4
Both surfaces


Comp. ex.
127
580
680
1.17
0.9

10
2140
2.5
20600
1.6
Both surfaces


Comp. ex.
128
590
400
0.68
0.9
791
10
1940
2.5
18800
2.4
Both surfaces


Comp. ex.
129
590
400
0.68
0.9
1187
10
1930
2.5
11500
1.6
Both surfaces


Inv. ex.
130
740
500
0.68
0.5
1000
10
2510
1
28400
2.4
One surface


Inv. ex.
131
740
490
0.66
0.5
1562
10
2460
1
14000
1.6
One surface


Inv. ex.
132
600
510
0.85
0.4
375
10
1970
1
21000
2.4
One surface


Inv. ex.
133
580
510
0.88
0.5
148
10
1970
1
13400
1.6
One surface


Inv. ex.
134
680
520
0.76
0.5
333
10
2050
1
23900
2.4
One surface


Inv. ex.
135
670
520
0.78
0.5
937
10
2050
1
13300
1.6
One surface


Inv. ex.
136
680
510
0.75
0.4
542
10
2100
1
23100
2.4
One surface


Inv. ex.
137
670
490
0.73
0.4
792
10
2070
1
16400
1.6
One surface


Comp. ex.
138
590
370
0.63
0.9
5300
10
1730
2.5
2200
1.2
Both surfaces


Comp. ex.
139
590
370
0.63
0.9
5200
10
1720
2.5
2100
1.2
Both surfaces


Comp. ex.
140
590
370
0.63
0.9
5400
10
1740
3
3200
1.2
Both surfaces


Comp. ex.
141
590
370
0.63
0.9
5100
10
1710
2.5
2500
1.2
Both surfaces


Comp. ex.
142
590
370
0.63
0.9
5200
10
1720
2.5
3100
1.2
Both surfaces









If referring to Table 4, for example, in the steel sheets of Comparative Examples 107, 128, and 129, the requirement of the average Vickers hardness of the soft surface layer being more than 0.60 time and 0.90 time or less the average Vickers hardness of the 1/2 position in sheet thickness was satisfied and further the requirement of the average hardness change in the sheet thickness direction of the hardness transition zone being 5000 (ΔHv/mm) or less was satisfied, but it was learned that the nano-hardness standard deviation of the soft surface layer was 0.9, i.e., the requirement of being 0.8 or less was not satisfied. As a result, in the steel sheets of these comparative examples, the limit curvature radius R was 2.5 mm. On the other hand, in Invention Example 110, the requirement of the average Vickers hardness of the soft surface layer being more than 0.60 time and 0.90 time or less the average Vickers hardness of the 1/2 position in sheet thickness was satisfied and further the requirement of the nano-hardness standard deviation of the soft surface layer being 0.8 or less was satisfied, but it was learned that the average hardness change in the sheet thickness direction of the hardness transition zone was 5015 (ΔHv/mm), i.e., more than 5000 (ΔHv/mm). As a result, in the steel sheet of Invention Example 110, the limit curvature radius R was 1.5 mm. In contrast to this, in the steel sheets in the invention examples satisfying the two requirements of “the average Vickers hardness of the soft surface layer being more than 0.60 time and 0.90 time or less the average Vickers hardness of the 1/2 position in sheet thickness” and “the nano-hardness standard deviation of the soft surface layer being 0.8 or less” and having “the average hardness change in the sheet thickness direction of the hardness transition zone of 5000 (ΔHv/mm) or less”, the limit curvature radius R was 1 mm. For this reason, it was learned that by controlling both the variation of hardness of the soft surface layer and the average hardness change in the sheet thickness direction of the hardness transition zone to within specific ranges, it is possible to remarkably improve the bendability of the steel sheet compared with steel sheet just combining a middle part in sheet thickness and a soft surface layer softer than the same in which only one of the variation of hardness of the soft surface layer and the average hardness change in the sheet thickness direction of the hardness transition zone is controlled to within a specific range.


Further, if referring to the hot rolled steel sheet of Comparative Example 104, if making the holding time at 750° C. to 550° C. in the cooling process after hot rolling 1 second, the nano-hardness standard deviation of the soft surface layer was 0.9 and the limit curvature radius R was 2.5 mm. In contrast to this, in the hot rolled steel sheet of Invention Example 103 prepared in the same way as Comparative Example 104 except for making the holding time 5 seconds and the coiling temperature 180° C. the nano-hardness standard deviation of the soft surface layer was 0.5 and the limit curvature radius R was 1 mm.


Further, if referring to the cold rolled steel sheets of Invention Examples 105 and 108, it was learned that by suitably selecting the temperature, the holding time, and the average cooling rate at the time of annealing so as to satisfy the requirement of holding at the Ac3 point of the surface layer-use steel sheet minus 50° C. or more and the Ac3 point of the matrix steel sheet minus 50° C. or more and a temperature of 900° C. or less for 5 seconds or more and cooling from 750° C. to 550° C. or less by an average cooling rate of 2.5° C./s or more, it is possible to suppress variation of hardness of the soft surface layer (nano-hardness standard deviation of soft surface layer: 0.4 or 0.5) and as a result to remarkably improve the bendability of the cold rolled steel sheet (limit curvature radius R of 1 mm). On the other hand, in the cold rolled steel sheets of Comparative Examples 106, 107, and 109 not satisfying the above requirements, the nano-hardness standard deviation of the soft surface layer was 0.9 and the limit curvature radius R was 2.5 mm.


Further, in steel sheet manufactured by hot rolling without rough rolling being performed two times or more under conditions of a rough rolling temperature of 1100° C. or more, a sheet thickness reduction rate per pass of 5% to less than 50%, and a time between passes of 3 seconds or more, the limit curvature radius R was high and/or the bending load was low and a sufficient bendability could not be achieved.


Example C
Formation of Middle Part in Sheet Thickness Comprising, by Area Percent, 10% or More of Retained Austenite

A continuously cast slab of a thickness of 20 mm having each of the chemical compositions shown in Table 5 (matrix steel sheet) was ground at its surfaces to remove surface oxides, then was superposed with surface layer-use steel sheet having the chemical compositions shown in Table 5 at one surface or both surfaces by arc welding. This was hot rolled under conditions of a heating temperature, finishing temperature, and coiling temperature shown in Table 6 to obtain a multilayer hot rolled steel sheet. In the case of a test material having the hot rolled steel sheet as the finished product, the holding time at the 700° C. to 500° C. of hot rolling was intentionally controlled to the value shown in Table 6. If having a cold rolled steel sheet as the finished product, after that, the sheet was pickled, cold rolled by the cold rolling rate shown in Table 6, and further annealed under the conditions shown in Table 6.


When the obtained products were measured for chemical compositions at positions of 2% of the sheet thickness from the surface layer and for chemical compositions at 1/2 positions of sheet thickness, there were substantially no changes from the chemical compositions of the matrix steel sheets and steel sheets for surface layer use shown in Table 6.











TABLE 5









Matrix steel sheet (mass %)























Steel type
C
Si
Mn
S
P
Al
N
Cr
Mo
B
Ti
Nb
V
Cu
Ni
REM





A
0.05
0.8
2.10
0.001
0.02


B
0.10
1.4
2.00
0.002
0.03


C
0.15
1.8
2.1
0.04
0.01


D
0.20
1.5
2
0.03
0.03


E
0.35
1.9
2.60
0.001
0.05


F
0.45
1.9
2.80
0.002
0.01


G
0.62
2.2
3.10
0.002
0.03


H
0.78
2.3
2.00
0.002
0.02









0.10


I
0.15
0.4
3.10
0.001
0.02








0.05


J
0.17
1.2
3.10
0.001
0.04


K
0.14
1.5
1.00
0.001
0.02


L
0.24
2.2
2.00
0.001
0.02


M
0.18
2.5
2.00
0.001
0.01


N
0.18
1.5
0.5
0.002
0.06


O
0.15
1.6
1.2
0.01
0.04


P
0.14
1.4
1.8
0.01
0.03


Q
0.16
1.8
2.5
0.02
0.01


R
0.17
1.7
3.8
0.03
0.01


U
0.61
2.4
3.7
0.05
0.03


0.5







0.01


V
0.41
2.3
4
0.04
0.01


1


W
0.21
2.1
3.4
0.01
0.01



0.5


X
0.3
2.1
3
0.03
0.01



1


Y
0.41
1.7
3.4
0.01
0.01




0.002




0.3


Z
0.58
2
3.9
0.02
0.01





0.03


0.1


AA
0.6
2.4
2
0.01
0.02


0.3



0.03

0.2
0.1


AB
0.19
2.5
2.8
0.01
0.01



0.05

0.02

0.02


AC
0.54
1.6
3.2
0.02
0.01







0.06


AD
0.18
1.6
3.9
0.02
0.01


0.2
0.1
0.01
0.02
0.02



0.03


AE
0.02
1.2
2
0.001
0.02


AF
0.15
0.2
2
0.001
0.02


AG
0.15
1.2
0.005
0.001
0.02


AH
0.15
1.2
2
0.001
0.2


AI
0.1
1.2
2
0.001
0.02


AJ
0.15
1.8
2.1
0.04
0.01



0.5
0.002


AK
0.15
1.3
2.5
0.001
0.02





0.02


AL
0.15
1.5
3
0.001
0.02






0.02












Surface layer-use steel sheet (mass %)























Steel type
C
Si
Mn
S
P
Al
N
Cr
Mo
B
Ti
Nb
V
Cu
Ni
REM





A
0.04
1.32
1.7
0.001
0.001


B
0.07
0.50
1.5
0.001
0.001


0.100


C
0.12
1.28
1.5
0.002
0.001



0.050


D
0.13
0.53
1.5
0.001
0.001


E
0.09
1.83
2.1
0.001
0.005





0.02


F
0.07
1.36
1.8
0.002
0.010






0.02


G
0.09
1.43
2.3
0.002
0.010







0.02


H
0.03
1.52
1.7
0.002
0.010








0.01


I
0.08
0.57
2.0
0.002
0.010









0.01


J
0.11
1.60
2.7
0.001
0.005


0.2
0.1

0.02


K
0.03
1.48
0.8
0.001
0.005





0.01
0.02


L
0.07
0.69
1.7
0.001
0.005


M
0.01
0.52
1.6
0.001
0.005







0.03


N
0.11
0.51
0.4
0.001
0.005


O
0.13
1.28
1.0
0.002
0.001





0.04


P
0.02
1.92
1.3
0.001
0.001


Q
0.05
1.41
2.0
0.001
0.005






0.03


R
0.04
0.87
2.7
0.002
0.010




0.0014


U
0.04
1.25
2.5
0.002
0.005


V
0.15
0.99
2.8
0.001
0.005






0.01
0.02


W
0.02
0.83
2.0
0.001
0.005




0.0008
0.01

0.02


X
0.07
1.19
2.2
0.001
0.001


Y
0.02
0.77
2.7
0.002
0.001


1


Z
0.01
1.76
3.1
0.001
0.001



1


AA
0.10
1.69
1.8
0.002
0.005








0.08


AB
0.10
0.66
1.9
0.001
0.010


AC
0.00
0.57
2.4
0.001
0.010


AD
0.13
1.76
2.4
0.002
0.02


AE
0.01
0.50
1.6
0.001
0.001


AF
0.07
0.50
1.3
0.001
0.001


AG
0.07
0.50
0.01
0.001
0.001


AH
0.07
0.50
1.4
0.001
0.001


AI
0.07
0.50
1.2


AJ
0.04
1.32
1.7
0.001
0.001










0.02


AK
0.04
1.32
2.0
0.001
0.001


AL
0.04
1.32
1.9
0.001
0.001










0.03



















TABLE 6









Hot rolling conditions























Rough
Sheet thickness
Time




Cold rolling





Heating
rolling
reduction rate
between
Rolling
Finishing
700° C. to 500° C.
Coiling
Cold rolling


Class
No.
Steel
temp. (° C.)
temp. (° C.)
per pass (%)
passes (s)
operations
temp. (° C.)
holding time (s)
temp. (° C.)
rate (%)





Inv. ex.
201
A
1166
1160
32
5
2
827
3
480



Inv. ex.
202
B
1110
1100
34
7
3
840
10
539



Inv. ex.
203
C
1115
1110
25
7
2
854
16
481



Inv. ex.
204
D
1170
1150
24
10
3
850
28
447



Inv. ex.
205
E
1172
1130
10
7
4
852
42
330



Inv. ex.
206
F
1120
1100
31
4
3
845

640
23


Inv. ex.
207
G
1220
1180
43
6
3
878

660
45


Inv. ex.
208
H
1160
1105
10
7
3
844

510
66


Inv. ex.
209
I
1238
1160
16
4
4
828

420
62


Inv. ex.
210
J
1245
1190
16
5
4
854

680
65


Inv. ex.
211
K
1152
1110
42
9
4
860

270
72


Inv. ex.
212
L
1253
1190
20
5
4
843

480
34


Inv. ex.
213
M
1116
1110
17
10
2
886

680
23


Inv. ex.
214
N
1126
1115
29
4
2
835

490
29


Inv. ex.
215
O
1112
1110
42
4
3
893

490
35


Inv. ex.
216
P
1201
1150
42
10
3
872

580
62


Inv. ex.
217
Q
1233
1140
16
8
3
862

620
76


Inv. ex.
218
R
1257
1100
44
7
4
887

360
47


Inv. ex.
219
U
1214
1180
13
10
3
887

500
62


Inv. ex.
220
V
1116
1110
31
5
5
896

640
60


Inv. ex.
221
W
1252
1100
39
8
2
862

390
23


Inv. ex.
222
X
1248
1170
23
10
3
822

470
31


Inv. ex.
223
Y
1203
1130
29
5
3
882

530
48


Inv. ex.
224
Z
1121
1120
34
3
4
855

540
79


Inv. ex.
225
AA
1126
1110
34
6
3
869

450
50


Inv. ex.
226
AA
1212
1200
18
10
3
892

320
65


Inv. ex.
227
AA
1249
1150
34
4
5
841

590
72


Inv. ex.
228
AA
1151
1100
15
7
3
850

450
64


Inv. ex.
229
AA
1157
1150
41
7
3
871

320
30


Inv. ex.
230
AA
1109
1100
13
6
2
845

380
60


Inv. ex.
231
AA
1107
1100
12
6
2
860

390
50


Inv. ex.
232
AA
1131
1100
28
5
2
889

540
71


Inv. ex.
233
AA
1121
1110
13
7
3
829

390
35


Inv. ex.
234
AB
1123
1120
41
9
4
860

390
27


Inv. ex.
235
AB
1219
1190
16
4
5
827

550
60


Inv. ex.
236
AB
1193
1180
18
10
5
892

360
67


Inv. ex.
237
AC
1166
1150
30
9
5
892

390
67


Inv. ex.
238
AC
1231
1110
36
5
5
845

520
43


Inv. ex.
239
AD
1120
1100
12
10
4
845

580
79


Inv. ex.
240
AD
1219
1180
14
5
3
827

550
60


Inv. ex.
241
AD
1193
1100
40
9
5
892

360
67


Comp. ex.
242
AE
1241
1160
16
9
2
882

541
59


Inv. ex.
243
AF
1226
1100
32
8
5
889

567
49


Comp. ex.
244
AG
1257
1190
25
6
3
893

589
47


Comp. ex.
245
AH
1244
1140
14
7
2
879

541
62


Comp. ex.
246
AI
1215
1160
43
6
3
862

528
59















Comp. ex.
247
AJ
1000
1000
31
4
3
Sheet fractured during hot rolling, so subsequent tests not possible
















Comp. ex.
248
AK
1200
1100
14
6
2
760
Due to shape defects of hot rolled sheet, subsequent tests not possible


















Comp. ex.
249
AL
1250
1190
22
4
5
850

560
5


Comp. ex.
250
AL
1250
1160
23
7
2
850

560
95


Comp. ex.
251
AL
1250
1110
36
6
2
850

560
45


Inv. ex.
252
AL
1250
1170
28
7
4
850

560
50


Comp. ex.
253
AL
1250
1110
29
8
4
850

560
45


Inv. ex.
254
AL
1250
1180
31
7
5
850

560
45


Inv. ex.
255
AL
1250
1190
23
4
4
850

560
45


Inv. ex.
256
AL
1250
1180
28
3
3
850

560
45


Comp. ex.
257
AL
1250
1160
31
8
2
850

560
45


Comp. ex.
258
AL
1250
1000
35
10
3
850

560
45


Comp. ex.
259
AL
1250
1200
4
5
8
850

560
45


Comp. ex.
260
AL
1250
1200
65
5
1
850

560
45


Comp. ex.
261
AL
1250
1200
35
2
4
850

560
45


Comp. ex.
262
AL
1250
1200
30
4
1
850

560
45

















Annealing conditions



























Stopping time









Heating

Preliminary
during

Cooling

Stopping time


















temp.
Holding
cooling stop
preliminary
Cooling
stop temp.
300° C. to 500° C.
at Ms-100° C.
Plating























Class
No.
(° C.)
time (s)
temp. (° C.)
cooling (s)
rate (° C./s)
(° C.)
stopping time (s)
or more (s)
Plating
Alloying
Sf (%)
Bs
Ms
Ac3





Inv. ex.
201










11
585
429
900


Inv. ex.
202










16
554
394
908


Inv. ex.
203










23
508
348
912


Inv. ex.
204










28
504
317
886


Inv. ex.
205










36
357
162
875


Inv. ex.
206
810
43
None
None
18
223
148
158
None
None
32
306
101
859


Inv. ex.
207
823
94
None
None
18
207
233
248
None
None
0
280
106
848


Inv. ex.
208
832
62
None
None
42
207
220
240
None
None
0
324
65
832


Inv. ex.
209
730
28
None
None
25
386
250
262
None
None
64
405
229
849


Inv. ex.
210
780
133
None
None
38
354
305
315
Yes
Yes
44
408
270
880


Inv. ex.
211
800
32
None
None
36
483
133
163
None
None
17
626
404
901


Inv. ex.
212
840
171
None
None
40
419
275
295
None
None
0
489
324
909


Inv. ex.
213
890
70
None
None
45
464
289
305
None
None
0
495
348
936


Inv. ex.
214
825
5
None
None
29
402
195
205
None
None
16
657
399
891


Inv. ex.
215
821
30
None
None
35
280
223
234
None
None
38
583
360
903


Inv. ex.
216
838
100
None
None
34
513
235
260
None
None
43
534
340
897


Inv. ex.
217
859
230
None
None
25
379
250
257
None
None
35
457
310
909


Inv. ex.
218
856
128
730
5
22
254
333
339
None
None
51
314
218
902


Inv. ex.
219
845
40
650
6
14
163
203
215
None
None
0
189
78
859


Inv. ex.
220
839
170
650
15 
26
105
335
355
None
None
32
135
64
883


Inv. ex.
221
828
147
None
None
10
309
284
301
Yes
None
45
325
209
927


Inv. ex.
222
826
165
None
None
20
265
141
169
None
None
52
292
109
924


Inv. ex.
223
856
91
None
None
50
200
230
255
None
None
27
273
125
851


Inv. ex.
224
838
84
None
None
80
191
201
229
None
None
12
204
62
845


Inv. ex.
225
838
89
None
None
100
200
212
239
None
None
30
281
23
859


Inv. ex.
226
856
133
None
None
25
144
188
204
None
None
21
309
69
859


Inv. ex.
227
827
43
None
None
44
184
323
349
None
None
18
317
82
859


Inv. ex.
228
850
85
None
None
41
202
238
256
None
None
1
353
141
859


Inv. ex.
229
837
12
None
None
18
224
263
263
None
None
7
341
122
859


Inv. ex.
230
845
44
None
None
11
254
123
123
None
None
16
322
90
859


Inv. ex.
231
830
58
None
None
42
284
265
265
None
None
16
322
90
859


Inv. ex.
232
833
146
None
None
28
250
337
337
None
None
30
279
20
859


Inv. ex.
233
832
106
None
None
37
80
253
282
None
None
32
275
13
859


Inv. ex.
234
821
96
None
None
39
230
313
318
None
None
68
305
126
937


Inv. ex.
235
855
98
None
None
14
150
137
153
None
None
48
370
233
937


Inv. ex.
236
827
96
None
None
35
293
186
201
None
None
64
321
154
937


Inv. ex.
237
851
70
None
None
10
233
304
304
None
None
0
316
149
839


Inv. ex.
238
835
101
None
None
35
233
190
190
None
None
3
311
140
839


Inv. ex.
239
854
171
None
None
22
270
125
125
None
None
27
326
261
899


Inv. ex.
240
828
51
None
None
10
250
146
176
Yes
None
42
307
230
899


Inv. ex.
241
859
68
None
None
38
324
173
253
Yes
Yes
24
328
265
899


Comp. ex.
242
835
80
None
None
19
447
340
349
None
None
50
584
434
935


Inv. ex.
243
859
60
None
None
30
387
282
297
None
None
0
589
397
840


Comp. ex.
244
859
68
None
None
24
377
132
138
None
None
20
721
434
885


Comp. ex.
245
849
39
None
None
19
386
172
197
None
None
24
538
359
885


Comp. ex.
246
849
69
None
None
26
382
214
246
None
None
31
554
384
899









Comp. ex.
247
Sheet fractured during hot rolling, so subsequent tests not possible


Comp. ex.
248
Due to shape defects of hot rolled sheet, subsequent tests not possible


Comp. ex.
249
Due to shape defects of cold rolled sheet, subsequent tests not possible


Comp. ex.
250
Due to excessive cold rolling load, cold rolling not possible






















Comp. ex.
251
680
60
None
None
30
300
300
315
None
None
100
None
None
898


Inv. ex.
252
800
2
None
None
30
250
50
213
None
None
30
432
312
898


Comp. ex.
253
800
60
None
None
1
280
315
356
None
None
50
408
271
898


Inv. ex.
254
800
60
None
None
20
235
0
0
None
None
30
432
312
898


Inv. ex.
255
800
60
None
None
20
260
3
3
None
None
30
432
312
898


Inv. ex.
256
800
60
None
None
20
260
15
25
None
None
30
432
312
898


Comp. ex.
257
800
60
None
None
20
260
20
1050
None
None
30
432
312
898


Comp. ex.
258
800
60
None
None
20
235
0
150
None
None
30
432
312
898


Comp. ex.
259
800
60
None
None
20
235
0
150
None
None
30
432
312
898


Comp. ex.
260
800
60
None
None
20
235
0
150
None
None
30
432
312
898


Comp. ex.
261
800
60
None
None
20
235
0
150
None
None
30
432
312
898


Comp. ex.
262
800
60
None
None
20
235
0
150
None
None
30
432
312
898













Sheet thickness

























Middle




A
B

Soft surface









part
Soft surface

Ratio of soft

Sheet
Soft surface

layer



Limit




in sheet
layer
Position of
surface layer
Total
thickness ½
layer average

nano-hardness

Tensile

bending




thickness
(one side)
soft surface
(one side) to
thickness
average Vickers
Vickers

standard

strength
Elongation
radius R
Bending


Class
No.
(mm)
(mm)
layer
sheet thickness (%)
(mm)
hardness (Hv)
hardness (Hv)
B/A
deviation
(%)
(MPa)
(%)
(mm)
load (N)





Inv. ex.
201
2.0
0.3
Both surfaces
12
2.6
289
253
0.87
0.3
10
910
15
1.5
37800


Inv. ex.
202
2.5
0.3
One surface
11
2.8
305
270
0.89
0.3
10
963
16
1.5
42600


Inv. ex.
203
2.4
0.4
Both surfaces
13
3.2
329
294
0.89
0.3
12
1037
19
1.5
43700


Inv. ex.
204
2.8
0.4
Both surfaces
11
3.6
351
299
0.85
0.5
15
1104
25
1.5
52300


Inv. ex.
205
1.8
0.3
Both surfaces
13
2.4
409
279
0.68
0.6
13
1249
23
1.5
19200


Inv. ex.
206
2.6
0.25
Both surfaces
8
3.1
440
270
0.61
0.7
13
1361
25
1.0
50600


Inv. ex.
207
2.9
0.3
Both surfaces
9
3.5
486
299
0.61
0.3
14
1494
17
1.0
128200


Inv. ex.
208
1.6
0.3
Both surfaces
14
2.2
452
276
0.61
0.7
13
1545
17
1.5
43700


Inv. ex.
209
2.1
0.5
Both surfaces
16
3.1
385
275
0.72
0.4
14
1164
30
1.5
90500


Inv. ex.
210
1.9
0.35
Both surfaces
13
2.6
348
288
0.83
0.6
17
1083
31
1.0
37600


Inv. ex.
211
1.9
0.35
Both surfaces
13
2.6
332
247
0.74
0.5
13
1022
19
1.5
22300


Inv. ex.
212
3.0
0.15
One surface
5
3.2
379
270
0.71
0.5
15
1182
20
1.5
55800


Inv. ex.
213
2.6
0.35
Both surfaces
11
3.3
343
236
0.69
0.5
16
1056
21
1.5
18500


Inv. ex.
214
2.8
0.45
Both surfaces
12
3.7
333
289
0.87
0.7
13
1045
19
1.5
53200


Inv. ex.
215
2.3
0.25
Both surfaces
9
2.8
325
287
0.88
0.6
13
1032
24
1.5
56600


Inv. ex.
216
3.0
0.25
Both surfaces
7
3.5
314
242
0.77
0.6
14
988
25
1.5
109600


Inv. ex.
217
2.3
0.3
Both surfaces
10
2.9
324
261
0.81
0.3
14
1012
25
1.5
20200


Inv. ex.
218
2.9
0.45
Both surfaces
12
3.8
328
255
0.78
0.7
18
1018
36
1.0
106800


Inv. ex.
219
1.6
0.35
Both surfaces
15
2.3
444
269
0.61
0.3
13
1390
24
1.0
29300


Inv. ex.
220
2.0
0.45
Both surfaces
16
2.9
418
309
0.74
0.4
18
1275
36
1.5
18500


Inv. ex.
221
2.5
0.4
Both surfaces
12
3.3
346
241
0.70
0.4
15
1060
29
1.0
102400


Inv. ex.
222
2.4
0.8
One surface
25
3.2
381
269
0.70
0.6
13
1158
25
1.5
37200


Inv. ex.
223
3.0
0.5
Both surfaces
13
4.0
418
256
0.61
0.3
13
1257
22
1.0
70500


Inv. ex.
224
1.8
0.25
Both surfaces
11
2.3
459
278
0.61
0.4
13
1401
20
1.0
14200


Inv. ex.
225
1.7
0.45
Both surfaces
17
2.6
471
286
0.61
0.4
13
1384
23
1.0
40500


Inv. ex.
226
1.7
0.45
Both surfaces
17
2.6
471
286
0.61
0.6
13
1384
23
1.5
26100


Inv. ex.
227
1.7
0.45
Both surfaces
17
2.6
471
286
0.61
0.6
18
1384
35
1.5
43100


Inv. ex.
228
1.7
0.45
Both surfaces
17
2.6
471
286
0.61
0.3
14
1384
18
1.0
42500


Inv. ex.
229
1.7
0.45
Both surfaces
17
2.6
471
286
0.61
0.3
15
1384
21
1.0
79400


Inv. ex.
230
1.7
0.45
Both surfaces
17
2.6
471
286
0.61
0.3
13
1384
19
1.0
44400


Inv. ex.
231
1.7
0.45
Both surfaces
17
2.6
471
286
0.61
0.4
15
1384
26
1.5
47800


Inv. ex.
232
1.7
0.45
Both surfaces
17
2.6
471
286
0.61
0.6
17
1384
30
1.5
46900


Inv. ex.
233
1.7
0.45
Both surfaces
17
2.6
471
286
0.61
0.7
14
1384
24
1.5
23200


Inv. ex.
234
1.9
0.3
Both surfaces
12
2.5
337
287
0.85
0.5
17
1057
36
1.5
59800


Inv. ex.
235
1.9
0.3
Both surfaces
12
2.5
337
287
0.85
0.5
13
1057
25
1.0
21700


Inv. ex.
236
1.9
0.3
Both surfaces
12
2.5
337
287
0.85
0.6
13
1057
28
1.0
32300


Inv. ex.
237
2.8
0.45
Both surfaces
12
3.7
419
258
0.62
0.6
16
1359
23
1.5
97600


Inv. ex.
238
2.8
0.45
Both surfaces
12
3.7
423
256
0.61
0.4
13
1359
17
1.0
58500


Inv. ex.
239
1.9
0.45
Both surfaces
16
2.8
333
287
0.86
0.4
13
1043
21
1.5
40500


Inv. ex.
240
1.9
0.45
Both surfaces
16
2.8
333
287
0.86
0.7
13
1043
24
1.0
41100


Inv. ex.
241
1.9
0.45
Both surfaces
16
2.8
333
287
0.86
0.5
13
1043
20
1.5
15300


Comp. ex.
242
1.7
0.3
Both surfaces
13
2.3
252
236
0.94
0.6
7
798
17
3.0
3700


Inv. ex.
243
2.9
0.45
Both surfaces
12
3.8
319
254
0.80
0.8
8
1000
9
1.0
23300


Comp. ex.
244
1.6
0.5
Both surfaces
19
2.6
199
270
1.36
0.6
13
769
20
3.0
4300


Comp. ex.
245
1.6
0.45
Both surfaces
18
2.5
319
251
0.79
0.9
13
986
20
3.0
6800


Comp. ex.
246
1.6
1.3
One surface
31
4.2
295
269
0.91
0.5
13
917
22
2.5
3500









Comp. ex.
247
Cannot be evaluated






















Comp. ex.
248
















Comp. ex.
249


Comp. ex.
250


Comp. ex.
251
1.6
0.2
Both surfaces
10
2.0
187
178
0.95
0.7
0
766
13
1.0
13300


Inv. ex.
252
1.6
0.2
Both surfaces
10
2.0
315
198
0.63
0.7
4
990
14
1.0
19100


Comp. ex.
253
1.6
0.2
Both surfaces
10
2.0
315
198
0.63
0.9
13
990
27
3.0
4100


Inv. ex.
254
1.6
0.2
Both surfaces
10
2.0
315
198
0.63
0.2
0
990
11
1.0
10900


Inv. ex.
255
1.6
0.2
Both surfaces
10
2.0
315
198
0.63
0.2
3
990
14
1.0
22900


Inv. ex.
256
1.6
0.2
Both surfaces
10
2.0
315
198
0.63
0.5
4
990
13
1.5
10200


Comp. ex.
257
1.6
0.2
Both surfaces
10
2.0
189
176
0.93
0.6
18
709
37
3.0
2300


Comp. ex.
258
1.6
0.2
Both surfaces
10
2.0
320
198
0.62
0.9
13
986
19
2.5
7100


Comp. ex.
259
1.6
0.2
Both surfaces
10
2.0
320
198
0.62
0.9
13
988
18
3.0
8800


Comp. ex.
260
1.6
0.2
Both surfaces
10
2.0
320
198
0.62
0.9
13
1002
20
3.0
6600


Comp. ex.
261
1.6
0.2
Both surfaces
10
2.0
320
198
0.62
0.9
13
996
18
2.5
4800


Comp. ex.
262
1.6
0.2
Both surfaces
10
2.0
320
198
0.62
0.9
13
985
19
2.5
7200









Sheets having a tensile strength of 800 MPa or more, a limit curvature radius R of less than 2 mm, and a bending load (N) of more than 3000 times the sheet thickness (mm) were evaluated as high strength steel sheets excellent in bendability (invention examples in Table 6). Further, sheets having an elongation of 15% or more were evaluated as high strength steel sheets excellent in bendability and ductility (Invention Examples 201 to 241 in Table 6). On the other hand, if even one of the performances of a “tensile strength of 800 MPa or more”, a “limit curvature radius R of less than 2 mm”, and a “bending load (N) of more than 3000 times the sheet thickness (mm)” is not satisfied, the sheet was designated a comparative example.


Further, in steel sheets manufactured by hot rolling without rough rolling being performed two times or more under conditions of a rough rolling temperature of 1100° C. or more, a sheet thickness reduction rate per pass of 5% to less than 50%, and a time between passes of 3 seconds or more, the limit curvature radius R was high and/or the bending load was low and a sufficient bendability could not be achieved.


Example D
Formation of Hardness Transition Zone and Middle Part in Sheet Thickness Comprising, by Area Percent, 10% or More of Retained Austenite

A continuously cast slab of a thickness of 20 mm having each of the chemical compositions shown in Table 7 (matrix steel sheet) was ground at its surfaces to remove surface oxides, then was superposed with surface layer-use steel sheet having the chemical compositions shown in Table 7 at one surface or both surfaces by arc welding. This was hot rolled under conditions of a heating temperature, finishing temperature, and coiling temperature shown in Table 8 to obtain a multilayer hot rolled steel sheet. In the case of a test material having the hot rolled steel sheet as the finished product, the holding time at the 700° C. to 500° C. of hot rolling was intentionally controlled to the value shown in Table 8. If having a cold rolled steel sheet as the finished product, after that, the sheet was pickled, cold rolled by the cold rolling rate shown in Table 8, and further annealed under the conditions shown in Table 8.


When the obtained products were measured for chemical compositions at positions of 2% of the sheet thickness from the surface layer and for chemical compositions at 1/2 positions of sheet thickness, there were substantially no changes from the chemical compositions of the matrix steel sheets and steel sheets for surface layer use shown in Table 7.











TABLE 7









Matrix steel sheet (mass %)























Steel type
C
Si
Mn
S
P
Al
N
Cr
Mo
B
Ti
Nb
V
Cu
Ni
REM





A′
0.05
0.8
2.10
0.001
0.02


B′
0.10
1.4
2.00
0.002
0.03


C′
0.15
1.8
2.1
0.04
0.01


D′
0.20
1.5
2
0.03
0.03


E′
0.35
1.9
2.60
0.001
0.05


F′
0.45
1.9
2.80
0.002
0.01


G′
0.62
2.2
3.10
0.002
0.03


H′
0.78
2.3
2.00
0.002
0.02









0.10


I′
0.15
0.4
3.10
0.001
0.02








0.05


J′
0.17
1.2
3.10
0.001
0.04


K′
0.14
1.5
1.00
0.001
0.02


L′
0.24
2.2
2.00
0.001
0.02


M′
0.18
2.5
2.00
0.001
0.01


N′
0.18
1.5
0.5
0.002
0.06


O′
0.15
1.6
1.2
0.01
0.04


P′
0.14
1.4
1.8
0.01
0.03


Q′
0.16
1.8
2.5
0.02
0.01


R′
0.17
1.7
3.8
0.03
0.01


U′
0.61
2.4
3.7
0.05
0.03


0.5







0.01


V′
0.41
2.3
4
0.04
0.01


1


W′
0.21
2.1
3.4
0.01
0.01



0.5


X′
0.3
2.1
3
0.03
0.01



1


Y′
0.41
1.7
3.4
0.01
0.01




0.002




0.3


Z′
0.58
2
3.9
0.02
0.01





0.03


0.1


AA′
0.6
2.4
2
0.01
0.02


0.3



0.03

0.2
0.1


AB′
0.19
2.5
2.8
0.01
0.01



0.05

0.02

0.02


AC′
0.54
1.6
3.2
0.02
0.01







0.06


AD′
0.18
1.6
3.9
0.02
0.01


0.2
0.1
0.01
0.02
0.02



0.03


AE′
0.02
1.2
2
0.001
0.02


AF′
0.15
0.2
2
0.001
0.02


AG′
0.15
1.2
0.005
0.001
0.02


AH′
0.15
1.2
2
0.001
0.2


AI′
0.1
1.2
2
0.001
0.02


AJ′
0.15
1.8
2.1
0.04
0.01



0.5
0.002


AK′
0.15
1.3
2.5
0.001
0.02





0.02


AL′
0.15
1.5
3
0.001
0.02






0.02












Surface layer-use steel sheet (mass %)























Steel type
C
Si
Mn
S
P
Al
N
Cr
Mo
B
Ti
Nb
V
Cu
Ni
REM





A′
0.04
1.32
1.7
0.001
0.001


B′
0.07
0.50
1.5
0.001
0.001


0.100


C′
0.12
1.28
1.5
0.002
0.001



0.050


D′
0.13
0.53
1.5
0.001
0.001


E′
0.09
1.83
2.1
0.001
0.005





0.02


F′
0.07
1.36
1.8
0.002
0.010






0.02


G′
0.09
1.43
2.3
0.002
0.010







0.02


H′
0.03
1.52
1.7
0.002
0.010








0.01


I′
0.08
0.57
2.0
0.002
0.010









0.01


J′
0.11
1.60
2.7
0.001
0.005


0.2
0.1

0.02


K′
0.03
1.48
0.8
0.001
0.005





0.01
0.02


L′
0.07
0.69
1.7
0.001
0.005


M′
0.01
0.52
1.6
0.001
0.005







0.03


N′
0.11
0.51
0.4
0.001
0.005


O′
0.13
1.28
1.0
0.002
0.001





0.04


P′
0.02
1.92
1.3
0.001
0.001


Q′
0.05
1.41
2.0
0.001
0.005






0.03


R′
0.04
0.87
2.7
0.002
0.010




0.0014


U′
0.04
1.25
2.5
0.002
0.005


V′
0.15
0.99
2.8
0.001
0.005






0.01
0.02


W′
0.02
0.83
2.0
0.001
0.005




0.0008
0.01

0.02


X′
0.07
1.19
2.2
0.001
0.001


Y′
0.02
0.77
2.7
0.002
0.001


1


Z′
0.01
1.76
3.1
0.001
0.001



1


AA′
0.10
1.69
1.8
0.002
0.005








0.08


AB′
0.10
0.66
1.9
0.001
0.010


AC′
0.00
0.57
2.4
0.001
0.010


AD′
0.13
1.76
2.4
0.002
0.02


AE′
0.01
0.50
1.6
0.001
0.001


AF′
0.07
0.50
1.3
0.001
0.001


AG′
0.07
0.50
0.0
0.001
0.001


AH′
0.07
0.50
1.4
0.001
0.001


AI′
0.07
0.50
1.2


AJ′
0.04
1.32
1.7
0.001
0.001










0.02


AK′
0.04
1.32
2.0
0.001
0.001


AL′
0.04
1.32
1.9
0.001
0.001










0.03



















TABLE 8









Hot rolling conditions

























Rough
Sheet thickness
Time




Cold rolling





Heating
Heating
rolling
reduction rate
between
Rolling
Finishing
700° C. to 500° C.
Coiling
Cold rolling


Class
No.
Steel
temp. (° C.)
time (min)
temp. (° C.)
per pass (%)
passes (s)
operations
temp. (° C.)
holding time (s)
temp. (° C.)
rate (%)





Inv. ex.
301
A′
1166
200
1160
32
5
2
827
3
480



Inv. ex.
302
B′
1110
200
1100
34
7
3
840
10
539



Inv. ex.
303
C′
1115
120
1110
25
7
2
854
16
481



Inv. ex.
304
D′
1170
200
1150
24
10
3
850
28
447



Inv. ex.
305
E′
1172
120
1130
10
7
4
852
42
330



Inv. ex.
306
F′
1120
150
1100
31
4
3
845

640
23


Inv. ex.
307
G′
1220
200
1180
43
6
3
878

660
45


Inv. ex.
308
H′
1160
200
1105
10
7
3
844

510
66


Inv. ex.
309
I′
1238
150
1160
16
4
4
828

420
62


Inv. ex.
310
J′
1245
200
1190
16
5
4
854

680
65


Inv. ex.
311
K′
1152
150
1110
42
9
4
860

270
72


Inv. ex.
312
L′
1253
150
1190
20
5
4
843

480
34


Inv. ex.
313
M′
1116
120
1110
17
10
2
886

680
23


Inv. ex.
314
N′
1126
200
1115
29
4
2
835

490
29


Inv. ex.
315
O′
1112
150
1110
42
4
3
893

490
35


Inv. ex.
316
P′
1201
150
1150
42
10
3
872

580
62


Inv. ex.
317
Q′
1233
150
1140
16
8
3
862

620
76


Inv. ex.
318
R′
1257
200
1100
44
7
4
887

360
47


Inv. ex.
319
U′
1214
120
1180
13
10
3
887

500
62


Inv. ex.
320
V′
1116
120
1110
31
5
5
896

640
60


Inv. ex.
321
W′
1252
150
1100
39
8
2
862

390
23


Inv. ex.
322
X′
1248
200
1170
23
10
3
822

470
31


Inv. ex.
323
Y′
1203
150
1130
29
5
3
882

530
48


Inv. ex.
324
Z′
1121
120
1120
34
3
4
855

540
79


Inv. ex.
325
AA′
1126
150
1110
34
6
3
869

450
50


Inv. ex.
326
AA′
1212
150
1200
18
10
3
892

320
65


Inv. ex.
327
AA′
1249
120
1150
34
4
5
841

590
72


Inv. ex.
328
AA′
1151
150
1100
15
7
3
850

450
64


Inv. ex.
329
AA′
1157
150
1150
41
7
3
871

320
30


Inv. ex.
330
AA′
1109
120
1100
13
6
2
845

380
60


Inv. ex.
331
AA′
1107
120
1100
12
6
2
860

390
50


Inv. ex.
332
AA′
1131
150
1100
28
5
2
889

540
71


Inv. ex.
333
AA′
1121
200
1110
13
7
3
829

390
35


Inv. ex.
334
AB′
1123
150
1120
41
9
4
860

390
27


Inv. ex.
335
AB′
1219
150
1190
16
4
5
827

550
60


Inv. ex.
336
AB′
1193
150
1180
18
10
5
892

360
67


Inv. ex.
337
AC′
1166
300
1150
30
9
5
892

390
67


Inv. ex.
338
AC′
1231
150
1110
36
5
5
845

520
43


Inv. ex.
339
AD′
1120
200
1100
12
10
4
845

580
79


Inv. ex.
340
AD′
1219
120
1180
14
5
3
827

550
60


Inv. ex.
341
AD′
1193
150
1100
40
9
5
892

360
67


Comp. ex.
342
AE′
1241
120
1160
16
9
2
882

541
59


Inv. ex.
343
AF′
1226
150
1100
32
8
5
889

567
49


Comp. ex.
344
AG′
1257
120
1190
25
6
3
893

589
47


Comp. ex.
345
AH′
1244
300
1140
14
7
2
879

541
62


Comp. ex.
346
AI′
1215
120
1160
43
6
3
862

528
59
















Comp. ex.
347
AJ′
1000
120
1000
31
4
3
Sheet fractured during hot rolling, so subsequent tests not possible

















Comp. ex.
348
AK′
1200
200
1100
14
6
2
760
Due to shape defects of hot rolled sheet, subsequent tests not possible



















Comp. ex.
349
AL′
1250
120
1190
22
4
5
850

560
5


Comp. ex.
350
AL′
1250
120
1160
23
7
2
850

560
95


Comp. ex.
351
AL′
1250
200
1110
36
6
2
850

560
45


Inv. ex.
352
AL′
1250
150
1170
28
7
4
850

560
50


Comp. ex.
353
AL′
1250
150
1110
29
8
4
850

560
45


Inv. ex.
354
AL′
1250
150
1180
31
7
5
850

560
45


Inv. ex.
355
AL′
1250
120
1190
23
4
4
850

560
45


Inv. ex.
356
AL′
1250
120
1180
28
3
3
850

560
45


Comp. ex.
357
AL′
1250
200
1160
31
8
2
850

560
45


Comp. ex.
358
AL′
1250
200
1000
35
10
3
850

560
45


Comp. ex.
359
AL′
1250
150
1200
4
5
8
850

560
45


Comp. ex.
360
AL′
1250
150
1200
65
5
1
850

560
45


Comp. ex.
361
AL′
1250
120
1200
35
2
4
850

560
45


Comp. ex.
362
AL′
1250
200
1200
30
4
1
850

560
45

















Annealing conditions



























Stopping time









Heating

Preliminary
during

Cooling

Stopping time


















temp.
Holding
cooling stop
preliminary
Cooling
stop temp.
300° C. to 500° C.
at Ms-100° C.
Plating























Class
No.
(° C.)
time (s)
temp. (° C.)
cooling (s)
rate (° C./s)
(° C.)
stopping time (s)
or more (s)
Plating
Alloying
Sf (%)
Bs
Ms
Ac3





Inv. ex.
301










11
585
429
900


Inv. ex.
302










16
554
394
908


Inv. ex.
303










23
508
348
912


Inv. ex.
304










28
504
317
886


Inv. ex.
305










36
357
162
875


Inv. ex.
306
810
43
None
None
18
223
148
158
None
None
32
306
101
859


Inv. ex.
307
823
94
None
None
18
207
233
248
None
None
0
280
106
848


Inv. ex.
308
832
62
None
None
42
207
220
240
None
None
0
324
65
832


Inv. ex.
309
730
28
None
None
25
386
250
262
None
None
64
405
229
849


Inv. ex.
310
780
133
None
None
38
354
305
315
Yes
Yes
44
408
270
880


Inv. ex.
311
800
32
None
None
36
483
133
163
None
None
17
626
404
901


Inv. ex.
312
840
171
None
None
40
419
275
295
None
None
0
489
324
909


Inv. ex.
313
890
70
None
None
45
464
289
305
None
None
0
495
348
936


Inv. ex.
314
825
5
None
None
29
402
195
205
None
None
16
657
399
891


Inv. ex.
315
821
30
None
None
35
280
223
234
None
None
38
583
360
903


Inv. ex.
316
838
100
None
None
34
513
235
260
None
None
43
534
340
897


Inv. ex.
317
859
230
None
None
25
379
250
257
None
None
35
457
310
909


Inv. ex.
318
856
128
730
5
22
254
333
339
None
None
51
314
218
902


Inv. ex.
319
845
40
650
6
14
163
203
215
None
None
0
189
78
859


Inv. ex.
320
839
170
650
15 
26
105
335
355
None
None
32
135
64
883


Inv. ex.
321
828
147
None
None
10
309
284
301
Yes
None
45
325
209
927


Inv. ex.
322
826
165
None
None
20
265
141
169
None
None
52
292
109
924


Inv. ex.
323
856
91
None
None
50
200
230
255
None
None
27
273
125
851


Inv. ex.
324
838
84
None
None
80
191
201
229
None
None
12
204
62
845


Inv. ex.
325
838
89
None
None
100
200
212
239
None
None
30
281
23
859


Inv. ex.
326
856
133
None
None
25
144
188
204
None
None
21
309
69
859


Inv. ex.
327
827
43
None
None
44
184
323
349
None
None
18
317
82
859


Inv. ex.
328
850
85
None
None
41
202
238
256
None
None
1
353
141
859


Inv. ex.
329
837
12
None
None
18
224
263
263
None
None
7
341
122
859


Inv. ex.
330
845
44
None
None
11
254
123
123
None
None
16
322
90
859


Inv. ex.
331
830
58
None
None
42
284
265
265
None
None
16
322
90
859


Inv. ex.
332
833
146
None
None
28
250
337
337
None
None
30
279
20
859


Inv. ex.
333
832
106
None
None
37
80
253
282
None
None
32
275
13
859


Inv. ex.
334
821
96
None
None
39
230
313
318
None
None
68
305
126
937


Inv. ex.
335
855
98
None
None
14
150
137
153
None
None
48
370
233
937


Inv. ex.
336
827
96
None
None
35
293
186
201
None
None
64
321
154
937


Inv. ex.
337
851
70
None
None
10
233
304
304
None
None
0
316
149
839


Inv. ex.
338
835
101
None
None
35
233
190
190
None
None
3
311
140
839


Inv. ex.
339
854
171
None
None
22
270
125
125
None
None
27
326
261
899


Inv. ex.
340
828
51
None
None
10
250
146
176
Yes
None
42
307
230
899


Inv. ex.
341
859
68
None
None
38
324
173
253
Yes
Yes
24
328
265
899


Comp. ex.
342
835
80
None
None
19
447
340
349
None
None
50
584
434
935


Inv. ex.
343
859
60
None
None
30
387
282
297
None
None
0
589
397
840


Comp. ex.
344
859
68
None
None
24
377
132
138
None
None
20
721
434
885


Comp. ex.
345
849
39
None
None
19
386
172
197
None
None
24
538
359
885


Comp. ex.
346
849
69
None
None
26
382
214
246
None
None
31
554
384
899









Comp. ex.
347
Sheet fractured during hot rolling, so subsequent tests not possible


Comp. ex.
348
Due to shape defects of hot rolled sheet, subsequent tests not possible


Comp. ex.
349
Due to shape defects of cold rolled sheet, subsequent tests not possible


Comp. ex.
350
Due to excessive cold rolling load, cold rolling not possible






















Comp. ex.
351
680
60
None
None
30
300
300
315
None
None
100
None
None
898


Inv. ex.
352
800
2
None
None
30
250
50
213
None
None
30
432
312
898


Comp. ex.
353
800
60
None
None
1
280
315
356
None
None
50
408
271
898


Inv. ex.
354
800
60
None
None
20
235
0
0
None
None
30
432
312
898


Inv. ex.
355
800
60
None
None
20
260
3
3
None
None
30
432
312
898


Inv. ex.
356
800
60
None
None
20
260
15
25
None
None
30
432
312
898


Comp. ex.
357
800
60
None
None
20
260
20
1050
None
None
30
432
312
898


Comp. ex.
358
800
60
None
None
20
235
0
150
None
None
30
432
312
898


Comp. ex.
359
800
60
None
None
20
235
0
150
None
None
30
432
312
898


Comp. ex.
360
800
60
None
None
20
235
0
150
None
None
30
432
312
898


Comp. ex.
361
800
60
None
None
20
235
0
150
None
None
30
432
312
898


Comp. ex.
362
800
60
None
None
20
235
0
150
None
None
30
432
312
898













Average













Sheet thickness

hardness


























Middle




A
B

Soft surface
change of









part
Soft surface

Ratio of soft

Sheet
Soft surface

layer
hardness



Limit




in sheet
layer
Position of
surface layer
Total
thickness ½
layer average

nano-hardness
transition

Tensile

bending




thickness
(one side)
soft surface
(one side) to
thickness
average Vickers
Vickers

standard
zone

strength
Elongation
radius R
Bending


Class
No.
(mm)
(mm)
layer
sheet thickness (%)
(mm)
hardness (Hv)
hardness (Hv)
B/A
deviation
(ΔHv/mm)
(%)
(MPa)
(%)
(mm)
load (N)





Inv. ex.
301
2.0
0.3
Both surfaces
12
2.6
289
253
0.87
0.3
1979
10
901
15
1.0
22400


Inv. ex.
302
2.5
0.3
One surface
11
2.8
305
270
0.89
0.3
2071
10
949
16
1.0
31200


Inv. ex.
303
2.4
0.4
Both surfaces
13
3.2
329
294
0.89
0.3
1963
12
1021
19
1.0
42500


Inv. ex.
304
2.8
0.4
Both surfaces
11
3.6
351
299
0.85
0.5
2318
15
1090
25
1.0
33900


Inv. ex.
305
1.8
0.3
Both surfaces
13
2.4
409
279
0.68
0.6
2720
13
1237
23
1.0
36300


Inv. ex.
306
2.6
0.25
Both surfaces
8
3.1
440
270
0.61
0.7
2344
13
1348
25
1.0
75000


Inv. ex.
307
2.9
0.3
Both surfaces
9
3.5
486
299
0.61
0.3
2137
14
1480
17
1.0
63700


Inv. ex.
308
1.6
0.3
Both surfaces
14
2.2
452
276
0.61
0.7
1949
13
1530
17
1.0
24500


Inv. ex.
309
2.1
0.5
Both surfaces
16
3.1
385
275
0.72
0.4
1964
14
1149
30
1.0
39000


Inv. ex.
310
1.9
0.35
Both surfaces
13
2.6
348
288
0.83
0.6
2046
17
1068
31
1.0
46900


Inv. ex.
311
1.9
0.35
Both surfaces
13
2.6
332
247
0.74
0.5
2092
13
1007
19
1.0
11300


Inv. ex.
312
3.0
0.15
One surface
5
3.2
379
270
0.71
0.5
2309
15
1169
20
1.0
50000


Inv. ex.
313
2.6
0.35
Both surfaces
11
3.3
343
236
0.69
0.5
2538
16
1044
21
1.0
53000


Inv. ex.
314
2.8
0.45
Both surfaces
12
3.7
333
289
0.87
0.7
1829
13
1029
19
1.0
28100


Inv. ex.
315
2.3
0.25
Both surfaces
9
2.8
325
287
0.88
0.6
2351
13
1019
24
1.0
14300


Inv. ex.
316
3.0
0.25
Both surfaces
7
3.5
314
242
0.77
0.6
2187
14
974
25
1.0
45200


Inv. ex.
317
2.3
0.3
Both surfaces
10
2.9
324
261
0.81
0.3
2278
14
999
25
1.0
50800


Inv. ex.
318
2.9
0.45
Both surfaces
12
3.8
328
255
0.78
0.7
1890
18
1003
36
1.0
44700


Inv. ex.
319
1.6
0.35
Both surfaces
15
2.3
444
269
0.61
0.3
1917
13
1375
24
1.0
15800


Inv. ex.
320
2.0
0.45
Both surfaces
16
2.9
418
309
0.74
0.4
2731
18
1263
36
1.0
17200


Inv. ex.
321
2.5
0.4
Both surfaces
12
3.3
346
241
0.70
0.4
2779
15
1049
29
1.0
48800


Inv. ex.
322
2.4
0.8
One surface
25
3.2
381
269
0.70
0.6
1876
13
1142
25
1.0
20400


Inv. ex.
323
3.0
0.5
Both surfaces
13
4.0
418
256
0.61
0.3
1776
13
1241
22
1.0
51100


Inv. ex.
324
1.8
0.25
Both surfaces
11
2.3
459
278
0.61
0.4
1760
13
1385
20
1.0
28000


Inv. ex.
325
1.7
0.45
Both surfaces
17
2.6
471
286
0.61
0.4
2019
13
1369
23
1.0
31700


Inv. ex.
326
1.7
0.45
Both surfaces
17
2.6
471
286
0.61
0.6
2521
13
1372
23
1.0
35400


Inv. ex.
327
1.7
0.45
Both surfaces
17
2.6
471
286
0.61
0.6
2668
18
1372
35
1.0
50000


Inv. ex.
328
1.7
0.45
Both surfaces
17
2.6
471
286
0.61
0.3
2432
14
1371
18
1.0
19300


Inv. ex.
329
1.7
0.45
Both surfaces
17
2.6
471
286
0.61
0.3
2674
15
1372
21
1.0
20400


Inv. ex.
330
1.7
0.45
Both surfaces
17
2.6
471
286
0.61
0.3
2311
13
1371
19
1.0
44200


Inv. ex.
331
1.7
0.45
Both surfaces
17
2.6
471
286
0.61
0.4
2218
15
1370
26
1.0
22000


Inv. ex.
332
1.7
0.45
Both surfaces
17
2.6
471
286
0.61
0.6
2250
17
1370
30
1.0
20800


Inv. ex.
333
1.7
0.45
Both surfaces
17
2.6
471
286
0.61
0.7
2530
14
1372
24
1.0
19600


Inv. ex.
334
1.9
0.3
Both surfaces
12
2.5
337
287
0.85
0.5
1891
17
1041
36
1.0
33100


Inv. ex.
335
1.9
0.3
Both surfaces
12
2.5
337
287
0.85
0.5
2337
13
1043
25
1.0
38700


Inv. ex.
336
1.9
0.3
Both surfaces
12
2.5
337
287
0.85
0.6
2543
13
1044
28
1.0
27700


Inv. ex.
337
2.8
0.45
Both surfaces
12
3.7
419
258
0.62
0.6
2367
16
1346
23
1.0
44500


Inv. ex.
338
2.8
0.45
Both surfaces
12
3.7
423
256
0.61
0.4
2698
13
1348
17
1.0
71400


Inv. ex.
339
1.9
0.45
Both surfaces
16
2.8
333
287
0.86
0.4
1827
13
1027
21
1.0
26300


Inv. ex.
340
1.9
0.45
Both surfaces
16
2.8
333
287
0.86
0.7
1906
13
1028
24
1.0
44300


Inv. ex.
341
1.9
0.45
Both surfaces
16
2.8
333
287
0.86
0.5
2343
13
1030
20
1.0
19700


Comp. ex.
342
1.7
0.3
Both surfaces
13
2.3
252
236
0.94
0.6
5200
7
799
17
3.0
6800


Inv. ex.
343
2.9
0.45
Both surfaces
12
3.8
319
254
0.80
0.8
2205
8
986
9
1.0
107300


Comp. ex.
344
1.6
0.5
Both surfaces
19
2.6
199
270
1.36
0.6
5400
13
771
20
3.0
5900


Comp. ex.
345
1.6
0.45
Both surfaces
18
2.5
319
251
0.79
0.9
6300
13
993
20
3.0
7500


Comp. ex.
346
1.6
1.3
One surface
31
4.2
295
269
0.91
0.5
1200
13
898
22
2.5
8660









Comp. ex.
347
Cannot be evaluated























Comp. ex.
348

















Comp. ex.
349


Comp. ex.
350


Comp. ex.
351
1.6
0.2
Both surfaces
10
2.0
187
178
0.95
0.7
2300
0
752
13
1.0
10500


Inv. ex.
352
1.6
0.2
Both surfaces
10
2.0
315
198
0.63
0.7
2200
4
976
14
1.0
6900


Comp. ex.
353
1.6
0.2
Both surfaces
10
2.0
315
198
0.63
0.9
5500
13
993
27
3.0
4860


Inv. ex.
354
1.6
0.2
Both surfaces
10
2.0
315
198
0.63
0.2
1900
0
975
11
1.0
6900


Inv. ex.
355
1.6
0.2
Both surfaces
10
2.0
315
198
0.63
0.2
1800
3
974
14
1.0
8000


Inv. ex.
356
1.6
0.2
Both surfaces
10
2.0
315
198
0.63
0.5
5200
4
991
13
1.5
6900


Comp. ex.
357
1.6
0.2
Both surfaces
10
2.0
189
176
0.93
0.6
2100
18
694
37
3.0
4850


Comp. ex.
358
1.6
0.2
Both surfaces
10
2.0
320
198
0.62
0.9
5300
13
986
19
2.5
4980


Comp. ex.
359
1.6
0.2
Both surfaces
10
2.0
320
198
0.62
0.9
5500
13
988
18
3.0
4370


Comp. ex.
360
1.6
0.2
Both surfaces
10
2.0
320
198
0.62
0.9
5400
13
1002
20
3.0
4070


Comp. ex.
361
1.6
0.2
Both surfaces
10
2.0
320
198
0.62
0.9
5200
13
996
18
2.5
4480


Comp. ex.
362
1.6
0.2
Both surfaces
10
2.0
320
198
0.62
0.9
5300
13
985
19
2.5
3280









A sheet having a tensile strength of 800 MPa or more, a limit curvature radius R of less than 2 mm, and a bending load (N) of more than 3000 times the sheet thickness (mm) was evaluated as high strength steel sheet excellent in bendability (invention examples in Table 8). In particular, in Invention Example 356, the requirement of the average Vickers hardness of the soft surface layer being more than 0.60 time and 0.90 time or less the average Vickers hardness of the 1/2 position in sheet thickness is satisfied and further the requirement of the nano-hardness standard deviation of the soft surface layer being 0.8 or less is satisfied, but it is learned that the average hardness change in the sheet thickness direction of the hardness transition zone exceeds 5000 (ΔHv/mm). As a result, in the steel sheet of Invention Example 356, the limit curvature radius R was 1.5 mm. In contrast to this, in the steel sheets of the examples where the two requirements of “the average Vickers hardness of the soft surface layer being more than 0.60 time and 0.90 time or less the average Vickers hardness of the 1/2 position in sheet thickness” and “the nano-hardness standard deviation of the soft surface layer being 0.8 or less” were satisfied and “the average hardness change in the sheet thickness direction of the hardness transition zone was 5000 (ΔHv/mm) or less”, the limit curvature radius R was 1 mm. Furthermore, if the middle part in sheet thickness includes retained austenite by an area percent of 10% or more, the elongation becomes 15% or more and it was possible to obtain high strength steel sheet excellent in ductility in addition to bendability (Invention Examples 301 to 341 in Table 8). On the other hand, if even one of the performances of a “tensile strength of 800 MPa or more”, a “limit curvature radius R of less than 2 mm”, and a “bending load (N) of more than 3000 times the sheet thickness (mm) is not satisfied, the sheet was designated a comparative example.


Further, in steel sheet manufactured by hot rolling without rough rolling being performed two times or more under conditions of a rough rolling temperature of 1100° C. or more, a sheet thickness reduction rate per pass of 5% to less than 50%, and a time between passes of 3 seconds or more, the limit curvature radius R was high and/or the bending load was low and a sufficient bendability could not be achieved.

Claims
  • 1-12. (canceled)
  • 13. High strength steel sheet having a tensile strength of 800 MPa or more comprising a middle part in sheet thickness and a soft surface layer arranged at one side or both sides of the middle part in sheet thickness, wherein each soft surface layer has a thickness of more than 10 μm and 30% or less of the sheet thickness, the soft surface layer has an average Vickers hardness of more than 0.60 time and 0.90 time or less the average Vickers hardness of the sheet thickness 1/2 position, and the soft surface layer has a nano-hardness standard deviation of 0.8 or less.
  • 14. The high strength steel sheet according to claim 13, wherein the high strength steel sheet further comprises a hardness transition zone formed between the middle part in sheet thickness and each soft surface layer while adjoining them, wherein the hardness transition zone has an average hardness change in the sheet thickness direction of 5000 (ΔHv/mm) or less.
  • 15. The high strength steel sheet according to claim 13, wherein the middle part in sheet thickness comprises, by area percent, 10% or more of retained austenite.
  • 16. The high strength steel sheet according to claim 14, wherein the middle part in sheet thickness comprises, by area percent, 10% or more of retained austenite.
  • 17. The high strength steel sheet according to claim 13, wherein the middle part in sheet thickness comprises, by mass %, C: 0.05 to 0.8%,Si: 0.01 to 2.50%,Mn: 0.010 to 8.0%,P: 0.1% or less,S: 0.05% or less,Al: 0 to 3%, andN: 0.01% or less, anda balance of Fe and unavoidable impurities.
  • 18. The high strength steel sheet according to claim 14, wherein the middle part in sheet thickness comprises, by mass %, C: 0.05 to 0.8%,Si: 0.01 to 2.50%,Mn: 0.010 to 8.0%,P: 0.1% or less,S: 0.05% or less,Al: 0 to 3%, andN: 0.01% or less, anda balance of Fe and unavoidable impurities.
  • 19. The high strength steel sheet according to claim 15, wherein the middle part in sheet thickness comprises, by mass %, C: 0.05 to 0.8%,Si: 0.01 to 2.50%,Mn: 0.010 to 8.0%,P: 0.1% or less,S: 0.05% or less,Al: 0 to 3%, andN: 0.01% or less, anda balance of Fe and unavoidable impurities.
  • 20. The high strength steel sheet according to claim 16, wherein the middle part in sheet thickness comprises, by mass %, C: 0.05 to 0.8%,Si: 0.01 to 2.50%,Mn: 0.010 to 8.0%,P: 0.1% or less,S: 0.05% or less,Al: 0 to 3%, andN: 0.01% or less, anda balance of Fe and unavoidable impurities.
  • 21. The high strength steel sheet according to claim 17, wherein the middle part in sheet thickness further comprises, by mass %, at least one element selected from the group consisting of: Cr: 0.01 to 3%,Mo: 0.01 to 1%,B: 0.0001% to 0.01%,Ti: 0.01 to 0.2%,Nb: 0.01 to 0.2%,V: 0.01 to 0.2%,Cu: 0.01 to 1%,Ni: 0.01 to 1%, andREM: 0.001 to 0.05%.
  • 22. The high strength steel sheet according to claim 18, wherein the middle part in sheet thickness further comprises, by mass %, at least one element selected from the group consisting of: Cr: 0.01 to 3%,Mo: 0.01 to 1%,B: 0.0001% to 0.01%,Ti: 0.01 to 0.2%,Nb: 0.01 to 0.2%,V: 0.01 to 0.2%,Cu: 0.01 to 1%,Ni: 0.01 to 1%, andREM: 0.001 to 0.05%.
  • 23. The high strength steel sheet according to claim 19, wherein the middle part in sheet thickness further comprises, by mass %, at least one element selected from the group consisting of: Cr: 0.01 to 3%,Mo: 0.01 to 1%,B: 0.0001% to 0.01%,Ti: 0.01 to 0.2%,Nb: 0.01 to 0.2%,V: 0.01 to 0.2%,Cu: 0.01 to 1%,Ni: 0.01 to 1%, andREM: 0.001 to 0.05%.
  • 24. The high strength steel sheet according to claim 20, wherein the middle part in sheet thickness further comprises, by mass %, at least one element selected from the group consisting of: Cr: 0.01 to 3%,Mo: 0.01 to 1%,B: 0.0001% to 0.01%,Ti: 0.01 to 0.2%,Nb: 0.01 to 0.2%,V: 0.01 to 0.2%,Cu: 0.01 to 1%,Ni: 0.01 to 1%, andREM: 0.001 to 0.05%.
  • 25. The high strength steel sheet according to claim 17, wherein the C content of the soft surface layer is 0.30 time or more and 0.90 time or less the C content of the middle part in sheet thickness.
  • 26. The high strength steel sheet according to claim 21, wherein the total of the Mn content, Cr content, and Mo content of the soft surface layer is 0.3 time or more the total of the Mn content, Cr content, and Mo content of the middle part in sheet thickness.
  • 27. The high strength steel sheet according to claim 21, wherein the B content of the soft surface layer is 0.3 time or more the B content of the middle part in sheet thickness.
  • 28. The high strength steel sheet according to claim 21, wherein the total of the Cu content and Ni content of the soft surface layer is 0.3 time or more the total of the Cu content and Ni content of the middle part in sheet thickness.
  • 29. The high strength steel sheet according to claim 13, further comprising a hot dip galvanized layer, hot dip galvannealed layer, or electrogalvanized layer at the surface of the soft surface layer.
  • 30. The high strength steel sheet according to claim 14, further comprising a hot dip galvanized layer, hot dip galvannealed layer, or electrogalvanized layer at the surface of the soft surface layer.
  • 31. The high strength steel sheet according to claim 15, further comprising a hot dip galvanized layer, hot dip galvannealed layer, or electrogalvanized layer at the surface of the soft surface layer.
  • 32. The high strength steel sheet according to claim 16, further comprising a hot dip galvanized layer, hot dip galvannealed layer, or electrogalvanized layer at the surface of the soft surface layer.
Priority Claims (2)
Number Date Country Kind
2017-029283 Feb 2017 JP national
2017-029295 Feb 2017 JP national
PCT Information
Filing Document Filing Date Country Kind
PCT/JP2018/006053 2/20/2018 WO 00