STEEL SHEET AND PLATED STEEL SHEET
20240240278 ยท 2024-07-18
Assignee
Inventors
- Takuya MITSUNOBU (Tokyo, JP)
- Keitaro MATSUDA (Tokyo, JP)
- Jun Maki (Tokyo, JP)
- Takehiro TAKAHASHI (Tokyo, JP)
- Hiroshi TAKEBAYASHI (Tokyo, JP)
Cpc classification
C21D8/0257
CHEMISTRY; METALLURGY
C22C38/002
CHEMISTRY; METALLURGY
C23C30/00
CHEMISTRY; METALLURGY
International classification
Abstract
A steel sheet comprising, by mass %, C: 0.05 to 0.40%, Si: 0.2 to 3.0%, and Mn: 0.1 to 5.0%, wherein a surface layer of the steel sheet contains granular oxides, an average grain size of the granular oxides is 300 nm or less, a number density of granular oxides is 4.0/?m.sup.2 or more, the steel sheet comprises an SiMn depleted layer having a thickness of 3.0 ?m or more from the surface of the steel sheet, and Si and Mn contents of the SiMn depleted layer not containing oxides at the ? position of the thickness are respectively less than 10% of the Si and Mn contents at the sheet thickness center part of the steel sheet, and a plated steel sheet using the same are provided.
Claims
1. A steel sheet having a chemical composition comprising, by mass %, C: 0.05 to 0.40%, Si: 0.2 to 3.0%, Mn: 0.1 to 5.0%, sol. Al: 0 to less than 0.4000%, P: 0.0300% or less, S: 0.0300% or less, N: 0.0100% or less, B: 0 to 0.010%, Ti: 0 to 0.150%, Nb: 0 to 0.150%, V: 0 to 0.150%, Cr: 0 to 2.00%, Ni: 0 to 2.00%, Cu: 0 to 2.00%, Mo: 0 to 1.00%, W: 0 to 1.00%, Ca: 0 to 0.100%, Mg: 0 to 0.100%, Zr: 0 to 0.100%, Hf: 0 to 0.100%, REM: 0 to 0.100% and a balance of Fe and impurities, wherein a surface layer of the steel sheet contains granular oxides, an average grain size of the granular oxides is 300 nm or less, a number density of the granular oxides is 4.0/?m.sup.2 or more, the steel sheet comprises an SiMn depleted layer having a thickness of 3.0 ?m or more from the surface of the steel sheet, and Si and Mn contents of the SiMn depleted layer at ? position of the thickness and not containing oxides are respectively less than 10% of the Si and Mn contents at a sheet thickness center part of the steel sheet.
2. The steel sheet according to claim 1, wherein the average grain size of the granular oxides is 200 nm or less.
3. The steel sheet according to claim 1, wherein the number density of the granular oxides is 10.0/?m.sup.2 or more.
4. The steel sheet according to claim 1, wherein the surface layer of the steel sheet further contains grain boundary oxides.
5. The steel sheet according to claim 4, wherein, when examining a cross-section of the surface layer of the steel sheet, a Ratio A of a length of the grain boundary oxides projected on the surface of the steel sheet to a length of the surface of the steel sheet is 50% or more.
6. The steel sheet according to claim 5, wherein the Ratio A is 80% or more.
7. A plated steel sheet having a plating layer including Zn on the steel sheet of claim 1.
8. The plated steel sheet according to claim 7, wherein the plating layer has a chemical composition of Zn-(0.3 to 1.5)% Al.
9. The steel sheet according to claim 2, wherein the number density of the granular oxides is 10.0/?m.sup.2 or more.
10. The steel sheet according to claim 2, wherein the surface layer of the steel sheet further contains grain boundary oxides.
11. The steel sheet according to claim 3, wherein the surface layer of the steel sheet further contains grain boundary oxides.
12. A plated steel sheet having a plating layer including Zn on the steel sheet of claim 2.
13. A plated steel sheet having a plating layer including Zn on the steel sheet of claim 3.
14. A plated steel sheet having a plating layer including Zn on the steel sheet of claim 4.
15. A plated steel sheet having a plating layer including Zn on the steel sheet of claim 5.
16. A plated steel sheet having a plating layer including Zn on the steel sheet of claim 6.
Description
BRIEF DESCRIPTION OF DRAWINGS
[0052]
[0053]
[0054]
[0055]
[0056]
DESCRIPTION OF EMBODIMENTS
<Steel Sheet>
[0057] The steel sheet according to the present invention has a chemical composition comprising, by mass %, [0058] C: 0.05 to 0.40%, [0059] Si: 0.2 to 3.0%, [0060] Mn: 0.1 to 5.0%, [0061] sol. Al: 0 to less than 0.4000%, [0062] P: 0.0300% or less, [0063] S: 0.0300% or less, [0064] N: 0.0100% or less, [0065] B: 0 to 0.010%, [0066] Ti: 0 to 0.150%, [0067] Nb: 0 to 0.150%, [0068] V: 0 to 0.150%, [0069] Cr: 0 to 2.00%, [0070] Ni: 0 to 2.00%, [0071] Cu: 0 to 2.00%, [0072] Mo: 0 to 1.00%, [0073] W: 0 to 1.00%, [0074] Ca: 0 to 0.100%, [0075] Mg: 0 to 0.100%, [0076] Zr: 0 to 0.100%, [0077] Hf: 0 to 0.100%, [0078] REM: 0 to 0.100% and [0079] a balance of Fe and impurities, wherein [0080] a surface layer of the steel sheet contains granular oxides, [0081] an average grain size of the granular oxides is 300 nm or less, [0082] a number density of the granular oxides is 4.0/?m.sup.2 or more, [0083] the steel sheet comprises an SiMn depleted layer having a thickness of 3.0 ?m or more from the surface of the steel sheet, and [0084] Si and Mn contents of the SiMn depleted layer at ? position of the thickness and not containing oxides are respectively less than 10% of the Si and Mn contents at a sheet thickness center part of the steel sheet.
[0085] In the production of a high strength steel sheet, a steel slab adjusted to a predetermined chemical composition is rolled (typically, hot rolled and cold rolled), then generally annealed for the purpose of obtaining the desired microstructure, etc. In the annealing, the comparatively easily oxidizable constituents in the steel sheet (for example, Si and Mn) bond with the oxygen in the annealing atmosphere whereby a layer including oxides is formed in the vicinity of the surface of the steel sheet. For example, like the steel sheet 1 shown in
[0086] In contrast, as illustrated in
[0087] Further, a high strength steel sheet used in an atmospheric environment, particularly a high strength steel sheet for automobiles, is repeatedly exposed and used in various environments of differing temperature and humidity. Such an environment is called a corrosive atmospheric environment. It is known that hydrogen is generated in the process of corrosion in the corrosive atmospheric environment. Moreover, the hydrogen penetrates deeper than the surface layer region in the steel and segregates at the martensite grain boundaries of the steel sheet microstructure thereby causing embrittlement of the grain boundaries and triggering hydrogen embrittlement cracking (delayed cracking) in the steel sheet. Martensite is a hard structure, and therefore has a high hydrogen susceptibility and is more vulnerable to hydrogen embrittlement cracking. Such cracking can become a problem when working steel sheet. Accordingly, to prevent hydrogen embrittlement cracking, in a high strength steel sheet used in a corrosive atmospheric environment, it is effective to reduce the amount of hydrogen built up in the steel, more specifically, the amount of hydrogen built up at positions deeper than the surface layer region of the steel sheet. The inventors discovered that by controlling the form of oxides present at the surface layer of a steel sheet, more specifically, by making the oxides inside of the steel sheet granular oxides having an average grain size and number density in predetermined ranges and, further, controlling the SiMn depleted layer formed due to the drop in the Si and Mn concentrations of the surroundings caused by the formation of such internal oxides to within predetermined ranges of thickness and composition, the granular oxides function as trap sites for hydrogen penetrating the steel sheet at the surface layer region of the steel sheet in a corrosive environment and the SiMn depleted layer promotes diffusion of penetrating hydrogen to improve the discharge of hydrogen from inside the steel and that as a result, the amount of hydrogen built up in the steel sheet used in a corrosive environment can be reduced not only by suppression of penetration of hydrogen, but also promotion of discharge of penetrated hydrogen to the outside of the system. The term high hydrogen embrittlement resistance means a state in which the amount of hydrogen built up in steel sheet or plated steel sheet is reduced enough so that hydrogen embrittlement cracking can be sufficiently suppressed.
[0088] The inventors analyzed in detail the relationship between the form of the oxides and their effectiveness as trap sites for hydrogen. As a result, they discovered that, as shown in
[0089] Further, the inventors analyzed in detail the relationship between the form of the SiMn depleted layer formed due to the drop in the concentrations of Si and Mn in the surroundings caused by the formation of granular oxides 12 and other internal oxides such as shown in
[0090] Further, it is known that hydrogen embrittlement cracking sometimes occurs not only when using a high strength steel sheet such as explained above in a corrosive atmospheric environment, but also in annealing at the time of producing the high strength steel sheet due to hydrogen present in the annealing atmosphere penetrating deeper than the surface layer region of the base steel. At this time, the inventors discovered that the combination of the granular oxides and SiMn depleted layer acts effectively not only for use in a corrosive atmospheric environment, but also for suppression of penetration of hydrogen into the steel sheet at the time of annealing in the production process and for discharge of the penetrating hydrogen and as a result high hydrogen embrittlement resistance can be achieved both at the time of production of steel sheet and at the time of its use.
[0091] On the other hand, when hot stamping or welding a plated steel sheet that has a plating layer including Zn provided on the steel sheet surface, because of the high temperature during working, sometimes the Zn included in the plating layer will melt. If the Zn melts, the molten Zn will penetrate the steel. If working is performed in that state, sometimes liquid metal embrittlement (LME) cracking will occur inside of the steel sheet and the fatigue properties of the steel sheet will degrade due to the LME. The inventors discovered that if the granular oxides have the desired average grain size and number density, they can contribute not only to improving hydrogen embrittlement resistance but also improving LME resistance. In further detail, they discovered that the granular oxides function as trap sites for Zn trying to penetrate the steel during working at a high temperature. Due to this, Zn trying to penetrate the steel during, for example, hot stamping, is trapped by the granular oxides at the surface layer of the steel sheet and penetration of Zn into the crystal grain boundaries is suitably suppressed.
[0092] Accordingly, they discovered that not only for improving the above-mentioned hydrogen penetration resistance but also improving the LME resistance, it is important for granular oxides to be made present in a fine size and a large amount. The steel sheet according to the present invention is not necessarily limited to such a plated steel sheet and also encompasses a steel sheet which is not plated. The reason is that even a steel sheet which is not plated can suffer from LME cracking for example at the time of spot welding it with galvanized steel sheet due to zinc melting in the galvanized steel sheet penetrating the steel sheet which is not plated.
[0093] Below; the steel sheet according to the present invention will be explained in detail. The thickness of the steel sheet according to the present invention is not particularly limited but may be, for example, 0.1 to 3.2 mm.
[Chemical Composition of Steel Sheet]
[0094] The chemical composition contained in the steel sheet according to the present invention will be explained next. The % regarding content of the elements, unless otherwise stated, will mean mass %. In the numerical ranges in the chemical composition, a numerical range expressed using to, unless otherwise indicated, will mean a range having the numerical values before and after the to as the lower limit value and the upper limit value.
(C: 0.05 to 0.40%)
[0095] C (carbon) is an important element for securing the strength of steel. To secure sufficient strength and furthermore obtain the desired form of the internal oxides, the C content is 0.05% or more. The C content is preferably 0.07% or more, more preferably 0.10% or more, even more preferably 0.12% or more. On the other hand, if the C content is excessive, the weldability is liable to fall. Accordingly, the C content is 0.40% or less. The C content may also be 0.38% or less, 0.35% or less, 0.32% or less, or 0.30% or less.
(Si: 0.2 to 3.0%)
[0096] Si (silicon) is an element effective for improving the strength of steel. To secure sufficient strength and furthermore sufficiently cause the formation of the desired oxides, in particular, granular oxides inside the steel sheet, the Si content is 0.2% or more. The Si content is preferably 0.3% or more, more preferably 0.5% or more, further preferably 1.0% or more. On the other hand, if the Si content is excessive, external oxides are excessively formed and in turn deterioration of the surface properties is liable to be triggered. Furthermore, coarsening of the granular oxides is liable to be invited. Accordingly, the Si content is 3.0% or less. The Si content may also be 2.8% or less, 2.5% or less, 2.3% or less, or 2.0% or less.
(Mn: 0.1 to 5.0%)
[0097] Mn (manganese) is an element effective for obtaining hard structures to improve the strength of steel. To secure sufficient strength and further make the desired oxides, in particular granular oxides, sufficiently form inside of the steel sheet, the Mn content is 0.1% or more. The Mn content is preferably 0.5% or more, more preferably 1.0% or more, further preferably 1.5% or more. On the other hand, if the Mn content is excessive, external oxides will be excessively formed, the metallographic structure is liable to become uneven due to Mn segregation, and the workability is liable to decline. Furthermore, coarsening of the granular oxides is liable to be invited. Accordingly, the Mn content is 5.0% or less. The Mn content may also be 4.5% or less, 4.0% or less, 3.5% or less, or 3.0% or less.
(Sol. Al: 0 to Less than 0.4000%)
[0098] Al (aluminum) is an element which acts as a deoxidizing element. The Al content may also be 0%, but to obtain a sufficient deoxidizing effect, the Al content is preferably 0.0010% or more. The Al content is more preferably 0.0050% or more, further preferably 0.0100% or more, further more preferably 0.0150% or more. On the other hand, if the Al content is excessive, it is liable to trigger a reduction in the workability or a deterioration in surface properties. Therefore, the Al content is less than 0.4000%. The Al content may be 0.3900% or less, 0.3800% or less, 0.3700% or less, 0.3500% or less, 0.3400% or less, 0.3300% or less, 0.3000% or less, or 0.2000% or less. The Al content means the content of so-called acid-soluble Al (sol. Al).
(P: 0.0300% or Less)
[0099] P (phosphorus) is an impurity generally contained in steel. If excessively containing P, the weldability is liable to decline. Accordingly, the P content is 0.0300% or less. The P content is preferably 0.0200% or less, more preferably 0.0100% or less, even more preferably 0.0050% or less. The lower limit of the P content is 0%, but from the viewpoint of production costs, the P content may be more than 0% or be 0.0001% or more.
(S: 0.0300% or Less)
[0100] S (sulfur) is an impurity generally contained in steel. If excessively containing S, the weldability is liable to decline and further the amount of precipitated MnS is liable to increase and the bendability or other workability is liable to fall. Accordingly, the S content is 0.0300% or less. The S content is preferably 0.0100% or less, more preferably 0.0050% or less, even more preferably 0.0020% or less. The lower limit of the S content is 0%, but from the viewpoint of desulfurization costs, the S content may be more than 0% or be 0.0001% or more.
(N: 0.0100% or Less)
[0101] N (nitrogen) is an impurity generally contained in steel. If excessively containing N, the weldability is liable to decline. Accordingly, the N content is 0.0100% or less. The N content is preferably 0.0080% or less, more preferably 0.0050% or less, even more preferably 0.0030% or less. The lower limit of the N content is 0%, but from the viewpoint of production costs, the N content may be more than 0% or be 0.0010% or more.
[0102] The basic chemical composition of the steel sheet according to the present invention is as explained above. Furthermore the steel sheet may contain, in accordance with need, the following optional elements. Inclusion of these elements is not essential. The lower limits of contents of these elements are 0%.
(B: 0 to 0.010%)
[0103] B (boron) is an element which contributes to increasing hardenability and improving strength and further segregates at the grain boundaries to strengthen the grain boundaries and improve toughness. The B content may be 0%, but may be included in accordance with need so as to obtain the above effect. The B content may be 0.0001% or more, 0.0005% or more, or 0.001% or more. On the other hand, from the viewpoint of securing sufficient toughness and weldability, the B content is preferably 0.010% or less and may be 0.008% or less or 0.006% or less as well.
(Ti: 0 to 0.150%)
[0104] Ti (titanium) is an element which precipitates during cooling of steel as TiC and contributes to improving strength. The Ti content may be 0%, but may be included in accordance with need so as to obtain the above effect. The Ti content may be 0.001% or more, 0.003% or more, 0.005% or more, or 0.010% or more. On the other hand, if excessively containing Ti, coarse TiN is formed and the toughness is liable to be harmed. For this reason, the Ti content is preferably 0.150% or less and may also be 0.100% or less or 0.050% or less.
(Nb: 0 to 0.150%)
[0105] Nb (niobium) is an element which contributes to improving strength through improving hardenability. The Nb content may be 0%, but may be included in accordance with need so as to obtain the above effect. The Nb content may be 0.001% or more, 0.005% or more, 0.010% or more, or 0.015% or more. On the other hand, from the viewpoint of securing sufficient toughness and weldability, the Nb content is preferably 0.150% or less and may also be 0.100% or less or 0.060% or less.
(V: 0 to 0.150%)
[0106] V (vanadium) is an element which contributes to improving strength through improving hardenability. The V content may be 0%, but may be included in accordance with need so as to obtain the above effect. The V content may be 0.001% or more, 0.010% or more, 0.020% or more, or 0.030% or more. On the other hand, from the viewpoint of securing sufficient toughness and weldability, the V content is preferably 0.150% or less and may be 0.100% or less or 0.060% or less.
(Cr: 0 to 2.00%)
[0107] Cr (chromium) is effective for increasing the hardenability of steel and increasing the strength of steel. The Cr content may be 0%, but may be included in accordance with need so as to obtain the above effect. The Cr content may be 0.01% or more, 0.10% or more, 0.20% or more, 0.50% or more, or 0.80% or more. On the other hand, if excessively containing Cr, Cr carbides are formed in a large amount and conversely the hardenability is liable to be harmed, so the Cr content is preferably 2.00% or less and may be 1.80% or less or 1.50% or less.
(Ni: 0 to 2.00%)
[0108] Ni (nickel) is an element effective for increasing the hardenability of steel and increasing the strength of steel. The Ni content may be 0%, but may be included in accordance with need so as to obtain the above effect. The Ni content may be 0.01% or more, 0.10% or more, 0.20% or more, 0.50% or more, or 0.80% or more. On the other hand, excessive increase of Ni invites a rise in costs. Therefore, the Ni content is preferably 2.00% or less and may also be 1.80% or less or 1.50% or less.
(Cu: 0 to 2.00%)
[0109] Cu (copper) is an element effective for increasing the hardenability of steel and increasing the strength of steel. The Cu content may be 0%, but may be included in accordance with need so as to obtain the above effect. The Cu content may be 0.001% or more, 0.005% or more, or 0.01% or more. On the other hand, from the viewpoint of suppressing a drop in toughness, cracking of slabs after casting, and a drop in weldability, the Cu content is preferably 2.00% or less and may be 1.80% or less, 1.50% or less, or 1.00% or less.
(Mo: 0 to 1.00%)
[0110] Mo (molybdenum) is an element effective for increasing the hardenability of steel and increasing the strength of steel. The Mo content may be 0%, but may be included in accordance with need so as to obtain the above effect. The Mo content may be 0.01% or more, 0.10% or more, 0.20% or more, or 0.30% or more. On the other hand, from the viewpoint of suppressing a drop in toughness and weldability, the Mo content is preferably 1.00% or less and may also be 0.90% or less or 0.80% or less.
(W: 0 to 1.00%)
[0111] W (tungsten) is an element effective for increasing the hardenability of steel and increasing the strength of steel. The W content may be 0%, but may be included in accordance with need so as to obtain the above effect. The W content may be 0.001% or more, 0.005% or more, or 0.01% or more. On the other hand, from the viewpoint of suppressing a drop in toughness and weldability, the W content is preferably 1.00% or less and may also be 0.90% or less, 0.80% or less, 0.50% or less, or 0.10% or less.
(Ca: 0 to 0.100%)
[0112] Ca (calcium) is an element contributing to inclusion control, particularly fine dispersion of inclusions, and has the action of increasing toughness. The Ca content may be 0%, but may be included in accordance with need so as to obtain the above effect. The Ca content may also be 0.0001% or more, 0.0005% or more, or 0.001% or more. On the other hand, if excessively containing Ca, degradation of the surface properties will sometimes appear. For this reason, the Ca content is preferably 0.100% or less and may be 0.080% or less, 0.050% or less, 0.010% or less, or 0.005% or less.
(Mg: 0 to 0.100%)
[0113] Mg (magnesium) is an element contributing to inclusion control, particularly fine dispersion of inclusions, and has the action of increasing toughness. The Mg content may be 0%, but may be included in accordance with need so as to obtain the above effect. The Mg content may also be 0.0001% or more, 0.0005% or more, or 0.001% or more. On the other hand, if excessively containing Mg, degradation of the surface properties will sometimes appear. For this reason, the Mg content is preferably 0.100% or less and may also be 0.090% or less, 0.080% or less, 0.050% or less, or 0.010% or less.
(Zr: 0 to 0.100%)
[0114] Zr (zirconium) is an element contributing to inclusion control, particularly fine dispersion of inclusions, and has the action of increasing toughness. The Zr content may be 0%, but may be included in accordance with need so as to obtain the above effect. The Zr content may also be 0.001% or more, 0.005% or more, or 0.010% or more. On the other hand, if excessively containing Zr, degradation of the surface properties will sometimes appear. For this reason, the Zr content is preferably 0.100% or less and may be 0.050% or less, 0.040% or less, or 0.030% or less.
(Hf: 0 to 0.100%)
[0115] Hf (hafnium) is an element contributing to inclusion control, particularly fine dispersion of inclusions, and has the action of increasing toughness. The Hf content may be 0%, but may be included in accordance with need so as to obtain the above effect. The Hf content may also be 0.0001% or more, 0.0005% or more, or 0.001% or more. On the other hand, if excessively containing Hf, degradation of the surface properties will sometimes appear. Therefore, the Hf content is preferably 0.100% or less and may be 0.050% or less, 0.030% or less, or 0.010% or less.
(REM: 0 to 0.100%)
[0116] A REM (rare earth element) is an element contributing to inclusion control, particularly fine dispersion of inclusions, and has the action of increasing toughness. The REM content may be 0%, but may be included in accordance with need so as to obtain the above effect. The REM content may also be 0.0001% or more, 0.0005% or more, or 0.001% or more. On the other hand, if excessively containing REM, degradation of the surface properties will sometimes appear. For this reason, the REM content is preferably 0.100% or less and may also be 0.050% or less, 0.030% or less, or 0.010% or less. REM is an acronym for rare earth metals and indicates elements belonging to the lanthanide series. A REM is normally added as mischmetal.
[0117] In the steel sheet according to the present invention, the balance excluding the above chemical composition is comprised of Fe and impurities. Here, impurities mean constituents, etc., which enter from the ore, scraps, and other raw materials and various factors in the manufacturing process when industrially producing steel sheet.
[0118] In the present invention, the chemical composition of the steel sheet may be analyzed using an elemental analysis technique known to persons skilled in the art. For example, it is performed by inductively coupled plasma-mass spectroscopy (ICP-MS). However, C and S may be measured by combustion-infrared absorption, and N may be measured using inert gas fusion-thermal conductivity. These analyses may be performed on samples taken from the steel sheet by a method based on JIS G0417: 1999.
[Surface Layer]
[0119] In the present invention, the surface layer of the steel sheet means a region from the surface of the steel sheet (in the case of a plated steel sheet, the interface between the steel sheet and plating layer) to a predetermined depth in the thickness direction. The predetermined depth is typically 50 ?m or less.
[0120] As illustrated in
[0121] Furthermore, as illustrated in
[Granular Oxides]
[0122] In the present invention, granular oxides mean oxides dispersed as grains inside the crystal grains of the steel or on the crystal grain boundaries. Furthermore, granular means being present away from each other mutually in the steel matrix, having, for example, a 1.0 to 5.0 aspect ratio (maximum linear length (major diameter) traversing the granular oxide/maximum linear length (minor diameter) traversing the oxide perpendicular to the major diameter). Dispersed as grains means that the grains of oxides are not positioned according to a specific rule (for example, linearly) but are positioned randomly. Since granular oxides are in fact typically present three-dimensionally in spherical shapes or substantially spherical shapes in the surface layer of the steel sheet, the granular oxides are typically observed to have circular shapes or substantially circular shapes when a cross-section of the surface layer of the steel sheet is observed. In
(Average Grain Size)
[0123] In the present invention, the average grain size of the granular oxides is 300 nm or less. By controlling the average grain size to such a range, it is possible to make granular oxides finely disperse at the surface layer of the steel sheet. The granular oxides function well as trap sites for hydrogen suppressing the penetration of hydrogen in a corrosive environment and/or at the time of annealing in the production process and further function well as trap sites for Zn able to penetrate plated steel sheet comprised of steel sheet on which a plating layer is formed at the time of hot stamping or welding. On the other hand, if the average grain size is too large, the granular oxides will not sufficiently function as trap sites for hydrogen and/or trap sites for Zn and excellent hydrogen embrittlement resistance and/or LME resistance is liable to not be obtained. The average grain size of the granular oxides is preferably 250 nm or less, more preferably 200 nm or less, further preferably 150 nm or less. The finer the granular oxides, the better, so the average grain size of the granular oxides is not particularly prescribed in lower limit, but for example is 5 nm or more, 10 nm or more, or 50 nm or more.
(Number Density)
[0124] In the present invention, the number density of granular oxides is 4.0/?m.sup.2 or more. By controlling the number density to such a range, it is possible to make granular oxides finely disperse at the surface layer of the steel sheet. The granular oxides function well as trap sites for hydrogen suppressing the penetration of hydrogen in a corrosive environment and/or at the time of annealing in the production process and further function well as trap sites for Zn able to penetrate plated steel sheet obtained by forming a plating layer on steel sheet at the time of hot stamping or welding. On the other hand, if the number density is less than 4.0/?m.sup.2, the number density as trap sites for hydrogen and/or trap sites for Zn is not sufficient, the granular oxides do not sufficiently function as trap sites for hydrogen and/or trap sites for Zn, and good hydrogen embrittlement resistance and/or LME resistance is liable to be unable to be obtained. The number density of granular oxides is preferably 6.0/?m.sup.2 or more, more preferably 8.0/?m.sup.2 or more, further preferably 10.0/?m.sup.2 or more. The larger the amount of granular oxides present, the better, so while the number density of granular oxides is not particularly set in upper limit, it may for example be 100.0 ?m.sup.2 or less.
[0125] The average grain size and number density of the fine granular oxides are measured by a scan electron microscope (SEM). The specific measurement is as follows: A cross-section of the surface layer of the steel sheet is examined by a SEM and a SEM image including the granular oxides is obtained. From the SEM image, as examined regions, a total of 10 regions of 1.0 ?m (depth direction)?1.0 ?m (width direction) are selected. The examined position of each region is made 1.0 ?m in the region from the steel sheet surface to 1.5 ?m for the depth direction (direction vertical to surface of steel sheet) and is made 1.0 ?m at any position of the SEM image for the width direction (direction parallel to surface of steel sheet). Next, SEM images of the regions selected in the above way are extracted and digitalized to divide them into oxide parts and steel parts. From the digitalized images, the area of each granular oxide part is calculated. Further, the number of granular oxides in each digitalized image is counted. From the total area and number of granular oxides of the total of regions in the 10 locations found in this way, the average grain size (nm) of the granular oxides is found as the circle equivalent diameter. Further, the number density of granular oxides (/?m.sup.2) is equal to the average value of the numbers of granular oxides counted from the digitalized images. If only parts of the granular oxides are observed in the examined regions, i.e., if not all of the contours of the granular oxides are inside the examined regions, they are not counted in the numbers. Further, from the viewpoint of the measurement precision, the lower limit counted as the number of granular oxides is 5.0 nm is more.
[Grain Boundary Oxides]
[0126] The steel sheet according to the present invention may further contain grain boundary oxides at the surface layer of the steel sheet. In the present invention, grain boundary oxides means oxides present along the crystal grain boundaries of the steel. Oxides present inside the crystal grains of the steel are not included. In actuality, the grain boundary oxides are present in planar shapes so as to run along the crystal grain boundaries at the surface layer of the steel sheet, so when examining a cross-section of the surface layer of a steel sheet, such grain boundary oxides are observed in line shapes. In
(Ratio A)
[0127] If examining the cross-section of the surface layer of the steel sheet, the Ratio A of the length of the grain boundary oxides projected on the surface of the steel sheet with respect to the length of the surface of the steel sheet may be any value of 0) to 100%. In the present invention, the Ratio A, as shown in
[0128] The Ratio A, as shown in
[Chemical Composition of Oxides]
[0129] In the present invention, the granular oxides and optional grain boundary oxides (below, also referred to simply as oxides) include one or more of the above-mentioned elements included in the steel sheet in addition to oxygen and typically have chemical compositions including Si, O, and Fe and in some cases further including Mn. More specifically, the oxides typically contain Si: 5 to 25%, Mn: 0 to 10%, 0: 40 to 65%, and Fe: 10 to 30%. The oxides may also contain elements able to be included in the above-mentioned steel sheet (for example, Cr, etc.) in addition to these elements.
[SiMn Depleted Layer]
[0130] The steel sheet according to the present invention contains an SiMn depleted layer having a thickness of 3.0 ?m or more from the surface of the steel sheet. The contents of Si and Mn of the SiMn depleted layer not containing oxides at the ? position of that thickness are respectively less than 10% of the contents of Si and Mn at the sheet thickness center part of the steel sheet. By making the SiMn depleted layer formed at the surface layer of the steel sheet due to the formation of the granular oxides and optional grain boundary oxides a thickness of 3.0 ?m or more and controlling the Si and Mn depletion rates of the SiMn depleted layer respectively less than 10%, it is possible to sufficiently reduce the amounts of dissolved Si and Mn impeding diffusion of hydrogen. As a result, it becomes possible to promote diffusion of hydrogen and remarkably improve the dischargeability of hydrogen from inside the steel. By making the thickness of the SiMn depleted layer greater, it is possible to promote more the diffusion of hydrogen from inside the steel, so the thickness of the SiMn depleted layer is preferably 4.0 ?m or more, more preferably 5.0 ?m or more, most preferably 7.0 ?m or more. The upper limit of thickness of the SiMn depleted layer is not particularly limited, but for example the thickness of the SiMn depleted layer may be 50.0 ?m or less.
[0131] Similarly, by making the Si and Mn depletion rates of the SiMn depleted layer smaller, it is possible to further reduce the amounts of dissolved Si and Mn in the steel. For this reason, the Si depletion rate of the SiMn depleted layer is preferably 8% or less, more preferably 6% or less, most preferably 4% or less. The lower limit of the Si depletion rate is not particularly prescribed, but may be 0%. Similarly, the Mn depletion rate of the SiMn depleted layer is preferably 8% or less, more preferably 6% or less, most preferably 4% or less. The lower limit of the Mn depletion rate is not particularly prescribed, but may be 0%. In the present invention, the expression not containing oxides means not containing not only the above granular oxides and grain boundary oxides, but also any other oxides. Such a region not containing oxides can be identified by examination of the cross-section by a SEM and energy dispersed X-ray spectroscopy (EDS). Further, the SiMn depleted layer according to the present invention cannot be controlled to the desired ranges of thickness and composition just by forming granular oxides and other internal oxides. As explained in detail later, it becomes important to suitably control the progression of internal oxidation in the production process.
[0132] The thickness of the SiMn depleted layer, as shown by D in
<Plated Steel Sheet>
[0133] The plated steel sheet according to the present invention has a plating layer containing Zn on the above-mentioned steel sheet according to the present invention. This plating layer may be formed on one side of the steel sheet or may be formed on both sides. As the plating layer containing Zn, for example, a hot dip galvanized layer, hot dip galvannealed layer, electrogalvanized layer, electrogalvannealed layer, etc., may be mentioned. More specifically, as the plating type, for example, Zn-0.2% Al (GI), Zn-(0.3 to 1.5)% Al, Zn-4.5% Al, Zn-0.09% Al-10% Fe (GA), Zn-1.5% Al-1.5% Mg, Zn-11% Al-3% Mg-0.2% Si, Zn-11% Ni, Zn-15% Mg, etc., can be used.
[Chemical Composition of Plating Layer]
[0134] The chemical composition included in a plating layer containing Zn in the present invention will be explained next. The % regarding content of the elements, unless otherwise stated, will mean mass %. In the numerical ranges in the chemical composition of the plating layer, a numerical range expressed using to, unless otherwise indicated, will mean a range having the numerical values before and after the to as the lower limit value and the upper limit value.
(Al: 0 to 60.0%)
[0135] Al is an element which is included together with Zn or is alloyed with it and improves the corrosion resistance of the plating layer, so may be included in accordance with need. Therefore, the Al content may be 0%. To form a plating layer containing Zn and Al, preferably the Al content is 0.01% or more. For example, it may be 0.1% or more, 0.5% or more, 1.0% or more, or 3.0% or more. On the other hand, even if excessively containing Al, the effect of improvement of the corrosion resistance becomes saturated, so the Al content is preferably 60.0% or less. For example, it may be 55.0% or less, 50.0% or less, 40.0% or less, 30.0% or less, 20.0% or less, 10.0% or less, or 5.0% or less. From the viewpoint of improvement of the LME resistance, the Al is preferably 0.4 to 1.5%.
(Mg: 0 to 15.0%)
[0136] Mg is an element which is included together with Zn and Al or is alloyed with the same and improves the corrosion resistance of the plating layer, so may be included in accordance with need. Therefore, the Mg content may be 0%. To form a plating layer containing Zn, Al, and Mg, preferably the Mg content is 0.01% or more. For example, it may be 0.1% or more, 0.5% or more, 1.0% or more, or 3.0% or more. On the other hand, if excessively containing Mg, the Mg will not completely dissolve in the plating bath but will float as oxides. If galvanizing by such a plating bath, oxides will deposit on the surface layer causing poor appearance or liable to cause the occurrence of non-plated parts. For this reason, the Mg content is preferably 15.0% or less, for example, may be 10.0% or less or 5.0% or less.
(Fe: 0 to 15.0%)
[0137] Fe can be included in the plating layer due to diffusion from the steel sheet when forming a plating layer containing Zn on the steel sheet, then heat treating the plated steel sheet. Therefore, Fe is not included in the plating layer in a state not treated by heat, so the Fe content may also be 0%. Further, the Fe content may be 1.0% or more, 2.0% or more, 3.0% or more, 4.0% or more, or 5.0% or more. On the other hand, the Fe content is preferably 15.0% or less, for example, may be 12.0% or less, 10.0% or less, 8.0% or less, or 6.0% or less.
(Si: 0 to 3.0%)
[0138] Si is an element which further improves the corrosion resistance if included in a plating layer containing Zn, in particular a ZnAlMg plating layer, so may be included in accordance with need. Therefore, the Si content may be 0%. From the viewpoint of improvement of the corrosion resistance, the Si content may for example be 0.005% or more, 0.01% or more, 0.05% or more, 0.1% or more, or 0.5% or more. Further, the Si content may be 3.0% or less, 2.5% or less, 2.0% or less, 1.5% or less, or 1.2% or less.
[0139] The basic chemical composition of the plating layer is as explained above. Furthermore the plating layer may contain, optionally, one or more of Sb: 0 to 0.50%, Pb: 0 to 0.50%, Cu: 0 to 1.00%, Sn: 0 to 1.00%, Ti: 0 to 1.00%, Sr: 0 to 0.50%, Cr: 0 to 1.00%, Ni: 0 to 1.00%, and Mn: 0) to 1.00%. While not particularly limited, from the viewpoint of sufficiently manifesting the actions and functions of the basic constituents forming the plating layer, the total content of these optional elements is preferably made 5.00% or less, more preferably 2.00% or less.
[0140] At the plating layer, the balance besides the above constituents is comprised of Zn and impurities. The impurities at the plating layer mean constituents such as the raw material entering due to various factors in the production process when producing the plating layer. In the plating layer, as impurities, elements besides the basic constituents and optional constituents explained above may be included in trace amounts in a range not impeding the effect of the present invention.
[0141] The chemical composition of the plating layer can be determined by dissolving the plating layer in an acid solution containing an inhibitor for inhibiting corrosion of the steel sheet and measuring the obtained solution by ICP (inductively coupled plasma) emission spectroscopy.
[0142] The thickness of the plating layer may for example be 3 to 50 ?m. Further, the amount of deposition of the plating layer is not particularly limited but for example may be 10 to 170 g/m.sup.2 per side. In the present invention, the amount of deposition of the plating layer is determined by dissolving the plating layer in an acid solution containing an inhibitor for inhibiting corrosion of the base iron and finding the change in weight before and after pickling.
[Tensile Strength]
[0143] The steel sheet and plated steel sheet according to the present invention preferably have a high strength. Specifically, they preferably have 440 MPa or more tensile strength. For example, the tensile strength may be 500 MPa or more, 600 MPa or more, 700 MPa or more, or 800 MPa or more. The upper limit of the tensile strength is not particularly prescribed, but from the viewpoint of securing toughness, may for example be 2000 MPa or less. The tensile strength may be measured by taking a JIS No. 5 tensile test piece having a direction vertical to the rolling direction as its longitudinal direction and performing a test based on JIS Z 2241(2011).
[0144] The steel sheet and plated steel sheet according to the present invention are high in strength and have a high plateability, LME resistance, and hydrogen embrittlement resistance, so can be suitably used in a broad range of fields such as automobiles, household electric appliances, and building materials, but are particularly preferably used in the automotive field. Steel sheet used for automobiles usually is plated (typically Zn-based plating), so if using the steel sheet according to the present invention as steel sheet for automobiles, the effect of the present invention of having a high plateability is optimally exhibited. Further, steel sheet and plated steel sheet used for automobiles are often hot stamped. In that case, hydrogen embrittlement cracking and LME cracking can become remarkable problems. Therefore, when using the steel sheet and plated steel sheet according to the present invention as steel sheet for automobiles, the effect of the present invention of having a high hydrogen embrittlement resistance and LME resistance is optimally exhibited.
<Method of Production of Steel Sheet>
[0145] Below, a preferable method of production of the steel sheet according to the present invention will be explained. The following explanation is intended to illustrate the characteristic method for producing the steel sheet according to the present invention and is not intended to limit the steel sheet to one produced by the method of production explained below.
[0146] The steel sheet according to the present invention can be obtained for example by performing a casting step of casting molten steel adjusted in chemical composition to form a steel slab, a hot rolling step of hot rolling the steel slab to obtain hot rolled steel sheet, a coiling step of coiling the hot rolled steel sheet, a cold rolling step of cold rolling the coiled hot rolled steel sheet to obtain cold rolled steel sheet, a grinding step of introducing dislocations into the surface of the cold rolled steel sheet, and an annealing step of annealing the ground cold rolled steel sheet. Alternatively, the hot rolled steel sheet may not be coiled after the hot rolling step, but pickled and then cold rolled as it is.
[Casting Step]
[0147] The conditions of the casting step are not particularly prescribed. For example, after smelting by a blast furnace or electric furnace, etc., various secondary refining operations may be performed, then the molten metal cast by the usual continuous casting, ingot casting, or other method.
[Hot Rolling Step]
[0148] The thus cast steel slab can be hot rolled to obtain hot rolled steel sheet. The hot rolling step is performed by directly hot rolling the cast steel slab or by reheating after cooling once. If reheating, the heating temperature of the steel slab may for example be 1100? C., to 1250? C. In the hot rolling step, usually rough rolling and finish rolling are performed. The temperatures and rolling reductions of the rolling operations may be suitably changed in accordance with the desired metallographic structure and sheet thickness. For example, the end temperature of the finish rolling may be made 900 to 1050? C., and the rolling reduction of the finish rolling may be made 10 to 50%.
[Coiling Step]
[0149] The hot rolled steel sheet can be coiled at a predetermined temperature. The coiling temperature may be suitably changed in accordance with the desired metallographic structure, etc., and may for example be 500 to 800? C. The hot rolled steel sheet may be heat treated under predetermined conditions before being coiled or after being coiled by being uncoiled. Alternatively, the sheet can be pickled after the hot rolling step without performing a coiling step and then subjected to a later explained cold rolling step.
[Cold Rolling Step]
[0150] After pickling the hot rolled steel sheet, the hot rolled steel sheet can be cold rolled to obtain cold rolled steel sheet. The rolling reduction of the cold rolling may be suitably changed in accordance with the desired metallographic structure and sheet thickness and may for example be 20 to 80%. After the cold rolling step, for example, the sheet may be air cooled to cool it down to room temperature.
[Grinding Step]
[0151] To obtain granular oxides in a fine size and large amount and further the optional grain boundary oxides in the desired amount at the surface layer of the finally obtained steel sheet and to cause the formation of an SiMn depleted layer having the desired thickness and composition, it is effective to perform a grinding step before annealing the cold rolled steel sheet. Due to that grinding step, it is possible to introduce a large amount of dislocations to the surface of the cold rolled steel sheet. Oxygen, etc., diffuse faster at the grain boundaries than inside the grains, so by introducing a large amount of dislocations to the surface of the cold rolled steel sheet, it is possible to form a large number of paths in the same way as the case of grain boundaries. For this reason, at the time of annealing, oxygen easily diffuses (penetrates) to the inside of the steel along these dislocations and the speeds of diffusion of Si and Mn are also improved, so as a result, the oxygen bonds with the Si and/or Mn inside of the steel and formation of granular oxides and further the optional grain boundary oxides can be promoted. Further, along with promotion of formation of these internal oxides, the drop in the concentrations of Si and Mn in the surroundings is also promoted, so it is also possible to promote the formation of an SiMn depleted layer having the desired thickness and composition. The grinding step is not particularly limited, but for example can be performed by using a heavy duty grinding brush to grind the surface of cold rolled steel sheet under conditions of an amount of grinding of 10 to 200 g/m.sup.2. The amount of grinding by the heavy duty grinding brush can be adjusted by any suitable method known to persons skilled in the art. While not particularly limited, for example, it can be adjusted by suitably selecting the number, speed, brushing pressure, coating solution used, etc., of the heavy duty grinding brush. By performing such a grinding step, in the later explained annealing step, it becomes possible to form the desired granular oxides and optional grain boundary oxides and possible to reliably and efficiently form an SiMn depleted layer having the desired thickness and composition, i.e., having a 3.0 ?m or more thickness and having Si and Mn 25 depletion rates of respectively less than 10%, at the surface layer of the steel sheet.
[Annealing Step]
[0152] The cold rolled steel sheet subjected to the above grinding step is annealed. The annealing is preferably performed in a state in which tension is applied to the cold rolled steel sheet in the rolling direction. In particular, in a region where the annealing temperature is 500? C., or more, it is preferable to raise the tension in performing the annealing compared with other regions. Specifically, in a region where the annealing temperature is 500? C., or more, it is preferable to perform the annealing in a state applying 3 to 150 MPa, in particular 15 to 150 MPa of tension to the cold rolled steel sheet in the rolling direction. If applying tension at the time of annealing, a large amount of dislocations can be more effectively introduced to the surface of the cold rolled steel sheet. Therefore, at the time of annealing, it is made easier for oxygen to diffuse to (penetrate) the inside of the steel along those dislocations and the speeds of diffusion of Si and Mn are also improved, so oxides become easier to form inside the steel sheet. As a result, this is advantageous for increase of the number density of the granular oxides, formation of the desired ratio of the grain boundary oxides, and formation of the SiMn depleted layer having the desired thickness and composition.
[0153] The holding temperature at the annealing step is preferably 700? C., to 870? C. From the viewpoint of making the granular oxides form in a fine size and large amount while keeping down the formation of the grain boundary oxides to within a range of a Ratio A of less than 50%, the holding temperature at the annealing step is preferably 700? C., to 780? C., more preferably 720 to 760? C. If the holding temperature of the annealing step is less than 700? C., granular oxides are liable to not be sufficiently formed and sometimes the hydrogen penetration resistance will become insufficient. On the other hand, from the viewpoint of causing the formation of a large amount of grain boundary oxides so that the granular oxides become fine in size and large in amount and the Ratio A becomes 50% or more, the holding temperature of the annealing step is preferably more than 780? C., to 870? C., more preferably 800 to 850? C. On the other hand, if the holding temperature of the annealing step is more than 870? C., granular oxides are liable to not be sufficiently formed and sometimes the hydrogen penetration resistance and in turn the hydrogen embrittlement resistance will become insufficient and further the LME resistance will become insufficient. Further, if the holding temperature of the annealing step is more than 900? C., an external oxidation layer will formed at the surface of the steel sheet and the plateability is liable to become insufficient. The temperature elevation rate up to the holding temperature is not particularly limited, but may be 1 to 10? C./s. Further, the temperature elevation may be performed in two stages by a first temperature elevation rate of 1 to 10? C./s and a second temperature elevation rate of 1 to 10? C./s different from the first temperature elevation rate.
[0154] The holding time at the holding temperature of the annealing step is preferably more than 50) seconds to 150 seconds, more preferably 80 to 120 seconds. If the holding time is 50 seconds or less, the granular oxides and optional grain boundary oxides are liable to not be sufficiently formed and sometimes the hydrogen embrittlement resistance and LME resistance will become insufficient. On the other hand, if the holding time is more than 150 seconds, the granular oxides are liable to become coarser and sometimes the hydrogen embrittlement resistance and LME resistance will become insufficient.
[0155] From the viewpoint of causing the formation of granular oxides in a fine size and large amount, the dew point of the atmosphere in the annealing step is preferably ?20 to 10? C., more preferably ?10 to 5? C. If the dew point is too low; an external oxidation layer is liable to be formed on the surface of the steel sheet and internal oxides liable to not be sufficiently formed. The plateability, hydrogen embrittlement resistance, and LME resistance will sometimes become insufficient. On the other hand, by raising the dew point, it is possible to promote the formation of grain boundary oxides, but if the dew point is too high, Fe oxides will form as external oxides on the steel sheet surface and sometimes the plateability will become insufficient. Further, sometimes the granular oxides will coarsened and the hydrogen embrittlement resistance and/or LME resistance will become insufficient. Further, the atmosphere in the annealing step may be a reducing atmosphere, more specifically a reducing atmosphere containing nitrogen and hydrogen, for example, a reducing atmosphere of hydrogen in 1 to 10% (for example, hydrogen 4% and balance of nitrogen).
[0156] Furthermore, it is effective to remove the internal oxidation layer (typically including the grain boundary oxides) of the steel sheet when performing the annealing step. During the above-mentioned rolling step, in particular the hot rolling step, sometimes an internal oxidation layer is formed at the surface layer of the steel sheet. Such an internal oxidation layer formed in a rolling step is liable to inhibit the formation of granular oxides at the annealing step, so that internal oxidation layer is preferably removed before annealing by pickling, etc. More specifically, the depth of the internal oxidation layer of the cold rolled steel sheet when performing an annealing step may be 0.5 ?m or less, preferably 0.3 ?m or less, more preferably 0.2 ?m or less, still more preferably 0.1 ?m or less.
[0157] By performing the steps explained above, it is possible to obtain steel sheet comprised of steel sheet with a surface layer containing granular oxides in a sufficiently fine size and large amount and including an SiMn depleted layer having a desired thickness and composition.
[0158] If providing a step, as a stage before the annealing step, of oxidizing and then reducing the steel in the oxidation zone by a 0.9 to 1.4 air ratio or air-fuel ratio, in the oxidation step, the granular oxides will excessively grow beyond the average grain size 300 nm, so the granular oxides will not sufficiently function as trap sites for hydrogen and/or trap sizes for Zn and it will become difficult to obtain good hydrogen embrittlement resistance and/or LME resistance.
<Method of Production of Plated Steel Sheet>
[0159] Below, a preferable method of production of the plated steel sheet according to the present invention will be explained. The following explanation is intended to illustrate the characteristic method for producing the plated steel sheet according to the present invention and is not intended to limit the plated steel sheet to one produced by the method of production explained below.
[0160] The plated steel sheet according to the present invention can be obtained by performing a plating step for forming a plating layer containing Zn on the steel sheet produced in the above way.
[Plating Step]
[0161] The plating step may be performed according to a method known to persons skilled in the art. The plating step may for example be performed by hot dip coating and may be performed by electroplating. Preferably, the plating step is performed by hot dip coating. The conditions of the plating step may be suitably set considering the chemical composition, thickness, amount of deposition, etc., of the desired plating layer. After the plating, alloying may be performed. Typically, the conditions of the plating step may be set so as to form a plating layer containing Al: 0 to 60.0%, Mg: 0 to 15.0%, Fe: 0 to 15%, and Si: 0 to 3% and having a balance of Zn and impurities. More specifically, the conditions of the plating step may for example be suitably set so as to form for example Zn-0.2% Al (GI), Zn-0.09% Al (GA), Zn-1.5% Al-1.5% Mg, or Zn-11% Al-3% Mg-0.2% Si.
Examples
[0162] Below, examples will be used to explain the present invention in more detail, but the present invention is not limited to these examples in any way.
[0163] In the following examples, in Example X, steel sheets having a Ratio A relating to grain boundary oxides of 0% or more and less than 50% were produced, while in Example Y, steel sheets having a Ratio A relating to grain boundary oxides of 50% or more were produced. The steel sheets produced in the respective example were investigated for plateability, hydrogen embrittlement resistance, and LME resistance.
Example X
(Preparation of Steel Sheet Samples)
[0164] Molten steels adjusted in chemical compositions were cast to form steel slabs. The steel slabs were hot rolled, pickled, then cold rolled to obtain cold rolled steel sheets. Next, the sheets were air-cooled down to room temperature. The cold rolled steel sheets were pickled, then the internal oxidation layers formed by rolling were removed down to the internal oxidation layer depth (?m) before annealing described in Table 1. Next, samples were taken from the cold rolled steel sheets by the method based on JIS G0417: 1999 and the chemical compositions of the steel sheets were analyzed by ICP-MS, etc. The measured chemical compositions of the steel sheets are shown in Table 1. The thicknesses of the steel sheets used were 1.6 mm in all cases.
[0165] Next, each of the cold rolled steel sheets was coated with an NaOH aqueous solution, then the surface of the cold rolled steel sheet was ground using a heavy duty grinding brush by an amount of 10 to 200 g/m.sup.2 (Sample No. 135 no grinding). After that, each was annealed by the dew point, holding temperature, and holding time shown in Table 1 (mainly holding temperature of 700 to 780? C., and holding time of more than 50 seconds to 150 seconds) (annealing atmosphere: hydrogen 4% and balance of nitrogen) to prepare each steel sheet sample. In all of the steel sheet samples, the temperature elevation rate at the time of annealing was made 6.0? C./s up to 500? C., and was made 2.0? C./s from 500? C., to the holding temperature. In the above annealing, the cold rolled steel sheet was annealed in the state applying 1 MPa or more of tension in the rolling direction. In the region of an annealing temperature of 500? C., or more, compared with other regions, the annealing was performed in the state applying a higher tension in the rolling direction, specifically a tension of 3 to 150 MPa (in Sample No. 134, such tension not applied). The presence of any grinding by a heavy duty grinding brush and the conditions of the annealing (presence of application of tension of 3 to 150 MPa, dew point (? C.), holding temperature (? C.), and holding time (s) in region with annealing temperature of 500? C., or more) are shown in Table 1. In each steel sheet sample, a JIS No. 5 tensile test piece having a direction vertical to the rolling direction as its longitudinal direction was taken. A tensile test was performed based on JIS Z 2241(2011). As a result, in Nos. 116 and 118, the tension strengths were less than 440) MPa, while in the others, they were 440 MPa or more.
(Analysis of Surface Layer of Steel Sheet Samples)
[0166] Each steel sheet sample prepared in the above way was cut to 25 mm?15 mm. The cut sample was buried in a resin and polished to a mirror surface. At the cross-section of each steel sheet sample. 1.0 ?m?1.0 ?m regions were examined by a SEM at 10 locations. The examined positions were made the 1.0 ?m from 0.2 to 1.2 ?m from the steel sheet surface for the depth direction (direction vertical to surface of steel sheet) and 1.0 ?m of any position of the SEM image for the width direction (direction parallel to surface of steel sheet). As the regions, regions not containing grain boundary oxides were selected. Next, the SEM images of the regions of the steel sheet samples obtained were digitalized, the areas of the granular oxide parts were calculated from the digitalized images, and further the numbers of the granular oxides in the SEM images were counted. From the areas and numbers of granular oxides at the 10 digitalized images found in this way, the average grain size as the circular equivalent diameter and number density of the granular oxides were found. The average grain size (nm) and number density (/?m.sup.2) of the granular oxides of the steel sheet samples are shown in Table 1. In Table 1, if there are no granular oxides in the SEM image (case where number density=0)), the average grain size was described as -.
[0167] Further, the Ratio A for each steel sheet sample was measured from examination of the cross-section of the above buried sample. Specifically, in a 150 ?m width (=L.sub.0) SEM image, the positions of grain boundary oxides were identified, the identified grain boundary oxides were projected on the surface of the steel sheet, and the lengths L of the grain boundary oxides in the field were found. Based on the L.sub.0 and L found in this way, the Ratio A (%)=100?L/L.sub.0 was found. The ratio A (%) of granular oxides for each steel sheet sample is shown in Table 1.
[0168] The thickness of the SiMn depleted layer was determined in the SEM image for which the Ratio A was measured by measuring the distance from the surface of the steel sheet to the furthest position where grain boundary oxides (granular oxides if no grain boundary oxides present) are present when proceeding from the surface of the steel sheet in the thickness direction of the steel sheet (direction vertical to surface of steel sheet). Further, the Si and Mn contents of the region not containing oxides at the ? position of thickness of the SiMn depleted layer are determined by analyzing points of 10 locations not containing oxides randomly selected at ? position of thickness of the SiMn depleted layer determined from the SEM image by a TEM-EDS and obtaining the arithmetic averages of the obtained measured values of the Si and Mn concentrations. Further, the Si and Mn contents at the sheet thickness center part of the steel sheet are determined by examining the cross-section of the sheet thickness center part by a SEM, analyzing points of 10 locations randomly selected at the sheet thickness center part from the SEM image by a TEM-EDS, and obtaining the arithmetic averages of the obtained measured values of the Si and Mn concentrations. Finally, the values of the Si and Mn contents at the ? position of thickness of the SiMn depleted layer divided by the Si and Mn contents at the sheet thickness center part of the steel sheet and expressed as percentages are determined as the Si and Mn depletion rates. Further, each steel sheet sample was analyzed for chemical compositions of the granular oxides and grain boundary oxides, whereupon each of the oxides contained Si, O. and Fe and numerous oxides further contained Mn. The chemical composition of each of the oxides also contained Si: 5 to 25%, Mn: 0) to 10%, O: 40 to 65%, and Fe: 10 to 30%.
(Preparation of Samples of Plated Steel Sheet)
[0169] Each of the samples of steel sheets of Example 1 was cut to 100 mm?200 mm size, then was plated for forming the plating type shown in Table 1 to thereby prepare a sample of the plated steel sheet. In Table 1, the plating type A means hot dip galvannealed steel sheet (GA), the plating type B means hot dip galvanized-0.2% Al-plated steel sheet (GI), and the plating type C means hot dip galvanized-(0.3 to 1.5)% Al-plated steel sheet (Al content described in Table 1). In the hot dip galvanization step, the cut sample was dipped in a 440? C., hot dip galvanization bath for 3 seconds. After dipping, it was pulled out at 100 mm/s. N.sub.2 wiping gas was used to control the amount of plating deposition to 50 g/m.sup.2. For the plating type A, alloying was performed after that at 460? C.
(Analysis of Composition of Plating Layer)
[0170] The composition of each plating layer was found by dipping a sample cut to 30 mm?30 mm in a 10% aqueous hydrochloric acid solution containing an inhibitor (Ibit made by Asahi Chemical), peeling off the plating layer by pickling, then analyzing the plating constituents dissolved in the aqueous solution by ICP.
(Evaluation of Plateability)
[0171] Each plated steel sheet sample was measured for area ratio of non-plated parts on the surface of that steel sheet so as to evaluate the plateability. Specifically, a 1 mm?1 mm region of the surface of each plated steel sheet sample formed with the plating layer was examined under an optical microscope, parts at which the plating layer was formed (plated parts) and parts where the plating layer was not formed (non-plated parts) were judged from the examined image, the area ratio of the non-plated parts (area of non-plated parts/area of observed image) was calculated, and the plateability was evaluated by the following criteria. The results are shown in Table 1. A is passing and B is failing. [0172] Evaluation A: 5.0% or less [0173] Evaluation B: more than 5.0%
(Evaluation of LME Resistance)
[0174] Each 100?100 mm plated steel sheet sample was spot welded and was cut to 50 mm?100 mm size to prepare two sheets. The two sheets of Zn-based plated steel sheet samples were spot welded using a dome radius type tip size 8 mm welding electrode at a weld angle of 7?, weld force of 3.0 kN, weld time 0.5 second, and weld current 7 kA to obtain a welded member. The welded part was polished at its cross-section, then examined under an optical microscope and measured for length of LME cracking occurring at the cross-section of the welded part and evaluated as follows. The results are shown in Table 1. AAA, AA, and A are passing and B is failing. [0175] Evaluation AAA: LME crack length more than 0 ?m to 150 ?m [0176] Evaluation AA: LME crack length more than 150 ?m to 300 ?m [0177] Evaluation A: LME crack length more than 300 ?m to 500 ?m [0178] Evaluation B: LME crack length more than 500 ?m
(Evaluation of Hydrogen Embrittlement Resistance)
[0179] Each 50 mm?100 mm plated steel sheet sample was treated to form zinc phosphate using a zinc phosphate-based conversion coating (Surfdine SD5350 series: made by Nippon Paint Industrial Coating), then was formed with an electrodeposition coating (PN110 Powernix Grey: made by Nippon Paint Industrial Coating) to 20 ?m and was baked at a 150? C., baking temperature for 20 minutes to form a coating on the plated steel sheet sample. Next, the sample was used for a cyclic corrosion test according to JASO(M609-91). The amount of diffused hydrogen after the elapse of 120 cycles was measured by the thermal desorption method. Specifically, the plated steel sheet sample was heated to 400? C., in a heating furnace provided with a gas chromatography device. The sum of the amount of hydrogen discharged until falling to 250? C., was measured. Based on the measured amount of diffusible hydrogen, the hydrogen embrittlement resistance (amount of hydrogen built up in sample) was evaluated by the following criteria. The results are shown in Table 1. AA and A are passing and B is failing. [0180] Evaluation AA: less than 0.3 ppm [0181] Evaluation A: 0.5 to 0.3 ppm or less [0182] Evaluation B: more than 0.5 ppm
TABLE-US-00001 TABLE 1 Grinding Depth of internal (heavy oxidation layer duty Chemical composition (mass %) before annealing grinding No. Class Fe C Si Mn Al P S N Others (?m) brush) 101 Comp. ex. Bal 0.05 1.6 2.0 0.0201 0.0090 0.0013 0.0024 2.7 Yes 102 Ex. Bal. 0.05 1.1 2.0 0.0152 0.0060 0.0150 0.0039 REM: 0.004 0.1 Yes 103 Ex. Bal. 0.05 2.0 2.0 0.1255 0.0120 0.0012 0.0021 0.1 Yes 104 Ex. Bal. 0.10 0.5 2.0 0.0122 0.0083 0.0025 0.0031 Hf: 0.003 0.2 Yes 105 Ex. Bal 0.10 1.5 2.0 0.0240 0.0120 0.0024 0.0024 0.2 Yes 106 Ex. Bal. 0.20 0.5 2.0 0.0212 0.0155 0.0020 0.0025 Mg: 0.004 0.1 Yes 107 Ex. Bal 0.20 1.0 2.0 0.0150 0.0152 0.0029 0.0011 Zr: 0.040 0.1 Yes 108 Ex. Bal. 0.20 1.8 2.2 0.0170 0.0244 0.0019 0.0021 B: 0.001 0.2 Yes 109 Comp. ex. Bal. 0.20 1.6 2.0 0.0200 0.0101 0.0017 0.0013 0.1 Yes 110 Comp. ex. Bal. 0.20 1.6 2.0 0.0320 0.0131 0.0015 0.0025 0.1 Yes 111 Comp. ex. Bal. 0.20 1.6 2.0 0.0040 0.0110 0.0025 0.0012 0.3 Yes 112 Comp. ex. Bal. 0.20 1.6 2.0 0.0070 0.0084 0.0026 0.0014 0.2 Yes 113 Comp. ex. Bal. 0.20 1.6 2.0 0.0253 0.0030 0.0017 0.0016 0.1 Yes 114 Comp. ex. Bal. 0.20 1.6 2.0 0.0210 0.0074 0.0013 0.0018 0.3 Yes 115 Comp. ex. Bal. 0.20 4.5 2.0 0.0014 0.0147 0.0023 0.0020 0.2 Yes 116 Comp. ex. Bal. 0.20 0 2.0 0.0015 0.0090 0.0024 0.0021 0.1 Yes 117 Comp. ex. Bal. 0.20 1.6 6.0 0.1002 0.0160 0.0011 0.0021 0.1 Yes 118 Comp. ex. Bal. 0.20 1.8 0 0.0299 0.0084 0.0010 0.0023 0.1 Yes 119 Comp. ex. Bal. 0.40 1.6 2.0 0.0501 0.0250 0.0016 0.0020 9.2 Yes 120 Ex. Bal. 0.20 3.0 2.0 0.0239 0.0040 0.0012 0.0018 Ni: 0.90 0.1 Yes 121 Ex. Bal. 0.20 1.8 5.0 0.0209 0.0120 0.0025 0.0019 Cr: 1.00 0.2 Yes 122 Ex. Bal. 0.20 1.0 2.3 0.0360 0.0090 0.0013 0.0017 0.1 Yes 123 Ex. Bal. 0.20 1.8 2.0 0.0380 0.0086 0.0025 0.0012 0.2 Yes 124 Ex. Bal. 0.25 1.5 2.3 0.0402 0.0160 0.0024 0.0025 Ti: 0.030 0.2 Yes 125 Ex. Bal. 0.25 1.5 2.0 0.0420 0.0108 0.0021 0.0021 V: 0.050 0.1 Yes 126 Ex. Bal. 0.30 1.5 2.3 0.0230 0.0132 0.0023 0.0020 0.1 Yes 127 Ex. Bal. 0.30 1.8 0.3 0.0390 0.0081 0.0022 0.0018 Nb: 0.020 0.1 Yes 128 Ex. Bal. 0.35 1.8 3.0 0.0384 0.0043 0.0024 0.0016 Cu: 0.01 0.3 Yes 129 Ex. Bal. 0.35 1.8 2.0 0.0280 0.0088 0.0020 0.0034 0.1 Yes 130 Ex. Bal. 0.40 1.8 2.0 0.0265 0.0070 0.0022 0.0011 Mo: 0.40 0.4 Yes 131 Ex. Bal. 0.40 1.8 2.0 0.0161 0.0120 0.0017 0.0010 W: 0.02 0.1 Yes 132 Ex. Bal. 0.40 1.8 2.0 0.0170 0.0142 0.0015 0.0009 Ca: 0.001 0.2 Yes 133 Ex. Bal. 0.40 1.8 2.0 0.0280 0.0082 0.0011 0.0014 0.1 Yes 134 Comp. ex. Bal. 0.40 1.6 2.0 0.0341 0.0085 0.0017 0.0017 0.1 Yes 135 Comp. ex. Bal. 0.20 1.0 2.3 0.0310 0.0110 0.0021 0.0022 0.2 No Form of internal oxides Granular Grain Annealing conditions Average Number boundary Dew point Holding temp. Holding time grain size density Ratio A No. Tension (? C.) (? C.) (s) (nm) (/?m.sup.2) (%) 101 Yes 0 750 55 0 22 102 Yes 0 750 55 150 4.2 0 103 Yes 0 720 55 100 5.9 0 104 Yes 0 730 55 120 5.3 0 105 Yes 0 700 55 70 6.5 0 106 Yes 0 700 55 50 4.7 0 107 Yes 0 760 55 150 10.8 30 108 Yes 0 740 55 120 13.6 0 109 Yes ?40 740 55 0 0 110 Yes 20 740 55 340 0.9 41 111 Yes 0 880 55 210 1.5 98 112 Yes 0 650 55 35 2.2 0 113 Yes 0 740 5 0 0 114 Yes 0 740 350 480 0.4 97 115 Yes 0 740 55 510 0.8 0 116 Yes 0 740 55 0 0 117 Yes 0 740 55 360 1.5 12 118 Yes 0 740 55 0 0 119 Yes 0 740 55 0 45 120 Yes 0 740 55 150 13.6 0 121 Yes 0 740 55 80 12.9 0 122 Yes 0 740 55 140 11.2 0 123 Yes 0 740 55 120 14.5 0 124 Yes 0 740 55 150 16.2 0 125 Yes 0 740 55 130 10.1 0 126 Yes 0 740 55 140 15.0 0 127 Yes 0 740 55 150 10.6 0 128 Yes 0 780 55 150 11.3 48 129 Yes 0 740 55 140 14.0 0 130 Yes 0 740 55 100 15.9 0 131 Yes 0 740 55 120 13.9 0 132 Yes 0 740 55 140 12.0 0 133 Yes 0 740 55 150 13.2 0 134 No 0 740 100 150 0.2 0 135 Yes 0 740 55 170 0.1 0 SiMn depleted layer Performance Depletion Hydrogen Thickness rate (%) Plating embrittlement No. (?m) Si Mn type Plateability resistance LME resistance 101 4.4 22 31 A A B B 102 3.8 2 3 A A A A 103 3.5 3 4 A A A A 104 3.3 2 3 C: 1.5 A A AAA 105 3.2 1 2 A A A A 106 3 3 3 C: 1.2 A A AAA 107 3 3 4 B A A AA 108 3.4 2 3 C: 0.3 A A AAA 109 A B B B 110 7.5 55 76 A B B B 111 9.5 4 3 A A B B 112 0.2 80 88 A A B B 113 1.2 7 7 A A B B 114 6.6 5 22 A A B B 115 5.6 9 12 A B B B 116 5.5 8 A A B B 117 5.4 6 11 A B B B 118 A A B B 119 4.1 89 90 A A B B 120 5.9 2 2 A A A AA 121 5.4 3 1 A A A AA 122 5.6 2 2 C: 0.8 A A AAA 123 5.2 3 3 A A A AA 124 5.6 4 2 A A A AA 125 5.1 1 3 B A A AA 126 5 2 1 C: 0.4 A A AAA 127 5.6 3 3 A A A AA 128 5.4 3 2 C: 0.6 A A AAA 129 6.1 4 3 A A A AA 130 4.5 3 2 A A A AA 131 4.6 4 3 A A A AA 132 4.3 5 4 A A A AA 133 4.9 4 3 A A A AA 134 8 34 53 A A B B 135 1.8 44 54 A A B B
[0183] In each of Sample Nos. 102 to 108 and 120 to 133, the chemical composition of the steel, the average grain size and number density of the granular oxides, and the thickness and composition of the SiMn depleted layer were suitable, so high plateability, hydrogen embrittlement resistance, and LME resistance were possessed. On the other hand, in each of Sample Nos. 101 and 119, the depth of the internal oxide layer before annealing was great, the desired granular oxides could not be formed, and the desired SiMn depleted layer was also not formed, so high hydrogen embrittlement resistance and LME resistance were not obtained. In Sample No. 109, the dew point at the time of annealing was low, not internal oxides, but an external oxidation layer was formed, and high plateability, hydrogen embrittlement resistance, and LME resistance were not obtained. In Sample No. 110, the dew point at the time of annealing was high, an external oxidation layer was formed, granular oxides could not be refined, and a high plateability, hydrogen embrittlement resistance, and LME resistance were not obtained. In Sample No. 111, the holding temperature at the time of annealing was high, formation of grain boundary oxides was promoted, granular oxides could not be refined, and a high hydrogen embrittlement resistance and LME resistance were not obtained. In Sample No. 112, the holding temperature at the time of annealing was low, internal oxides were not sufficiently formed, and the desired SiMn depleted layer was also not formed, so high hydrogen embrittlement resistance and LME resistance were not obtained. In Sample No. 113, the holding time at the time of annealing was short, internal oxides were not sufficiently formed, and the desired SiMn depleted layer was also not formed, so high hydrogen embrittlement resistance and LME resistance were not obtained. In Sample No. 114, the holding time at the time of annealing was long, formation of grain boundary oxides was promoted, granular oxides could not be refined, and high hydrogen embrittlement resistance and LME resistance were not obtained. In Sample Nos. 115 and 117, respectively the amount of Si and the amount of Mn were excessive and, in each, external oxides grew, further the granular oxides coarsened, and the desired SiMn depleted layer was also not formed, so a high plateability, hydrogen embrittlement resistance, and LME resistance were not obtained. In Sample Nos. 116 and 118, respectively the amount of Si and the amount of Mn were 0 (zero) and, in each, the internal oxidation layer was not formed, and the desired SiMn depleted layer was also not formed, so a high hydrogen embrittlement resistance and LME resistance were not obtained. In Sample No. 134, a predetermined tension was not applied at the time of annealing, so internal oxides were not sufficiently formed and the desired SiMn depleted layer was also not formed. As a result, high hydrogen embrittlement resistance and LME resistance were not obtained. In Sample No. 135, grinding before annealing was not performed, so internal oxides were not sufficiently formed and the desired SiMn depleted layer was also not formed. As a result, high hydrogen embrittlement resistance and LME resistance were not obtained.
Example Y
(Preparation of Steel Sheet Samples)
[0184] Except for making the holding temperature at the annealing mainly more than 780? C., to 870? C., the same procedure was performed as the case of Example X to prepare a sample of the steel sheet under the production conditions shown in Table 2. For each of the samples of the steel sheet, a JIS No. 5 tensile test piece having the direction vertical to the rolling direction as the longitudinal direction was taken and a tensile test was performed based on JIS Z 2241(2011). As a result, for Nos. 201, 216, and 218, the tensile strength was less than 440 MPa. For the others, it was 440 MPa or more.
(Preparation of Samples of Plated Steel Sheet)
[0185] Each of the samples of steel sheets was cut to 100 mm?200 mm size, then was plated for forming the plating type shown in Table 2 to thereby prepare a sample of the plated steel sheet. In Table 2, the plating type A means hot dip galvannealed steel sheet (GA), the plating type B means hot dip galvanized-0.2% Al-plated steel sheet (GI), and the plating type C means hot dip galvanized-(0.3 to 1.5)% Al-plated steel sheet (Al content described in Table 1). In the hot dip galvanization step, the cut sample was dipped in a 440? C., hot dip galvanization bath for 3 seconds. After dipping, it was pulled out at 100 mm/s. N.sub.2 wiping gas was used to control the amount of plating deposition to 50 g/m.sup.2. For the plating type A, alloying was performed after that at 460? C.
[0186] The analysis of the surface layer of the sample of steel sheet, the analysis of the chemical composition of the plating layer, the evaluation of the plateability, the evaluation of the LME resistance, and the evaluation of the hydrogen embrittlement resistance were as explained above in relation to the Example X.
TABLE-US-00002 TABLE 2 Depth of internal oxidation layer Grinding chemical composition (mass %) before annealing (heavy duty No. Class Fe C Si Mn Al P S N Others (?m) grinding brush) 201 Comp. ex. Bal. 0.03 1.8 2.0 0.0201 0.0090 0.0013 0.0024 0.3 Yes 202 Ex. Bal. 0.05 1.2 2.0 0.0133 0.0056 0.0146 0.0036 0.2 Yes 203 Ex. Bal. 0.10 2.1 2.0 0.1234 0.0118 0.0012 0.0023 REM: 0.002 0.1 Yes 204 Ex. Bal. 0.10 0.6 2.0 0.0117 0.0081 0.0025 0.0031 Hf: 0.002 0.2 Yes 205 Ex. Bal. 0.10 1.5 2.2 0.0240 0.0109 0.0024 0.0024 B: 0.001 0.2 Yes 206 Ex. Bal. 0.20 0.5 2.0 0.0212 0.0137 0.0017 0.0024 Mg: 0.003 0.1 Yes 207 Ex. Bal. 0.20 1.8 2.0 0.0150 0.0152 0.0029 0.0011 Zr: 0.035 0.2 Yes 208 Ex. Bal. 0.20 1.8 2.0 0.0160 0.0209 0.0019 0.0019 0.1 Yes 209 Comp. ex. Bal. 0.20 1.8 2.0 0.0199 0.0107 0.0014 0.0013 0.1 Yes 210 Comp. ex. Bal. 0.20 1.8 2.0 0.0311 0.0130 0.0013 0.0022 0.1 Yes 211 Comp. ex. Bal. 0.20 1.8 2.0 0.0032 0.0105 0.0023 0.0011 0.3 Yes 212 Comp. ex. Bal. 0.20 1.8 2.0 0.0066 0.0084 0.0026 0.0011 0.1 Yes 213 Comp. ex. Bal. 0.20 1.8 2.0 0.0253 0.0023 0.0018 0.0017 0.3 Yes 214 Comp. ex. Bal. 0.20 1.8 2.0 0.0235 0.0076 0.0015 0.0019 0.3 Yes 215 Comp. ex. Bal. 0.20 4.4 2.0 0.0017 0.0143 0.0027 0.0016 0.1 Yes 216 Comp. ex. Bal. 0.20 0 2.0 0.0015 0.0090 0.0022 0.0022 0.1 Yes 217 Comp. ex. Bal. 0.20 1.7 6.0 0.1002 0.0166 0.0011 0.0021 0.1 Yes 218 Comp. ex. Bal. 0.20 1.7 0 0.0312 0.0084 0.0010 0.0023 0.1 Yes 219 Comp. ex. Bal. 0.40 1.5 2.0 0.0501 0.0233 0.0013 0.0020 2.5 Yes 220 Ex. Bal. 0.20 2.5 2.5 0.0255 0.0034 0.0010 0.0022 Cr: 1.00 0.2 Yes 221 Ex. Bal. 0.20 3.0 2.3 0.0221 0.0110 0.0027 0.0013 Cu: 0.01 0.2 Yes 222 Ex. Bal. 0.20 1.0 5.0 0.0311 0.0089 0.0044 0.0017 Ti: 0.030 0.1 Yes 223 Ex. Bal. 0.20 1.8 2.0 0.0334 0.0099 0.0021 0.0012 Ni: 0.90 0.1 Yes 224 Ex. Bal. 0.25 1.8 2.0 0.0401 0.0099 0.0024 0.0012 0.1 Yes 225 Ex. Bal. 0.25 1.8 2.0 0.0224 0.0100 0.0021 0.0015 Nb: 0.017 0.1 Yes 226 Ex Bal. 0.30 1.8 2.0 0.0222 0.0131 0.0021 0.0021 V: 0.046 0.1 Yes 227 Ex. Bal. 0.30 1.5 0.3 0.0267 0.0111 0.0021 0.0024 0.1 Yes 228 Ex. Bal. 0.35 1.5 3.0 0.0312 0.0109 0.0021 0.0022 Mo: 0.08 0.2 Yes 229 Ex. Bal. 0.35 1.5 2.0 0.0367 0.0099 0.0015 0.0021 W: 0.01 0.1 Yes 230 Ex. Bal. 0.40 1.5 2.0 0.3999 0.0076 0.0014 0.0015 0.4 Yes 231 Ex. Bal. 0.40 1.5 2.0 0.0242 0.0113 0.0018 0.0011 0.1 Yes 232 Ex. Bal. 0.40 1.5 2.0 0.0173 0.0142 0.0016 0.0017 0.1 Yes 233 Ex. Bal. 0.40 1.5 2.0 0.0288 0.0082 0.0014 0.0017 Ca: 0.001 0.1 Yes 234 Comp. ex. Bal. 0.40 1.6 2.0 0.0332 0.0111 0.0021 0.0016 0.1 Yes 235 Comp. ex. Bal. 0.20 1.0 2.3 0.0326 0.0114 0.0023 0.0023 0.2 No Form of internal oxides Annealing conditions Granular Grain Holding Holding Average Number boundary Dew point temp. time grain size density Ratio A No. Tension (? C.) (? C.) (s) (nm) (/?m.sup.2) (%) 201 Yes 0 840 120 210 2.0 0 202 Yes 0 840 80 250 4.2 89 203 Yes 0 840 80 210 6.1 88 204 Yes 0 800 80 240 5.0 85 205 Yes 0 840 80 170 5.4 84 206 Yes 0 840 80 150 4.1 86 207 Yes 0 820 120 250 10.2 100 208 Yes 0 840 120 230 14.1 95 209 Yes ?40 840 120 0 0 210 Yes 20 840 120 310 1.1 38 211 Yes 0 980 120 290 1.0 5 212 No 0 700 120 220 10.6 0 213 Yes 0 840 35 0 52 214 Yes 0 840 350 380 4.4 97 215 Yes 0 840 120 510 1.5 0 216 Yes 0 840 120 0 0 217 Yes 0 840 120 370 1.2 10 218 Yes 0 840 120 0 0 219 Yes 0 840 120 0 39 220 Yes 0 840 120 160 13.1 100 221 Yes 0 840 120 200 12.9 93 222 Yes 0 840 120 150 11.0 91 223 Yes 0 840 120 130 15.2 95 224 Yes 0 860 120 170 16.3 90 225 Yes 0 840 120 190 10.7 82 226 Yes 0 840 80 150 14.8 89 227 Yes 0 840 80 220 10.0 95 228 Yes 0 840 80 160 11.4 96 229 Yes 0 840 55 170 13.6 66 230 Yes 0 800 80 180 14.8 80 231 Yes 0 840 80 200 14.5 89 232 Yes 0 860 80 250 11.9 88 233 Yes 0 840 80 240 13.4 85 234 No 0 840 360 360 4.1 100 235 Yes 0 840 80 220 0.4 0 SiMn depleted layer Performance Depletion Hydrogen Thickness rate (%) Plating embrittlement LME No. (?m) Si Mn type Plateability resistance resistance 201 0.5 20 25 A A B B 202 6.5 3 4 A A A A 203 6.7 5 6 A A A A 204 6.9 7 2 A A A A 205 6.3 2 5 B A A A 206 7.7 5 7 A A A A 207 6.5 2 3 B A A A 208 6.3 2 3 C: 0.3 A A AA 209 A B B B 210 8.1 65 70 A B B B 211 10.5 20 23 A B B B 212 1.00 4 9 A A B A 213 3.1 12 18 A A B B 214 14.8 8 24 A A B B 215 1.5 80 76 A B B B 216 A A B B 217 7.1 76 65 A B B B 218 A A B B 219 4 96 95 A A B B 220 5.5 2 2 A A AA A 221 4.2 3 1 C: 0.8 A A AA 222 9.2 2 3 C: 1.5 A AA AA 223 7.2 3 2 A A AA A 224 7.5 2 1 A A AA A 225 7.4 3 2 A A AA A 226 7.1 7 6 A A AA A 227 5.5 9 7 C: 0.6 A A AA 228 8.5 5 8 C: 0.9 A AA AA 229 7.4 6 3 A A AA A 230 7 7 2 A A AA A 231 7.6 3 4 A A AA A 232 7.1 4 6 A A A A 233 7.9 5 7 A A A A 234 12.1 45 38 A A B B 235 2 95 98 A A B B
[0187] In each of Sample Nos. 202 to 208 and 220 to 233, the chemical composition of the steel sheet, the average grain size and number density of the granular oxides, and the thickness and composition of the SiMn depleted layer were suitable, so high plateability. LME resistance, and hydrogen embrittlement resistance were possessed. In Sample No. 201, the amount of C was insufficient and a sufficient strength was not obtained. Not only that the desired granular oxides were not formed and the desired SiMn depleted layer was also not formed, so high hydrogen embrittlement resistance and LME resistance were not obtained. In Sample No. 209, the dew point at the time of annealing was low and not internal oxides, but an external oxidation layer was formed, and high plateability, hydrogen embrittlement resistance, and LME resistance were not obtained. In Sample No. 210, the dew point at the time of annealing was high, an external oxidation layer was formed, granular oxides could not be refined, and high plateability, hydrogen embrittlement resistance, and LME resistance were not obtained. In Sample No. 211, the holding temperature at the time of annealing was high, external oxides were formed, granular oxides were not sufficiently formed, and the desired SiMn depleted layer was also not formed, so high plateability, hydrogen embrittlement resistance, and LME resistance were not obtained. In Sample No. 212, a predetermined tension was not applied at the time of annealing, so the desired SiMn depleted layer was not formed, and high hydrogen embrittlement resistance was not obtained. In Sample No. 213, the holding time at the time of annealing was short, internal oxides were not sufficiently formed, and the desired SiMn depleted layer was also not formed, so high hydrogen embrittlement resistance and LME resistance were not obtained. In each of Sample Nos. 214 and 234, the holding time at the time of annealing was long, granular oxides could not be refined, and the desired SiMn depleted layer was also not formed, so high hydrogen embrittlement resistance and LME resistance were not obtained. In Sample Nos. 215 and 217, the respective Si content and Mn content were excessive and, in each, the external oxides grew, further the granular oxides coarsened, and the desired SiMn depleted layer was also not formed, so high plateability, hydrogen embrittlement resistance, and LME resistance were not obtained. In Sample Nos. 216 and 218, the respective Si amount and Mn amount were 0 (zero) and in each an internal oxidation layer was not sufficiently formed and the desired SiMn depleted layer was also not formed, so high hydrogen embrittlement resistance and LME resistance were not 30) obtained. In Sample No. 219, the depth of the internal oxide layer before annealing was great, the desired internal oxides could not be formed after annealing, and the desired SiMn depleted layer was also not formed, so high hydrogen embrittlement resistance and LME resistance were not obtained. In Sample No. 235, grinding was not performed before annealing, so internal oxides were not sufficiently formed and the desired SiMn depleted layer was also not formed. As a result, high hydrogen embrittlement resistance and LME resistance were not obtained.
INDUSTRIAL APPLICABILITY
[0188] According to the present invention, high strength steel sheet and plated steel sheet having a high plateability, LME resistance, and hydrogen embrittlement resistance can be provided. The steel sheet and plated steel can be suitably used for automobiles, home electric appliances, building materials, and other applications, in particular for automobiles. As steel sheet for automobile use and plated steel sheet for automobile use, higher collision safety and longer life can be expected. Therefore, the present invention can be said to be extremely high in value in industry.
REFERENCE NOTATIONS
[0189] 1 steel sheet [0190] 2 external oxidation layer [0191] 3 base steel [0192] 11 steel sheet [0193] 12 granular oxides [0194] 13 grain boundary oxides [0195] 14 base steel