USPatent applicationPatented

Galvannealed layer and steel sheet comprising the same, and method for producing the same

Granted 24 Jan 2017 · 4 office actions

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Abstract

Provided are: a galvannealed steel sheet, improved in the adhesiveness of a plated layer with a base steel sheet, as a galvannealed steel sheet, prepared by using a high-strength steel sheet as a base material; and a method for producing the galvannealed steel sheet. A galvannealed layer is formed on the base steel sheet including a high-strength steel having a predetermined composition. The average amount of Fe in the galvannealed layer is 8.0 to 12.0%. The absolute value of a difference (ΔFe) between the amount of Fe in the vicinity of an interface with the base steel sheet and the amount of Fe in the vicinity of the external surface of the plated layer in the plated layer is 0.0 to 3.0%.

Description

17 parts
›This application is a national stage application of…

This application is a national stage application of International Application No. PCT/JP2012/069229, filed Jul. 27, 2012, which claims priority to Japanese Application No. 2011-167779, filed Jul. 29, 2011, each of which is incorporated by reference in its entirety.

›TECHNICAL FIELD

The present invention relates to a galvannealed layer and a plated steel sheet, the galvannealed layer being formed on a surface of a high-strength steel sheet as a base material. In particular, the present invention relates to a galvannealed layer and a plated steel sheet, improved in the adhesiveness of a galvanized layer with a base steel sheet, and to a method for producing the galvannealed layer.

›BACKGROUND ART

In recent years, the higher strength of steel sheets used in various components and structures, such as automotive outside sheets (body sheets), construction machines, and, in addition, building and civil engineering structures, has been increasingly demanded, and a high-strength steel sheet with a maximum tensile stress of 900 MPa or more has also been used. Further, the steel sheets having such uses usually need excellent corrosion resistance because of often being used outdoors.

Conventionally, as steel sheets having such uses, hot dip galvanized steel sheets subjected to hot dip galvanizing have been widely used. Recently, there a galvannealed steel sheet subjected to alloying treatment including hot dip galvanizing, thereafter heating a plated layer to a temperature that is not less than the melting point of Zn to diffuse Fe from a base steel sheet into the plated layer, and forming the plated layer as a layer based on a Zn—Fe alloy has also been widely used. Such a galvannealed steel sheet is known to have excellent surface appearance and corrosion resistance, compared with a hot dip galvanized steel sheet that is not subjected to the alloying treatment.

However, in uses for automotive outside sheets and the like, the periphery of a sheet is usually subjected to severe bending working (hemming) by press working; and, in not only the automotive outside sheets but also in other uses, such a sheet, subjected to severe bending working, bore-expanding working, or the like by press working, is often used. In addition, when a conventional galvannealed steel sheet is subjected to severe bending working, bore-expanding working, or the like, a plated layer might peel from a base steel sheet in a portion worked in such a manner. When the plated layer peels off in such a manner, there is a problem that the corrosion resistance of an area where the plated layer peels off is lost to early corrode and rust the base steel sheet. Even when the plated layer does not peel off, lose of adhesiveness between the plated layer and the base steel sheet to produce even a few voids in an area where the adhesiveness is lost causes outside air and moisture to enter the voids, the anticorrosion function of the plated layer to be lost, and the base steel sheet to be early corroded and rusted in the same manner as described above. Thus, there has been a strong desire to develop a galvannealed layer and a plated steel sheet, having the excellent adhesiveness of the plated layer with a base steel sheet, for uses in which such severe bending working or the like is performed.

There have already been proposed various ways for improving the adhesiveness of a plated layer with a base steel sheet in a galvannealed steel sheet, and some examples thereof are described in Patent Literatures 1 to 8.

›CITATION LIST

Patent Literature

[Patent Literature 1]Japanese Laid-open Patent Publication No. 2009-68061

[Patent Literature 2]Japanese Laid-open Patent Publication No. 2008-26678

[Patent Literature 3]Japanese Laid-open Patent Publication No. 2005-256041

[Patent Literature 4]Japanese Laid-open Patent Publication No. 2002-173756

[Patent Literature 5]Japanese Laid-open Patent Publication No. 9-13147

[Patent Literature 6]Japanese Laid-open Patent Publication No. 6-235077

[Patent Literature 7]Japanese Laid-open Patent Publication No. 2002-146503

[Patent Literature 8]Japanese Laid-open Patent Publication No. 5-311371

›SUMMARY OF INVENTION · 1 of 2

Technical Problem

As mentioned above, a galvannealed layer and a plated steel sheet, subjected to bending working or the like and used, desirably have the excellent adhesiveness of a plated layer with a base steel sheet; however, conventional manners for improving adhesiveness, as described in Patent Literatures 1 to 8, have been still insufficient, and it has been difficult to reliably and stably prevent the plated layer from peeling off particularly when the galvannealed layer and the plated steel sheet are subjected to very severe working such as hemming working or bore-expanding working and are used.

For example, Patent Literature 7 describes that the recesses and projections of a plating coating can be eliminated by bending working or the like prior to hot dip galvanizing. This is presumed to be because a large number of preferred nucleation sites are generated in a base material interface by bending working or the like prior to plating, to accelerate alloying. However, there is neither a description nor a suggestion that the concentration of Fe in a plated layer is controlled by bending working after a plating treatment step.

Further, Patent Literature 8 describes that an alloying rate can be improved by bending working in alloying by heating after plating. This is because Fe—Al—Zn which decreases a Fe—Zn alloying rate is cracked by bending working, to accelerate Fe—Zn alloying. However, temperature in alloying by heating is not described at all, and there is nether description nor suggestion that the concentration of Fe in a plated layer is controlled by adjusting temperature.

The present invention was accomplished with respect to the above circumstances as a background and is directed at providing a galvannealed layer and a plated steel sheet, reliably and sufficiently improved in the adhesiveness of a plated layer with a base steel sheet, as a galvannealed layer and a plated steel sheet, prepared by using a high-strength steel sheet as a base material and at providing a method for producing the galvannealed layer.

Solution to Problem

As a result of repeating various experiments and examinations of the adhesiveness of a plated layer in a galvannealed steel sheet, the present inventors found that in a hot dip galvanized layer that is alloyed, the concentration gradient of the amount of Fe in the thickness direction of the plated layer has a great influence on the adhesiveness of the plated layer with a base steel sheet. In other words, when the hot dip galvanized layer is subjected to alloying treatment, Fe diffuses from the inside of the base steel sheet into the plated layer and the plated layer has a Zn—Fe alloy-based structure; however, in this case, since the diffusion of Fe proceeds from a side closer to the base steel sheet, the concentration of Fe in the plated layer after the alloying treatment is usually higher in the side closer to the base steel sheet and lower in a side closer to the external surface of the plated layer. On the other hand, the Zn—Fe alloy that forms the alloyed galvanized layer is softer with decreasing the concentration of Fe but is brittler with increasing the concentration of Fe. Therefore, by decreasing the concentration of Fe in the vicinity of the external surface due to the concentration gradient of Fe as mentioned above, the external surface is softened during press working and therefore adheres to a die causing flaking. In contrast, when the concentration of Fe is increased in the vicinity of an interface with the base steel sheet due to the above-mentioned Fe concentration gradient to make the vicinity brittle, the plated layer is fractured in the region by severe working, easily causing powdering.

As a result of further pursuing experiments and examinations based on such findings, it was found that, by performing treatment in which Fe in a plated layer is diffused in the layer while preventing Fe from diffusing from a base steel sheet into the plated layer as much as possible after alloying treatment of a hot dip galvanized layer, the concentration gradient of Fe in the plated layer can be reduced (the gradient of the concentration of Fe is flattened) to equalize the concentration of Fe in the plated layer to optimal concentration (around 10%), at which peeling resistance is excellent, in any portion in the thickness direction thereof, to thereby more greatly improve the adhesiveness of the galvannealed layer with the base steel sheet than ever before, and the present invention was thus accomplished.

The present invention was accomplished based on such novel findings as described above and is to basically provide a galvannealed layer and a plated steel sheet, improved in the adhesiveness of the plated layer with a base steel sheet, by flattening the concentration gradient of Fe in the plated layer of the plated steel sheet in which the galvannealed layer is formed on a surface of a high-strength steel sheet as a base material. Further, the present invention is to provide a method for producing a galvannealed layer, including a treatment step for reducing the concentration gradient of Fe in a hot dip galvanized layer.

Accordingly, the present invention is summarized as follows:

(1) A galvannealed layer formed on a surface of a base steel sheet, wherein the average amount of Fe in the galvannealed layer is in a range of 8.0 to 12.0%; and the absolute value of a difference ΔFe between the amount of Fe at a position of ⅛ of the thickness of the plated layer (the amount of Fe in the vicinity of an internal side) and the amount of Fe at a position of ⅞ of the thickness of the plated layer (the amount of Fe in the vicinity of an external side) in the galvannealed layer, the thickness being from an interface between the galvannealed layer and the base steel sheet to the external surface of the plated layer, is in a range of 0.0 to 3.0%.

(2) A galvannealed steel sheet, wherein the galvannealed layer according to (1) is formed on a surface of a base steel sheet including, in mass %,

›SUMMARY OF INVENTION · 2 of 2

C: 0.050 to 0.300%,

Si: 0.10 to 2.50%,

Mn: 0.50 to 3.50%,

P: 0.001 to 0.030%,

S: 0.0001 to 0.0100%,

Al: 0.005 to 1.500%,

O: 0.0001 to 0.0100%,

N: 0.0001 to 0.0100%, and

the balance of Fe and unavoidable impurities.

(3) The galvannealed steel sheet according to the above (2), wherein the base steel sheet further includes, in mass %, one or two or more selected from

Cr: 0.01 to 2.00%,

Ni: 0.01 to 2.00%,

Cu: 0.01 to 2.00%,

Ti: 0.005 to 0.150%,

Nb: 0.005 to 0.150%,

V: 0.005 to 0.150%,

Mo: 0.01 to 1.00%, and

B: 0.0001 to 0.0100%.

(4) The galvannealed steel sheet according to the above (2) or (3), wherein the base steel sheet further includes 0.0001 to 0.5000% in total of one or two or more selected from Ca, Ce, Mg, Zr, Hf, and REM.

(5) The galvannealed steel sheet according to any of the above (2) to (4), wherein a coating including a P oxide and/or a complex oxide containing P is formed on a surface of the galvannealed layer.

(6) A method for producing a galvannealed layer, including: in mass %,

a hot dip galvanizing step for subjecting a surface of a base steel sheet to hot dip galvanizing to obtain a hot dip galvanized steel sheet;

an alloying treatment step for heating a hot dip galvanized layer, formed in the hot dip galvanizing step, to a temperature in a range of 470 to 650° C. to form a galvannealed layer and to produce a galvannealed steel sheet; and

an intra-galvannealed-layer diffusion treatment step for, after the alloying treatment step, allowing the galvannealed steel sheet to stay at a temperature in a range of 250 to 450° C. and subjecting the galvannealed steel sheet to one or more times of bending-unbending working in the temperature range to diffuse Fe in the galvannealed layer.

(7) The method for producing a galvannealed layer according to the above (6), wherein the galvannealed steel sheet is obtained, in which, after the intra-galvannealed-layer diffusion treatment step, the average amount of Fe in the galvannealed layer is in a range of 8.0 to 12.0%; and the absolute value of a difference ΔFe between the amount of Fe at a position of ⅛ of the thickness of the plated layer (the amount of Fe in the vicinity of an internal side) and the amount of Fe at a position of ⅞ of the thickness of the plated layer (the amount of Fe in the vicinity of an external side) in the galvannealed layer, the thickness being from an interface between the galvannealed layer and the base steel sheet to the external surface of the plated layer, is in a range of 0.0 to 3.0%.

(8) The method for producing a galvannealed layer according to the above (6) or (7), wherein in the intra-galvannealed-layer diffusion treatment step, the bending working is performed so that a maximum tensile strain amount in a surface of the steel sheet ranges from 0.0007 to 0.0910.

(9) The method for producing a galvannealed steel sheet according to any of the above (6) to (8), wherein a surface of the galvannealed layer is subjected to phosphate coating treatment for forming a coating including a P oxide and/or a complex oxide containing P after the intra-galvannealed-layer diffusion treatment step.

(10) The method for producing a galvannealed layer according to any of (6) to (9), wherein a base steel sheet including, in mass %,

C: 0.050 to 0.300%,

Si: 0.10 to 2.50%,

Mn: 0.50 to 3.50%,

P: 0.001 to 0.030%,

S: 0.0001 to 0.0100%,

Al: 0.005 to 1.500%,

O: 0.0001 to 0.0100%,

N: 0.0001 to 0.0100%, and

the balance of Fe and unavoidable impurities is used as the base steel sheet.

(11) The method for producing a galvannealed layer according to the above (10), wherein the steel sheet further including, in mass %, one or two or more selected from

Cr: 0.01 to 2.00%,

Ni: 0.01 to 2.00%,

Cu: 0.01 to 2.00%,

Ti: 0.005 to 0.150%,

Nb: 0.005 to 0.150%,

V: 0.005 to 0.150%,

Mo: 0.01 to 1.00%, and

B: 0.0001 to 0.0100%

is used as the base steel sheet.

(12) The method for producing a galvannealed layer according to any of the above (10) to (11), wherein the steel sheet further including, in mass %, 0.0001 to 0.5000% in total of one or two or more selected from Ca, Ce, Mg, Zr, Hf, and REM is used as the base steel sheet.

Advantageous Effects of Invention

In accordance with the present invention, a galvanized layer and a plated steel sheet, reliably and sufficiently improved in the adhesiveness of a plated layer with a base steel sheet, can be obtained as a galvannealed layer and a plated steel sheet, in which a steel sheet, particularly a high-strength steel sheet is used as a base material, and therefore, the plated layer can be effectively prevented from being fractured and peeling even in uses subjected to severe working such as bending working or bore-expanding working.

›BRIEF DESCRIPTION OF DRAWINGS

FIG. 1 is a graph that indicates a relationship of the average amount of Fe and the absolute value of the amount of ΔFe in a plated layer and the appearance of the plated layer.

FIG. 2 is a graph that indicates a relationship between tensile strength and an elongation in the galvannealed steel sheet according to the present invention.

›DESCRIPTION OF EMBODIMENTS · 1 of 7

The present invention will be explained in detail below.

In the galvannealed layer and plated steel sheet of the present invention, basically, a high-strength steel sheet having a predetermined component composition is used as a base material and a galvannealed layer is formed on the surface of the base steel sheet. In addition, particularly as for the galvannealed layer, not only the average amount of Fe in the plated layer is specified but also a Fe concentration distribution (Fe concentration gradient) in the thickness direction of the plated layer is specified.

In other words, the galvannealed layer is an alloy layer formed by alloying treatment including forming a Zn plated layer on the surface of the base steel sheet by hot dip galvanizing and thereafter reheating the plated layer to a temperature that is not less than the melting point of Zn to diffuse Fe in the base steel sheet in the plated layer and has a structure based on a Zn—Fe alloy. In the present invention, the average amount of Fe in the galvannealed layer is, in mass %, in the range of 8.0 to 12.0%, and the absolute value of the difference ΔFe between the amount of Fe in the vicinity of the external side and the amount of Fe in the vicinity of the internal side is specified in the range of 0.0 to 3.0% as a Fe concentration gradient condition in the thickness direction in the galvannealed layer. Thus, the limitation reasons of the conditions will be explained.

[Average Amount of Fe in Plated Layer: 8.0 to 12.0%]

When the average amount of Fe in the galvannealed layer is less than 8.0%, the plated layer becomes soft and easily adheres to a die for press working, and therefore, flaking (flaky peeling) easily occurs during press working. Thus, the average amount of Fe in the plated layer is preferably 8.0% or more from the viewpoint of flaking resistance. Preferably, the average amount of Fe is 9.0% or more. On the other hand, the average amount of Fe in the galvannealed layer is more than 12.0%, the plated layer becomes brittle and is easily fractured, and powdering (powdery peeling) easily occurs during press working. Thus, the average amount of Fe in the plated layer is preferably 12.0% or less from the viewpoint of powdering resistance. Preferably, the average amount of Fe is 11.0% or less. Thus, an average Fe concentration in a range of 8.0 to 12.0%, preferably in a range of 9.0 to 11.0%, causes both flaking and powdering to hardly occur and the adhesiveness of the plated layer to become good.

[Condition of Fe Concentration Gradient in Plated Layer: Absolute Value of ΔFe of 0.0 to 3.0%]

As mentioned above, in a hot dip galvanized layer subjected to alloying treatment, a Fe concentration gradient usually exists in the thickness direction thereof. In the Fe concentration gradient, there is a general tendency for the concentration of Fe to be high in the vicinity of an interface with a base steel sheet and for the concentration of Fe to be low in the vicinity of the external surface of the plated layer. In a region in the vicinity of the surface, in which the concentration of Fe is low, the plated layer becomes soft to adhere to a die during press working and flaking peeling easily occurs. On the other hand, in the vicinity of the interface with the base steel sheet, in which the concentration of Fe is low, the plated layer becomes brittle and powdering peeling easily occurs. Accordingly, in any case, peeling of the plated layer easily occurs when severe working is performed. Thus, in the present invention, the Fe concentration gradient in the plated layer is reduced to specify a Fe concentration gradient condition so that the optimal concentration of Fe (8.0 to 12.0%, preferably 9.0 to 11.0%) at which flaking or powdering hardly occurs in any portion in the thickness direction thereof is achieved. In other words, it is specified that the absolute value of the difference ΔFe between the amount of Fe in the vicinity of the interface with the base steel sheet (the amount of Fe in the vicinity of the internal side) and the amount of Fe in the vicinity of the external surface of the plated layer (the amount of Fe in the vicinity of the external side) is in the range of 0.0 to 3.0%. The amount of Fe in the vicinity of the internal side means the amount of Fe at the position of ⅛ of the total thickness of the plated layer from the interface with the base steel sheet to the external surface of the plated layer, while the amount of Fe in the vicinity of the external side means the amount of Fe at the position of ⅞ of the total thickness of the plated layer from the interface with the base steel sheet to the external surface of the plated layer (i.e., the position of ⅛ of the total thickness of the plated layer from the external surface of the plated layer to the interface with the base steel sheet).

The absolute value of ΔFe of more than 3.0% results in the insufficient effect of improving the adhesiveness of the plated layer. Thus, it is specified that the absolute value of ΔFe is in the range of 0.0 to 3.0%. The absolute value of ΔFe of 3.0% or less results in less possibility that peeling due to flaking or powdering occurs in the plated layer even when severe working is performed, so that the adhesiveness of the plated layer is improved. In addition, for more reliably obtaining the adhesiveness improvement effect, the absolute value of ΔFe is preferably 2.0% or less, further more preferably 1.5% or less.

In addition, the coating amount of the galvannealed layer is not particularly limited but is desirably 20 g/m 2 or more from the viewpoint of corrosion resistance and 150 g/m 2 or less from the viewpoint of economical efficiency.

Furthermore, the galvannealed layer is prepared by alloying Fe based on Zn; however, even when the galvannealed layer contains Zn and Fe as well as a small amount of one or two or more of Al, Pb, Sb, Si, Sn, Mg, Mn, Ni, Cr, Co, Ca, Cu, Li, Ti, Be, Bi, Sr, I, Cs, and REM, the effects of the present invention are not deteriorated and a preferable effect such as improvement of corrosion resistance or workability may be provided depending on the amount.

›DESCRIPTION OF EMBODIMENTS · 2 of 7

The limitation reasons of the component composition of the steel sheet used as the base material for the galvannealed steel sheet of the present invention will be explained below. In the following description, all “%” represents mass %.

[C: 0.050 to 0.300%]

C is contained for increasing the strength of a high-strength steel sheet. However, a C content of more than 0.300% results in insufficient weldability. The content of C is preferably 0.250% or less, more preferably 0.220% or less, from the viewpoint of weldability. On the other hand, a C content of less than 0.050% results in decreased strength and precludes securing of a maximum tensile strength of 900 MPa or more. The content of C is preferably 0.075% or more, more preferably 0.100% or more, for more further enhancing strength.

[Si: 0.10 to 2.50%]

Si is an element that suppresses generation of an iron-based carbide in a steel sheet and enhances strength and moldability. However, a Si content of more than 2.50% results in embrittlement of the steel sheet and in deterioration of ductility. The content of Si is preferably 2.20% or less, more preferably 2.00% or less, from the viewpoint of ductility. On the other hand, a Si content of less than 0.10% results in generation of a large amount of coarse iron-based carbide during alloying treatment of a plated layer and in deterioration of strength and moldability. From the viewpoint of the above, the lower limit of Si is preferably 0.30% or more, more preferably 0.45% or more.

[Mn: 0.50 to 3.50%]

Mn is added for enhancing the strength of a steel sheet. However, a Mn content of more than 3.50% results in generation of a coarse Mn-concentrated unit in the center in the sheet thickness of the steel sheet to cause embrittlement to easily occur and to cause a trouble such as braking of a cast slab to easily occur. A Mn content of more than 3.50% also results in deterioration of weldability. Accordingly, the content of Mn is preferably 3.50% or less. The content of Mn is preferably 3.20% or less, more preferably 3.00% or less, from the viewpoint of weldability. On the other hand, since a Mn content of less than 0.50% results in formation of a large amount of soft structure during cooling after annealing, to thereby preclude securing of a maximum tensile strength of 900 MPa or more, the content of Mn is preferably 0.50% or more. The content of Mn is preferably 1.50% or more, more preferably 1.70% or more, for further enhancing strength.

[P: 0.001 to 0.030%]

P tends to segregate in the center in the sheet thickness of a steel sheet and embrittles a weld. Since a P content of more than 0.030% results in great embrittlement of the weld, the upper limit of the content of P is 0.030%. On the other hand, since a P content of less than 0.001% results in a greatly increased production cost, the lower limit thereof is 0.001%.

[S: 0.0001 to 0.0100%]

S adversely affects weldability as well as productability in casting and hot rolling. Thus, the upper limit of the content of S is 0.0100% or less. Further, S is bound to Mn to form MnS which is coarse and to deteriorate ductility and stretch flanging properties and is therefore preferably 0.0050% or less, more preferably 0.0025% or less. On the other hand, since a S content of less than 0.0001% results in a greatly increased production cost, the lower limit thereof is 0.0001%.

[Al: 0.005 to 1.500%]

Al suppresses generation of an iron-based carbide and enhances the strength and moldability of a steel sheet. However, an Al content of more than 1.500% results in deteriorated weldability and the upper limit of the content of Al is therefore 1.500%. From the viewpoint of the above, the content of Al is preferably 1.200% or less, more preferably 0.900% or less. Al is also an element that is effective as a deoxidation material; however, since an Al content of less than 0.005% results in an insufficient effect as the deoxidation material, the lower limit of the content of Al is 0.005%. The amount of Al is preferably 0.010% or more for more sufficiently obtaining a deoxidation effect.

[N: 0.0001 to 0.0100%]

Since N forms a coarse nitride and deteriorates ductility and stretch flanging properties, the amount of added N is preferably reduced. Since a N content of more than 0.0100% results in the significant tendency of the above, the upper limit of the content of N is 0.0100%. Since N also causes generation of blowholes in welding, the lower content thereof is better. The effects of the present invention are exerted even when the lower limit of the content of N is not particularly specified; however, since a N content of less than 0.0001% results in a greatly increased production cost, the N content is 0.0001% or more.

[O: 0.0001 to 0.0100%]

Since O forms an oxide and deteriorates ductility and stretch flanging properties, the content thereof is preferably reduced. Since an O content of more than 0.0100% results in significant deterioration of stretch flanging properties, the upper limit of the content of O is 0.0100%. Furthermore, the content of O is preferably 0.0080% or less, more preferably 0.0060% or less. The effects of the present invention are exerted even when the lower limit of the content of O is not particularly specified; however, since an O content of less than 0.0001% results in a greatly increased production cost, the lower limit is 0.0001%.

In addition, elements described below may be optionally added to the base steel sheet for the galvannealed steel sheet of the present invention.

[Cr: 0.01 to 2.00%]

Cr is an element that suppresses phase transformation at high temperature and is effective for higher strength and may be added instead of part of C and/or Mn. Since a Cr content of more than 2.00% results in deteriorated hot workability to reduce productivity, the content of Cr is 2.00% or less. Although the effects of the present invention are exerted even when the lower limit of the content of Cr is not particularly specified, the content of Cr is preferably 0.01% or more for sufficiently obtaining the effect of achieving higher strength by adding Cr.

›DESCRIPTION OF EMBODIMENTS · 3 of 7

[Ni: 0.01 to 2.00%]

Ni is an element that suppresses phase transformation at high temperature and is effective for higher strength and may be added instead of part of C and/or Mn. Since a Ni content of more than 2.00% results in deteriorated weldability, the content of Ni is 2.00% or less. Although the effects of the present invention are exerted even when the lower limit of the content of Ni is not particularly specified, the content of Ni is preferably 0.01% or more for sufficiently obtaining the effect of achieving higher strength by adding Ni.

[Cu: 0.01 to 2.00%]

Cu is an element that exists as fine particles in a steel to thereby enhance strength and can be added instead of part of C and/or Mn. Since a Cu content of more than 2.00% results in deteriorated weldability, the content of Cu is 2.00% or less. Although the effects of the present invention are exerted even when the lower limit of the content of Cu is not particularly specified, the content of Cu is preferably 0.01% or more for sufficiently obtaining the effect of achieving higher strength by adding Cu.

[Ti: 0.005 to 0.150%]

Ti is an element that contributes to increase in the strength of a steel sheet by precipitate strengthening, fine grain strengthening due to suppression of ferrite crystal grain growth, and dislocation strengthening through suppression of recrystallization. However, since a Ti content of more than 0.150% results in increase in precipitated carbonitrides to deteriorate moldability, the content of Ti is 0.150% or less. The content of Ti is more preferably 0.100% or less, further preferably 0.070% or less, from the viewpoint of moldability. Although the effects of the present invention are exerted even when the lower limit of the content of Ti is not particularly specified, the content of Ti is preferably 0.005% or more for sufficiently obtaining the effect of increasing strength by adding Ti. The content of Ti is more preferably 0.010% or more, further preferably 0.015% or more, for further achieving the higher strength of the steel sheet.

[Nb: 0.005 to 0.150%]

Nb is an element that contributes to increase in the strength of a steel sheet by precipitate strengthening, fine grain strengthening due to suppression of ferrite crystal grain growth, and dislocation strengthening through suppression of recrystallization. However, since a Nb content of more than 0.150% results in increase in precipitated carbonitrides to deteriorate moldability, the content of Nb is 0.150% or less. The content of Nb is more preferably 0.100% or less, further preferably 0.060% or less, from the viewpoint of moldability. Although the effects of the present invention are exerted even when the lower limit of the content of Nb is not particularly specified, the content of Nb is preferably 0.005% or more for sufficiently obtaining the effect of increasing strength by adding Nb. The content of Nb is more preferably 0.010% or more, further preferably 0.015% or more, for further achieving the higher strength of the steel sheet.

[V: 0.005 to 0.150%]

V is an element that contributes to increase in the strength of a steel sheet by precipitate strengthening, fine grain strengthening due to suppression of ferrite crystal grain growth, and dislocation strengthening through suppression of recrystallization. However, since a V content of more than 0.150% results in an increase in precipitated carbonitrides to deteriorate moldability, the content of V is 0.150% or less. Although the effects of the present invention are exerted even when the lower limit of the content of V is not particularly specified, the content of V is preferably 0.005% or more for sufficiently obtaining the effect of increasing strength by adding V.

[Mo: 0.01 to 1.00%]

Mo is an element that suppresses phase transformation at high temperature and is effective for higher strength and may be added instead of part of C and/or Mn. Since a Mo content of more than 1.00% results in deteriorated hot workability to reduce productivity, the content of Mo is 1.00% or less. Although the effects of the present invention are exerted even when the lower limit of the content of Mo is not particularly specified, the content of Mo is preferably 0.01% or more for sufficiently obtaining the effect of achieving higher strength by adding Mo.

[W: 0.01 to 1.00%]

W is an element that suppresses phase transformation at high temperature and is effective for higher strength and may be added instead of part of C and/or Mn. Since a W content of more than 1.00% results in deteriorated hot workability to reduce productivity, the content of W is preferably 1.00% or less. Although the effects of the present invention are exerted without particularly specifying the lower limit of the content of W, the content of W is preferably 0.01% or more for sufficiently obtaining higher strength due to W.

[B: 0.0001 to 0.0100%]

B is an element that suppresses phase transformation at high temperature and is effective for higher strength and may be added instead of part of C and/or Mn. Since a B content of more than 0.0100% results in deteriorated hot workability to reduce productivity, the content of B is 0.0100% or less. The content of B is more preferably 0.0050% or less, further preferably 0.0030% or less, from the viewpoint of productivity. Although the effects of the present invention are exerted even when the lower limit of the content of B is not particularly specified, the content of B is preferably 0.0001% or more for sufficiently obtaining the effect of achieving higher strength by adding B. The content of B is more preferably 0.0003% or more, more preferably 0.0005% or more, for further higher strength.

Furthermore, 0.0001 to 0.5000% in total of one or two or more of Ca, Ce, Mg, Zr, Hf, and REM as additional elements may be added to the base steel sheet in the galvannealed steel sheet of the present invention. The reason of adding the elements is as described below.

Ca, Ce, Mg, Zr, Hf, and REM are elements effective for improving moldability and one or two or more thereof can be added. However, since a total of the contents of one or two or more of Ca, Ce, Mg, Zr, Hf, and REM of more than 0.5000% may rather result in deteriorated ductility, the total of the contents of the respective elements is preferably 0.5000% or less. Although the effects of the present invention are exerted even when the lower limit of the content of one or two or more of Ca, Ce, Mg, Zr, Hf, and REM is not particularly specified, the total of the contents of the respective elements is preferably 0.0001% or more for sufficiently obtaining the effect of improving the moldability of a steel sheet. The total of the contents of one or two or more of Ca, Ce, Mg, Zr, Hf, and REM is preferably 0.0005% or more, further preferably 0.0010% or more, from the viewpoint of moldability. REM is an abbreviation for Rare Earth Metal and refers to an element belonging to the lanthanide series. In the present invention, REM and Ce are often added in a misch metal, which may contain a lanthanide series element as well as La and Ce in a complex. The effects of the present invention are exerted even when the lanthanide series element as well as La and Ce described above are contained as unavoidable impurities. Further, the effects of the present invention are exerted even when metal La and Ce are added.

›DESCRIPTION OF EMBODIMENTS · 4 of 7

The balance other than the above respective elements may be Fe and unavoidable impurities. In addition, each of Cr, Ni, Cu, Ti, Nb, V, Mo, W, and B mentioned above may be contained as an impurity in a minute amount less than the lower limit thereof. Ca, Ce, Mg, Zr, Hf, and REM may also be contained as impurities in a trace amount less than the lower limit of the total amount thereof.

The structure of the high-strength steel sheet used as the base material for the galvannealed steel sheet of the present invention will be explained below.

The high-strength steel sheet used as the base material for the galvannealed steel sheet of the present invention preferably includes, by volume fraction, ferrite: 10 to 75%, bainitic ferrite and/or bainite: 10 to 50%, tempered martensite: 10 to 50%, fresh martensite: 15% or less, and retained austenite: 20% or less as the microstructures thereof in the range of ⅛ to ⅜ of a sheet thickness assuming that ¼ of the thickness is a center. When the high-strength steel sheet as the base material has such structures, the galvannealed steel sheet having superior moldability is made. Thus, the preferred conditions of each of the structures will be explained below.

[Ferrite: 10 to 75%]

Ferrite is a structure effective for improving ductility and is preferably contained in a volume fraction of 10 to 75% in a steel sheet structure. A volume fraction of ferrite of less than 10% may result in insufficient ductility. Ferrite is more preferably contained in the steel sheet structure in a volume fraction of 15% or more, further preferably 20% or more, from the viewpoint of ductility. On the other hand, since ferrite is a soft structure, a volume fraction of ferrite of more than 75% may result in insufficient strength. The volume fraction of ferrite contained in the steel sheet structure is preferably 65% or less, further preferably 50% or less, for enhancing the tensile strength of the steel sheet.

[Bainitic Ferrite and/or Bainite: 10 to 50%]

Bainitic ferrite and/or bainite are structures excellent in balance between strength and ductility and are preferably contained in a volume fraction of 10 to 50% in a steel sheet structure. Further, bainitic ferrite and/or bainite are microstructures having strength between those of soft ferrite and hard martensite and between those of tempered martensite and retained austenite and are more preferably contained in 15% or more, further preferably contained in 20% or more, from the viewpoint of bendability and stretch flanging properties. On the other hand, a volume fraction of bainitic ferrite and/or bainite of more than 50% is not preferred because of resulting in excessively increased yield stress and deteriorated shape fixability.

[Tempered Martensite: 10 to 50%]

Tempered martensite is a structure that greatly improves tensile strength and may be contained in a volume fraction of 50% or less in a steel sheet structure. The volume fraction of tempered martensite is preferably 10% or more from the viewpoint of tensile strength. On the other hand, a volume fraction of tempered martensite contained in the steel sheet structure, of more than 50%, is not preferred because of resulting in excessively increased yield stress and deteriorated shape fixability.

[Fresh Martensite: 15% or Less]

Fresh martensite greatly improves tensile strength but becomes a fracture origin to greatly deteriorate bendability, and the volume fraction thereof is therefore preferably limited to 15% or less in a steel sheet structure. The volume fraction of fresh martensite is more preferably 10% or less, further preferably 5% or less, for enhancing bendability and stretch flanging properties.

[Retained Austenite: 20% or Less]

Retained austenite greatly improves strength and ductility and may be therefore contained in an amount having an upper limit of 20% in a steel sheet. On the other hand, retained austenite becomes a fracture origin to greatly deteriorate stretch flanging properties, and the volume fraction thereof is therefore preferably 17% or less, more preferably 15% or less.

[Other Structures]

The steel sheet structure of the high-strength steel sheet as the base material in the present invention may contain structures other than the above, such as pearlite and/or coarse cementite. However, bendability is deteriorated when there is a large amount of pearlite and/or coarse cementite in the steel sheet structure of the high-strength steel sheet. Thus, the total volume fraction of pearlite and/or coarse cementite contained in the steel sheet structure is preferably 10% or less, more preferably 5% or less.

The volume fraction of each structure contained in the steel sheet structure of the high-strength steel sheet used as the base material in the present invention can be measured, e.g., by a method described below.

For the volume fraction of retained austenite, X-ray analysis is performed with a surface that is parallel to the sheet surface of the steel sheet and is at ¼ of the thickness thereof as an observation surface, to calculate an area fraction, which can be regarded as the volume fraction.

For the volume fraction of each of the structures, i.e., ferrite, bainitic ferrite, bainite, tempered martensite, and fresh martensite, a sample is collected with a cross section in the sheet thickness parallel to the direction of rolling the steel sheet as an observation surface, the observation surface is polished and nital-etched, and the range of ⅛ to ⅜ of a the thickness, assuming that ¼ of the thickness is a center, is observed with a field emission scanning electron microscope (FE-SEM) to measure an area fraction, which can be regarded as the volume fraction.

The method for producing a galvannealed layer and a plated steel sheet of the present invention will be explained below.

In the production method of the present invention, steps before obtaining the base steel sheet are not particularly limited, and thus, each step for forming the galvannealed layer on the base steel sheet having a predetermined sheet thickness is first explained. However, each step for forming the galvannealed layer can also be incorporated into an annealing step after cold rolling in a process for producing the base steel sheet, particularly a cooling process thereof, and the above points will be re-explained later with the explanation of the method of producing the base steel sheet.

›DESCRIPTION OF EMBODIMENTS · 5 of 7

In the method for producing a galvannealed layer and a plated steel sheet of the present invention, the process for forming the galvannealed layer on the surface of the base steel sheet basically includes a hot dip galvanizing step, an alloying treatment step, and an intra-plated-layer diffusion treatment step. In some cases, a phosphate coating formation treatment may also be performed after the intra-plated-layer diffusion treatment step. The conditions of the steps will be explained below.

[Hot Dip Galvanizing Step]

The hot dip galvanizing may be performed by continuously or discontinuously dipping the base steel sheet in a hot dip galvanizing bath in the same manner as a known technique. The temperature of the hot dip galvanizing bath in the performance is basically preferably not less than the melting point (about 420° C.) of Zn; however, since Zn may be locally solidified due to bath temperature fluctuation to make an operation unstable when the temperature is almost the melting point, the temperature is usually preferably 440° C. or more. On the other hand, since a bath temperature of more than 480° C. may result in generation of a Fe—Al—Zn phase which inhibits alloying, the temperature is usually preferably 480° C. or less. In addition, there is no particular problem even when Zn and a small amount of one or two or more of Al, Pb, Sb, Si, Sn, Mg, Mn, Ni, Cr, Co, Ca, Cu, Li, Ti, Be, Bi, Sr, I, Cs, and REM are contained or mixed in the hot dip galvanizing bath, and a preferable effect such as improvement of corrosion resistance or workability may be provided depending on the amount, as mentioned above.

In addition, the coating weight of plating metal in galvannealing is preferably 20 g/m 2 or more from the viewpoint of corrosion resistance and preferably 150 g/m 2 or less from the viewpoint of economical efficiency, and dipping time (sheet leaping rate), bath temperature, and the like may be appropriately adjusted so that such a coating weight is achieved.

[Alloying Treatment Step]

The alloying treatment step is a step for diffusing Fe from the base steel sheet into the hot dip galvanized layer formed on the surface of the base steel sheet in the preceding step and may include heating to a temperature in a range of 470 to 650° C. to maintain the temperature in the range or heating to a temperature in a range of 470 to 650° C. to perform annealing to the solidification temperature (about 420° C.) of Zn. When the heating temperature for the alloying treatment is less than 470° C., it becomes difficult to sufficiently diffuse Fe in the base steel sheet into the plated layer or long time is needed for diffusing a sufficient amount of Fe, to deteriorate productivity. On the other hand, when the heating temperature for the alloying treatment is more than 650° C., a problem that a coarse iron-based carbide is generated in the steel sheet occurs. Thus, the heating temperature for alloying treatment is specified in the range of 470 to 650° C. When the alloying treatment is performed by maintaining the temperature in the range of 470 to 650° C. by heating, time for the maintenance is desirably in a range of 10 to 120 seconds. Further, annealing time in the case of heating to the temperature in the range of 470 to 650° C. to perform annealing to the solidification temperature (about 420° C.) of Zn is preferably 15 to 200 seconds.

[Intra-Plated Layer Diffusion Treatment Step]

The hot dip galvanized layer subjected to the alloying treatment in the preceding step is subjected to diffusion treatment for diffusing Fe into the plated layer to reduce the concentration gradient of the amount of Fe in the plated layer, i.e., treatment for achieving the absolute value of a difference ΔFe between the amount of Fe in the vicinity of the interface with the base steel sheet (the amount of Fe in the vicinity of an internal side) and the amount of Fe in the vicinity of the external surface of the plated layer (the amount of Fe in the vicinity of the external side) in the range of 0.0 to 3.0%. The intra-plated-layer diffusion treatment includes allowing the hot dip galvanized steel sheet subjected to the alloying treatment to stay at a temperature in a range of 250 to 450° C. and subjecting the hot dip galvanized steel sheet to one or more times of bending-unbending working in the temperature range. By bending-unbending working one or more times at the temperature in the range of 250 to 450° C. in such a manner, Fe can be easily diffused in the plated layer while suppressing diffusion of Fe from the base steel sheet into the plated layer, to thereby reduce the concentration gradient of Fe in the plated layer. The reason why Fe in the plated layer can be easily diffused while suppressing the diffusion of Fe from the base steel sheet in the bending-unbending working at the temperature in the above range can be considered as follows: a defect such as an atomic vacancy and/or a dislocation is introduced mainly into the plated layer by the bending-unbending working, to activate the diffusion of Fe atoms in the plated layer, while the diffusion of Fe atoms in the base steel sheet does not occur due to sufficiently low temperature, and therefore, the diffusion of Fe from the base steel sheet into the plated layer can only restrictively occur.

When the temperature in the intra-plated-layer diffusion treatment is less than 250° C., the diffusion of Fe in the plated layer does not sufficiently proceed; while, at the temperature of more than 450° C., melting of the plated layer may be started to rapidly diffuse Fe from the base steel sheet into the plated layer and to conversely increase the Fe concentration gradient, and hot dipping metal simultaneously adheres to a roll for bending-unbending working due to the melting of the plated layer, to make it practically impossible to perform the bending-unbending working. Thus, the temperature in the intra-plated-layer diffusion treatment is in the range of 250 to 450° C.

One bending working is preferably performed so that a maximum tensile strain amount on the surface of the steel sheet ranges from 0.0007 to 0.0910. A maximum tensile strain amount of less than 0.0007 results in an insufficient alloying acceleration effect. The maximum tensile strain amount is preferably 0.0010 or more for sufficiently accelerating alloying. On the other hand, a maximum tensile strain amount of more than 0.0910 results in impossible keeping of the shape of the steel sheet to deteriorate flatness. The maximum tensile strain amount is preferably 0.0500 or less, further preferably 0.0250 or less, for well keeping the shape of the steel sheet.

›DESCRIPTION OF EMBODIMENTS · 6 of 7

The sheet thickness of the steel sheet of the present invention is 0.6 mm to 10.0 mm. This is because the thickness of less than 0.6 mm results in impossible sufficient keeping of the flat shape of the sheet while the thickness of more than 10.0 mm results in difficult temperature control to make it impossible to obtain predetermined characteristics.

A roll diameter can be selected depending on the steel sheet so that a strain amount in bending working has an appropriate value and preferably ranges from 50 mm to 800 mm in consideration of a maintenance cost. The maximum tensile strain amount introduced into the surface of the steel sheet is a value obtained by dividing the thickness t of the sheet by the sum (D+t) of the roll diameter D and the thickness t of the sheet.

Such a galvannealed steel sheet of which the alloying treatment has been finished can be subjected as a product sheet without processing the sheet to coating or press working for an automotive outside sheet or the like and may be further subjected to phosphate coating treatment as described below.

[Phosphate Coating Formation Step]

The phosphate coating formation step is a step for forming a coating including a P oxide and/or a complex oxide containing P on the surface of the galvannealed layer subjected to the intra-plated-layer diffusion treatment. In other words, in some cases, an oxide layer containing P (phosphate coating) has been conventionally formed by treating the plated surface of the steel sheet with a treatment liquid including phosphoric acid or a P-containing oxide in order to enhance the press moldability and deep drawability of the galvannealed steel sheet, to thereby impart the die of the steel sheet with lubricity and adhesion prevention properties; and the galvannealed steel sheet of the present invention may also be subjected to treatment for forming such a coating, and the effects of the present invention are not deteriorated even in the case. The specific conditions of the phosphate coating treatment step are not particularly limited, but the step may be performed under the same conditions as conventional ones.

A desirable embodiment of the method for producing a high-strength steel sheet which becomes the base material for the galvannealed steel sheet of the present invention will be explained below. As mentioned above, hot dip galvanizing on the surface of the steel sheet, alloying treatment, and, in addition, intra-plated-layer diffusion treatment can be incorporated into a step for producing a base steel sheet, particularly into a cooling process in an annealing step after cold rolling, and the plating-related steps in the case will also be explained together. In addition, various conditions described in the explanation of the method for producing the base steel sheet below are described strictly as desirable conditions, and the method for producing the base steel sheet is not limited to the conditions.

For producing the high-strength steel sheet as the base steel sheet, first, a slab having the above-mentioned chemical components (composition) is cast and the slab is hot-rolled.

As the slab subjected to the hot rolling, a continuously cast slab or a slab produced by a thin slab caster or the like can be used. The method for producing the high-strength steel sheet of the present invention is adapted to a process such as continuous casting-direct rolling (CC-DR) in which hot rolling is performed immediately after casting.

In the hot rolling step, slab heating temperature is 1050° C. or more. When the slab heating temperature is excessively low, finishing rolling temperature is less than the Ar 3 transformation temperature to result in dual-phase rolling of ferrite and austenite, the structure of the hot-rolled sheet becomes a heterogeneous duplex grain structure, the heterogeneous structure does not disappear even through cold rolling and annealing steps, and ductility and bendability are poor. Since there is a concern that reduction in finishing rolling temperature results in excessive increase of a rolling load to preclude rolling or to result in the defect of the shape of the rolled steel sheet, the slab heating temperature is preferably 1050° C. or more. The effects of the present invention are exerted without particularly specifying the upper limit of the slab heating temperature; however, since the excessively high heating temperature is economically unfavorable, the upper limit of the slab heating temperature is desirably 1350° C. or less.

The above Ar 3 transformation temperature is calculated by the following expression:

Ar 3 =901−325×C+33×Si−92×(Mn+Ni/2+Cr/2+Cu/2+Mo/2)+52×Al

In the above expression, each of C, Si, Mn, Ni, Cr, Cu, Mo, and Al represents the content [mass %] of each element.

The lower and upper limits of the finishing rolling temperature of the hot rolling are the higher one of 800° C. and the Ar 3 temperature and 1000° C., respectively. There is a concern that a finishing rolling temperature of less than 800° C. results in increase of a rolling load in finishing rolling to preclude hot rolling or to result in the defect of the shape of the hot-rolled sheet steel obtained after hot rolling. When finishing rolling temperature is less than the Ar 3 temperature, hot rolling may become dual-phase rolling of ferrite and the austenite and the structure of the hot-rolled steel sheet may become a heterogeneous duplex grain structure.

On the other hand, the effects of the present invention are exerted without particularly specifying the upper limit of the finishing rolling temperature; however, when the finishing rolling temperature is excessively high temperature, excessively high slab heating temperature is preferred for securing the temperature. Thus, the upper limit temperature of the finishing rolling temperature is desirably 1000° C. or less.

The finishing-rolled steel sheet (hot-rolled steel sheet) is usually immediately wound up in coil form. Since the winding up at a temperature of more than 800° C. results in the excessively increased thickness of an oxide formed on the surface of the steel sheet to deteriorate pickling properties, the winding temperature is 750° C. or less. The winding temperature is preferably 720° C. or less, further preferably 700° C. or less, for enhancing pickling properties. On the other hand, since the winding temperature of less than 500° C. results in the excessively increased strength of the hot-rolled steel sheet to preclude cold-rolling, the winding temperature is 500° C. or more. The winding temperature is preferably 550° C. or more, more preferably 600° C. or more, for reducing a cold-rolling load.

›DESCRIPTION OF EMBODIMENTS · 7 of 7

The hot-rolled steel sheet produced in such a manner is pickled. Pickling makes it possible to remove an oxide on the surface of the steel sheet and is therefore important for the hot dipping properties of the steel sheet as the base material for the galvannealed steel sheet. Further, the pickling may be performed once or several times.

Although the pickled steel sheet may be subjected to an annealing step without being processed, the steel sheet having high sheet thickness accuracy and an excellent shape is obtained by being subjected to cold rolling at a rolling reduction of 35 to 75%. Since the rolling reduction of less than 35% makes it difficult to keep the flat shape to deteriorate the ductility of a final product, the rolling reduction is 35% or more. On the other hand, cold rolling at a rolling reduction of more than 75% results in an excessively large cold-rolling load to preclude cold rolling. Thus, the upper limit of the rolling reduction is 75% or less.

In addition, the effects of the present invention are exerted without particularly limiting the number of times of roll passing and a rolling reduction at each passing.

Then, the obtained cold-rolled steel sheet is subjected to annealing treatment. Hot dip galvanizing treatment, alloying treatment, and, in addition, intra-plated-layer diffusion treatment of the surface of the steel sheet are desirably incorporated into a cooling process in the annealing step. Thus, the annealing treatment of the base steel sheet, into which the plating-related steps are incorporated, will be explained.

It is desirable to heat the steel sheet so that maximum heating temperature is in a range of 740 to 870° C. and to then cool the steel sheet so that an average cooling rate is 1.0 to 10.0° C./sec until 680° C. and an average cooling rate is 5.0 to 200.0° C./sec in a range of 500° C. to 680° C., in the annealing treatment. The maximum heating temperature of more than 870° C. results in significantly deteriorated plating properties. Preferably, the maximum heating temperature is 850° C. or less. Further, the maximum heating temperature of less than 740° C. causes a large amount of molten coarse iron-based carbide to remain to deteriorate bendability. Preferably, the maximum heating temperature is 760° C. or more. When a cooling rate condition after heating to the maximum heating temperature deviates from the above range, it may be impossible to obtain the steel sheet that satisfies the preferred microstructure conditions of such a base steel sheet as mentioned above.

After cooling so that the average cooling rate in the range of 500° C. to 680° C. is 5.0 to 200.0° C./sec as mentioned above, cooling is temporally performed to 350 to 450° C. and reheating is then performed or the steel sheet is dipped without being processed in a hot dip galvanizing tank to perform hot dip galvanizing treatment. The hot dipping treatment may be performed under the conditions described in the above-mentioned section [Hot Dip Galvanizing Step].

After the hot dip galvanizing treatment, cooling is performed to a temperature that is lower than the solidification temperature of Zn to solidify Zn adhering to the surface of the steel sheet, followed by performing alloying treatment of the hot dip galvanized layer. In other words, reheating is performed to 470 to 650° C., and annealing is performed to 420° C. for 15 to 200 seconds to promote alloying of the plated layer. Alternatively, alloying of the plated layer may also be promoted by performing reheating to a temperature in a range of 470 to 650° C. and maintaining a temperature in the range for 10 to 120 seconds. Conditions on the alloying treatment are the same as those described in the above-mentioned section [Alloying Treatment Step].

Subsequently, diffusion treatment for flattening the concentration gradient of Fe in the plated layer is performed. In other words, staying is performed for 60 to 1000 seconds at a temperature in a range of 250 to 420° C. in the cooling process after the alloying treatment or cooling to room temperature or around room temperature is temporally performed after the alloying treatment, reheating is then performed to a temperature in a range of 250 to 420° C., and staying is performed at a temperature in the range for 60 to 1000 seconds. In addition, repeated bending-unbending transformation is performed one or more times in the temperature range. For the repeated bending-unbending transformation in the diffusion treatment, it is desirable to use a roll having a radius in a range of 50 to 800 mm, e.g., a roll having a radius of 800 mm as mentioned above.

In the above-mentioned annealing step, surface modification and improvement of plating properties may be attempted by controlling an atmosphere in a furnace, disposing an oxidizing zone and a reducing zone, and causing an oxidation-reduction reaction of Fe and alloy elements in the surface layer of the steel sheet. Specifically, plating treatment can be performed while making Si inhibiting plating properties remain in the steel by forming an external oxidizing zone mainly including Fe in the oxidizing zone at a combustion air ratio of 0.9 or more and 1.2 or less, further making Si participate therein to fix Si in the steel, and then performing reduction in the reducing zone in an atmosphere in which the logarithm log (PH2O/PH2) of a water partial pressure and a hydrogen partial pressure is −3.0 or more and 0.0 or less, to reduce only an iron oxide in the surface layer.

After the annealing treatment also serving as each step for plating treatment, cooling may be performed to room temperature, followed by performing cold-rolling again at 0.05 to 3.00% for correcting a shape.

Furthermore, a coating including a P oxide and/or a complex oxide containing P can be formed by such phosphate coating formation treatment as mentioned above.

The present invention is specifically explained below with reference to examples. It will be appreciated that the examples described below are intended to describe the specific effects by the present invention and conditions described in the examples do not limit the technical scope of the present invention.

›EXAMPLES · 1 of 2

Slabs having the chemical components (compositions) of A to BD listed in Table 1 and Table 2 (note: the left-side end of Table 2 follows the right-side end of Table 1 in Table 1 and Table 2 indicating each chemical component) were cast and subjected to hot rolling, cooling, winding, and pickling under conditions listed in Table 3 to Table 5 immediately after the casting. Then, Experiment Examples 3, 9, 27, 32, 35, and 44 were not processed but the other Experiment Examples were cold-rolled at rolling reductions listed in Table 3 to Table 5, followed by annealing the examples under conditions listed in Table 6 to Table 8 to make steel sheets in Experiment Examples 1 to 83 and 101 to 116.

Sheet thicknesses after the cold-rolling are 1.0 mm in Experiment Examples 1 to 29 and 81 to 83, 2.4 mm in Experiment Examples 30 to 48, 0.8 mm in Experiment Examples 49 to 66, and 1.6 mm in Experiment Examples 67 to 80. Sheet thicknesses in Experiment Examples 101 to 116 are listed in Table 8.

Heating was performed to maximum heating temperatures listed in Table 6 to Table 8 in the annealing step after the cold-rolling, and, in the subsequent cooling process, cooling was performed at “cooling rates 1” in Table 6 to Table 8 from the maximum heating temperatures to 680° C., cooling was performed at “cooling rates 2” from 680° C. to 500° C., and cooling was further performed to “cooling stop temperatures”. When the cooling stop temperature was less than 430° C., reheating was performed to 430° C. or more. Furthermore, dipping was performed in a galvanizing bath to perform hot dip galvanizing treatment, heating was then performed to alloying temperatures listed in Table 6 to Table 8 as an alloying treatment step, and annealing was performed to 420° C. for treatment times listed in Table 6 to Table 8.

Then, staying was performed at average temperatures listed in Table 6 to Table 8 in a range of 250 to 420° C. for times listed in Table 6 to Table 8 as an intra-plated-layer diffusion treatment step, during which bending-unbending working with rolls having radii listed in Table 6 to Table 8 was performed at strain amounts and the number of times of working listed in Table 6 to Table 8, followed by performing cooling to room temperature.

After the cooling to the room temperature, cold-rolling at 0.15% was performed on conditions 7 to 24, cold-rolling at 0.60% was performed on conditions 25 to 44, and cold-rolling at 0.25% was performed on conditions 45 to 83.

In addition, the condition 26 or 31 is an example in which a coating including a P-based complex oxide was applied to the surface of a plated layer and provides good characteristics.

The analysis results of the microstructures of the steel sheets in Experiment Examples 1 to 83 and 101 to 116 are listed in Table 9 to Table 11. In microstructure fractions, the amount of retained austenite (retained γ) was measured by X-ray diffraction on a plane at a ¼ thickness parallel to a sheet surface. The others, which were the results of measuring the fractions of microstructures in the range of a ⅛ thickness to a ⅜ thickness, were measured by cutting a sheet thickness cross section parallel to a rolling direction, nital-etching the cross section polished to be a mirror surface, and observing the cross section using a field emission scanning electron microscope (FE-SEM).

The evaluation results of the plated layers and characteristics of the steel sheets in Experiment Examples 1 to 83 and 101 to 116 are listed in Table 12 to Table 14. For Fe % of the plated layer, Fe % was measured in the range of (⅛×plated layer thickness) to (⅞×plated layer thickness) starting from a ferrite/plated layer interface using EDX, to determine the average amount of Fe, and the absolute value of a difference ΔFe between the amount of Fe at a position of (⅛×plated layer thickness) and the amount of Fe at a position of (⅞×plated layer thickness), i.e., the value of |ΔFe %| was determined. In addition, a relationship of the value of the average amount of Fe, the value of |ΔFe %|, and the appearance of the plated layer in each experiment example is indicated in FIG. 1 .

Tensile test pieces according to JIS Z 2201 were collected from the steel sheets in Experiment Examples 1 to 83 and 101 to 116 and were subjected to a tensile test according to JIS Z 2241 to measure the yield strengths, tensile strengths, and total elongations thereof.

Further, a 90-degree V-bending test was conducted. Test pieces of 35 mm×100 mm were cut from the steel sheets in Experiment Examples 1 to 83 and 101 to 116, the shear cutting planes thereof were mechanically ground to make a bend radius twice a sheet thickness, and a test piece in which broking and/or necking did not occur at all was evaluated as accepted (O) while a test piece in which any thereof was observed was evaluated as rejected (x).

In addition, for the tensile strength TS, the case of TS≧900 MPa can be evaluated as accepted, and for the ductility, the case of TS×EL≧15000 MPa·% can be evaluated as accepted.

Furthermore, as a test for evaluating the appearance of a plated layer, unbending of a test piece was performed, an adhesion tape (cellophane tape) was stuck to the test piece and was removed, and the degree of peeling of plating adhering to the adhesion tape was visually observed. A test piece in which a plated layer was not peeled was evaluated as accepted (O), while a test piece in which plating was considerably peeled was evaluated as rejected (x).

In Experiment Examples 1 to 83 and 101 to 116, Experiment Examples 1 to 3, 5 to 9, 11 to 14, 19, 20, 23, 25 to 64, 67, 68, 73 to 80, 101 to 102, 104 to 105, 107 to 108, 110 to 111, and 113 to 116 are present invention examples. All the invention examples were confirmed not only to be excellent in mechanical performance but also to have good workability, particularly good bendability and to have the good peeling resistance of a plated layer.

On the other hand, in each experiment example corresponding to a comparative example, poor performance was exhibited as described below.

›EXAMPLES · 2 of 2

In other words, Experiment Example 16 is a comparative example in which the completion temperature of hot rolling was low and bendability was poor because a microstructure elongated in one direction and became heterogeneous.

Experiment Example 15 is a comparative example in which winding temperature was high after hot rolling, a pickling property was deteriorated, and the peeling resistance of a plated layer thus became poor.

Experiment Examples 4 and 69 are comparative examples in which annealing after cold-rolling was performed under the condition of high maximum heating temperature and the peeling resistance of each plated layer was poor.

Experiment Example 5 is a comparative example in which annealing after cold-rolling was performed under the condition of low maximum heating temperature, a coarse iron-based carbide was present, and the bendability of the steel sheet was poor since a large amount of the coarse iron-based carbide which became a fracture origin was contained. However, a plated layer was not peeled to provide a good appearance.

Experiment Example 11 is a comparative example in which a cooling rate 1 was low in a cooling process in annealing, a coarse iron-based carbide was generated, and the bendability of the steel sheet was poor. However, a plated layer was not peeled to provide a good appearance.

Experiment Example 12 is a comparative example in which a cooling rate 1 was high in a cooling process in annealing, a soft structure was not sufficiently generated, and the ductility and stretch flanging property of the steel sheet were poor. However, a plated layer was not peeled to provide a good appearance.

Experiment Example 6 is a comparative example in which a cooling rate 2 was low in a cooling process in annealing, a coarse iron-based carbide was generated, the stretch flanging property of the steel sheet was poor, and the bendability thereof was thus poor. However, a plated layer was not peeled to provide a good appearance.

Experiment Example 10 is a comparative example in which the temperature of alloying treatment of a hot dip galvanized layer was high, the plated layer was excessively alloyed, the amount of Fe in the plated layer was excessive, a coarse iron-based carbide was generated in the steel sheet, bendability was poor, and the peeling resistance of the plated layer was also poor.

Experiment Example 70 is a comparative example in which alloying treatment temperature was low, alloying of a plated layer did not proceed, and the peeling resistance of the plated layer was poor.

Experiment Example 17 is a comparative example in which alloying treatment time was short, alloying of a plated layer did not proceed, and the peeling resistance of the plated layer was poor.

Experiment Example 18 is a comparative example in which alloying treatment temperature was long, a plated layer became an excessive alloy, a coarse iron-based carbide was generated in the steel sheet, bendability was poor, and the peeling resistance of the plated layer was poor.

Experiment Examples 21 and 65 are comparative examples in which staying temperature was low in the intra-plated-layer diffusion treatment step, flattening of Fe % did not proceed in a plated layer, and the peeling resistance of the plated layer was poor.

Experiment Examples 22 and 72 are comparative examples in which staying time was short in the intra-plated-layer diffusion treatment step, flattening of Fe % did not proceed in a plated layer, and the peeling resistance of the plated layer was poor.

Experiment Example 23 is a comparative example in which staying time was too long in the intra-plated-layer diffusion treatment step, a coarse iron-based carbide was generated in the steel sheet, and the bendability of the steel sheet was poor. However, a plated layer was not peeled to provide a good appearance.

Experiment Examples 24, 66, and 71 are comparative examples in which the number of times of working was insufficient in the intra-plated-layer diffusion treatment step, flattening of Fe % in a plated layer did not proceed, and the peeling resistance of the plated layer was poor.

Experiment Examples 81 to 83 are examples in which chemical components deviated from the predetermined ranges and any sufficient characteristics were not obtained in all the examples.

Experiment Examples 103 and 112 are comparative examples in which the strain amount of working in the intra-plated-layer diffusion treatment step was large, the shape of the steel sheet was not flat, it was impossible to conduct a tensile test, a bending test and an unbending test, and the examples were inadequate as products.

Experiment Examples 106 and 109 are comparative examples in which the strain amount of working in the intra-plated-layer diffusion treatment step was small, flattening of Fe % in a plated layer did not proceed, and the peeling resistance of the plated layer was poor.

Accordingly, it is clear from the above experimental results that the present invention is effective for improving the adhesiveness of the galvannealed layer with the base steel sheet.

›INDUSTRIAL APPLICABILITY

The present invention can be preferably applied to components in uses for hot dip galvanizing and working such as bending working, among components needing strength, such as structural members and reinforcement members for automobiles, construction machines, and the like and can be applied particularly to components needing the excellent adhesiveness of a plated layer.

›Tables in the description — 14
TABLE 1
ExperimentCSiMnPSAlNO
Examplemass %mass %mass %mass %mass %mass %mass %mass %
A0.870.681.140.0050.00230.0360.00290.0019
B0.1461.542.130.0170.00270.0780.00520.0006
C0.1751.792.470.0040.00630.0450.00360.0016
D0.0881.191.400.0050.00320.1360.00400.0013
E0.1500.232.220.0130.00230.0660.00350.0009
F0.0910.251.870.0070.00331.3240.00500.0028
G0.1471.403.100.0110.00630.0630.00300.0019
H0.2330.461.370.0110.00180.0100.00590.0025
I0.1890.391.970.0120.00020.0230.00170.0035
J0.2241.742.790.0140.00150.0560.00260.0011
K0.1890.581.840.0180.00370.2150.00530.0029
L0.0911.082.310.0110.00410.0400.00290.0025
M0.1830.441.820.0170.00040.0240.00100.0012
N0.1702.110.800.0080.00350.0770.00300.0009
O0.1150.181.100.0030.00530.0710.00570.0010
P0.1521.002.370.0100.00140.1920.00170.0009
Q0.1281.292.770.0100.00400.0350.00370.0016
R0.2070.921.520.0140.00770.0800.00500.0018
S0.2631.202.070.0220.00310.0510.00340.0004
T0.2340.451.870.0170.00591.0050.00480.0012
U0.1402.261.000.0150.00470.0460.00250.0014
V0.1160.651.290.0060.00310.0420.00180.0023
W0.2060.891.350.0130.00240.0160.00130.0018
X0.1681.340.810.0120.00640.0620.00510.0014
Y0.2201.940.920.0200.00570.0310.00540.0016
Z0.1440.291.980.0180.00180.5240.00210.0027
AA0.0581.522.620.0070.00160.0310.00230.0007
AB0.0081.031.990.0070.00160.0300.00250.0008
AC0.0952.802.970.0090.00310.0310.00270.0010
AD0.0990.971.960.0090.00332.0330.00350.0005
BA0.2380.982.130.0100.00470.0520.00350.0006
BB0.0711.352.640.0070.00040.1160.00230.0007
BC0.1540.301.830.0130.00251.1820.00860.0011
BD0.1520.923.070.0090.00310.0150.00730.0009
TABLE 2 — Experi-
mentTiNbBCrNiCuMoVCaCeMgZrHfREMFe
Exam-massmassmassmassmassmassmassmassmassmassmassmassmassmassmass
ple%%%%%%%%%%%%%%%
A——————————————BalancePresent
Invention
Example
B——————————————BalancePresent
Invention
Example
C——————————————BalancePresent
Invention
Example
D——————————————BalancePresent
Invention
Example
E0.055—————————————BalancePresent
Invention
Example
F—0.041————0.10———————BalancePresent
Invention
Example
G——0.0022——————————BalancePresent
Invention
Example
H———1.00——————————BalancePresent
Invention
Example
I—0.015————————————BalancePresent
Invention
Example
J————————0.0029—————BalancePresent
Invention
Example
K————0.98—————————BalancePresent
Invention
Example
L—————————0.0017————BalancePresent
Invention
Example
M—————0.45————————BalancePresent
Invention
Example
N——————0.22———————BalancePresent
Invention
Example
O0.021—0.0005———0.07———————BalancePresent
Invention
Example
P——————————0.0012———BalancePresent
Invention
Example
Q———————————0.0015——BalancePresent
Invention
Example
R————————————0.0009—BalancePresent
Invention
Example
S—————————————0.0022BalancePresent
Invention
Example
T0.0090.055——————0.0017—————BalancePresent
Invention
Example
U0.0030.0080.00220.220.390.210.18——0.0019————BalancePresent
Invention
Example
V———————0.107——————BalancePresent
Invention
Example
W——————————————BalancePresent
Invention
Example
X——0.00450.470.15——0.00150.0033————BalancePresent
Invention
Example
Y0.040——0.57——0.42—0.0009————0.0010BalancePresent
Invention
Example
Z——————————————BalancePresent
Invention
Example
AA————0.600.65————————BalancePresent
Invention
Example
AB——————————————BalanceComparative
Example
AC——————————————BalanceComparative
Example
AD——————————————BalanceComparative
Example
BA——————————————BalancePresent
Invention
Example
BB——————————————BalancePresent
Invention
Example
BC——————————————BalancePresent
Invention
Example
BD——————————————BalancePresent
Invention
Example
TABLE 3 — Hot
SlabAr 3RollingCold
HeatingTransformationCompletionWindingRolling
ExperimentChemicalTemperatureTemperatureTemperatureTemperatureReduction
ExampleComponent° C.° C.° C.° C.%
1A123079295064450Present
Invention Example
2A119079295760750Present
Invention Example
3A11857929616650Present
Invention Example
4A117579291056950Comparative
Example
5A117079288865450Comparative
Example
6A125579295068350Comparative
Example
7B119071290767067Present
Invention Example
8B125571292664947Present
Invention Example
9B11907129476800Present
Invention Example
10B121571289558447Comparative
Example
11B121571292868147Comparative
Example
12B123071292062747Comparative
Example
13C124567892256654Present
Invention Example
14C119067892366071Present
Invention Example
15C121067896181554Comparative
Example
16C125567879059054Comparative
Example
17C126067894859754Comparative
Example
18C120567895465354Comparative
Example
19D127079093058067Present
Invention Example
20D122579092259344Present
Invention Example
21D124079088962944Comparative
Example
22D123079092564844Comparative
Example
23D126579093456944Comparative
Example
24D123079089356044Comparative
Example
25E119565993268350Present
Invention Example
26E118065989460450Present
Invention Example
27E12156598955890Present
Invention Example
28F124077294356838Present
Invention Example
29F119577291859854Present
Invention Example
30G123061888662660Present
Invention Example
TABLE 4 — Hot
SlabAr 3RollingCold
HeatingTransformationCompletionWindingRolling
ExperimentChemicalTemperatureTemperatureTemperatureTemperatureReduction
ExampleComponent° C.° C.° C.° C.%
31G126061891171560Present
Invention Example
32G11756188976830Present
Invention Example
33H125066995460250Present
Invention Example
34H123566989168450Present
Invention Example
35H11706699046100Present
Invention Example
36I123067289261444Present
Invention Example
37I121067291968144Present
Invention Example
38J126063295561644Present
Invention Example
39J125563291062244Present
Invention Example
40K120565695972967Present
Invention Example
41K121065694960867Present
Invention Example
42L119569792852547Present
Invention Example
43L121069796256347Present
Invention Example
44L11856979195970Present
Invention Example
45M120566991763838Present
Invention Example
46M122566990157150Present
Invention Example
47N119583691365547Present
Invention Example
48N120583689260247Present
Invention Example
49O121576993160160Present
Invention Example
50O126576995460071Present
Invention Example
51P125567789665450Present
Invention Example
52P117067789166650Present
Invention Example
53Q124564992664354Present
Invention Example
54Q127064993858754Present
Invention Example
55R118072890456654Present
Invention Example
56R122572891062460Present
Invention Example
57S121566789866160Present
Invention Example
58S123066795256060Present
Invention Example
59T126072093065760Present
Invention Example
60T123572090667760Present
Invention Example
TABLE 5 — Hot
SlabAr 3RollingCold
HeatingTransformationCompletionWindingRolling
ExperimentChemicalTemperatureTemperatureTemperatureTemperatureReduction
ExampleComponent° C.° C.° C.° C.%
61U122079489070560Present
Invention Example
62U126079494562954Present
Invention Example
63V123576894568650Present
Invention Example
64V117576894960250Present
Invention Example
65V120076890362050Comparative
Example
66V122076893767250Comparative
Example
67W117574091060050Present
Invention Example
68W125074092861750Present
Invention Example
69W117074094760950Comparative
Example
70W126074095664650Comparative
Example
71W122574089966150Comparative
Example
72W120074090359950Comparative
Example
73X117579189364843Present
Invention Example
74X117079191863343Present
Invention Example
75Y125576588856650Present
Invention Example
76Y122076593967560Present
Invention Example
77Z126070992664040Present
Invention Example
78Z119070991664560Present
Invention Example
79AA117063592668047Present
Invention Example
80AA119563594157267Present
Invention Example
81AB123075191260950Comparative
Example
82AC69182888764850Comparative
Example
83AD118591691062850Comparative
Example
101BA121566389958567Present
Invention Example
102BA123066390851367Present
Invention Example
103BA120566392057067Comparative
Example
104BB121068691156367Present
Invention Example
105BB121068689552767Present
Invention Example
106BB121568690060067Comparative
Example
107BC122075491856150Present
Invention Example
108BC120575490859350Present
Invention Example
109BC122075489556750Comparative
Example
110BD121560086860050Present
Invention Example
111BD120560090455850Present
Invention Example
112BD122560089755650Comparative
Example
113BA119066394262467Present
Invention Example
114BB121068689162467Present
Invention Example
115BC123075490559450Present
Invention Example
116BD119060092663450Present
Invention Example
TABLE 6 — Intra-Plated Layer Diffusion Treatment Step Bending-Unbending Working The
Annealing StepNumber
Cooling ProcessAlloying Treatmentof
MaximumCoolingStepStayingTimes
HeatingCoolingCoolingStopAlloyingTreatmentAverageSheetRollStrainof
ExperimentChemicalTemperatureRate 1Rate 2TemperatureTemperatureTimeTemperatureTimeThicknessDiameterAmountWorking
ExampleComponent° C.° C./sec° C./sec° C.° C.Sec° C.Secmmmm[—]Times
1A7974.91242649942327821.05500.00182Present Invention Example
2A8483.3747249937379981.05500.00182Present Invention Example
3A8361.812467502773381001.05500.00183Present Invention Example
4A9185.68461515583811111.05500.00183Comparative Example
5A7026.77470509763391351.05500.00183Comparative Example
6A7934.52467509253991001.05500.00183Comparative Example
7B7983.88455491753896781.04300.00238Present Invention Example
8B7875.87428524803041141.04300.00233Present Invention Example
9B7952.49460497384041021.04300.00233Present Invention Example
10B7885.3747367869375981.04300.00233Comparative Example
11B7960.311457510253811361.04300.00234Comparative Example
12B83419.012469515253251231.04300.00234Comparative Example
13C7742.257475530693224351.05500.00188Present Invention Example
14C7925.4673715371173621181.05500.00184Present Invention Example
15C7786.472480500634091071.05500.00184Comparative Example
16C7774.368463528713931341.05500.00184Comparative Example
17C8172.15945750623391251.05500.00184Comparative Example
18C8213.0574735302783771271.05500.00184Comparative Example
19D8442.329473510343721281.05500.00184Present Invention Example
20D8186.129474531173281291.05500.00183Present Invention Example
21D7825.23445552952161841.05500.00183Comparative Example
22D7722.93947951453343221.05500.00181Comparative Example
23D7843.5414675142936118001.05500.00188Comparative Example
24D8006.141469520413761031.05500.00180Comparative Example
25E7858.237473507753481081.05500.00183Present Invention Example
26E8155.38385567713651191.03750.00273Present Invention Example
27E8482.09462533723901421.05500.00184Present Invention Example
28F7915.67458499323281501.05500.00184Present Invention Example
29F8415.917463487283694001.03750.00276Present Invention Example
30G8491.82546353780337882.45500.00433Present Invention Example
TABLE 7 — Intra-Plated Layer Diffusion Treatment Step Bending-Unbending Working The
Annealing StepNumber
Cooling ProcessAlloying Treatmentof
MaximumCoolingStepStayingTimes
HeatingCoolingCoolingStopAlloyingTreatmentAverageSheetRollStrainof
ExperimentChemicalTemperatureRate 1Rate 2TemperatureTemperatureTimeTemperatureTimeThicknessDiameterAmountWorking
ExampleComponent° C.° C./sec° C./sec° C.° C.Sec° C.Secmmmm[—]Times
31G8377.516426491273551112.45500.00433Present Invention Example
32G8033.518460528724103912.43750.00646Present Invention Example
33H7805.43043553548388942.43750.00643Present Invention Example
34H7913.189462575444091422.45500.00434Present Invention Example
35H8075.0814804981413384052.45500.00436Present Invention Example
36I8134.875474518614072422.45500.00434Present Invention Example
37I8423.943480525493591092.43750.00643Present Invention Example
38J7944.15647647251291872.43750.00642Present Invention Example
39J8252.560420507293602922.45500.00436Present Invention Example
40K8251.938476499393531362.46200.00394Present Invention Example
41K8345.353400521403331462.45500.00434Present Invention Example
42L8555.460436539294061312.45500.00434Present Invention Example
43L7831.23946860368353912.45500.00433Present Invention Example
44L8402.737466518773731902.45500.00434Present Invention Example
45M8315.959467482924091502.46200.00394Present Invention Example
46M8076.012748049382345902.46200.00392Present Invention Example
47N8088.011468478552911302.46200.00394Present Invention Example
48N8123.411427506653301372.46200.00394Present Invention Example
49O7783.612464536633081480.86200.00134Present Invention Example
50O7855.81084584811243341400.86200.00134Present Invention Example
51P7893.87457529683252130.84300.00195Present Invention Example
52P8474.212471490313421300.84300.00193Present Invention Example
53Q7724.16462524283981250.84300.00193Present Invention Example
54Q7944.312465490372791070.84300.00193Present Invention Example
55R8314.914469565463582040.84300.00194Present Invention Example
56R8265.032479531613923930.84300.00196Present Invention Example
57S7784.63436753234385960.85500.00153Present Invention Example
58S7813.130464504834051070.85500.00153Present Invention Example
59T8296.443457573784083560.85500.00155Present Invention Example
60T8525.018467499323471380.85500.00153Present Invention Example
TABLE 8 — Intra-Plated Layer Diffusion Treatment Step Bending-Unbending Working
Annealing StepAlloying TreatmentThe
MaximumCooling ProcessStepStayingNumber of
HeatingCoolingCoolingCooling StopAlloyingTreatmentAverageSheetRollStrainTimes of
ExperimentChemicalTemperatureRate 1Rate 2TemperatureTemperatureTimeTemperatureTimeThicknessDiameterAmountWorking
ExampleComponent° C.° C./sec° C./sec° C.° C.Sec° C.Secmmmm[—]Times
61U8296.42146353967320840.85500.00152Present Invention Example
62U8113.117472529413331160.85500.00153Present Invention Example
63V7996.42441749166407840.84300.00192Present Invention Example
64V7822.216465490323221160.84300.00193Present Invention Example
65V8302.124471485712031490.84300.00193Comparative Example
66V8284.822474497333241320.84300.00191Comparative Example
67W7876.554397482453234331.64300.00376Present Invention Example
68W7782.85645853662331871.64300.00372Present Invention Example
69W9293.049472516343211411.64300.00372Comparative Example
70W8495.953458451673311161.64300.00372Comparative Example
71W7893.153464515283511151.64300.00371Comparative Example
72W8462.95647950965399371.64300.00372Comparative Example
73X8235.9847952133392951.65500.00293Present Invention Example
74X7815.78469508633721041.65500.00293Present Invention Example
75Y8296.31246856047322901.63750.00423Present Invention Example
76Y8186.38468498513251491.63750.00424Present Invention Example
77Z7964.314475577703601341.66200.00262Present Invention Example
78Z7955.220465537493571121.66200.00262Present Invention Example
79AA8616.321466516563851261.65500.00293Present Invention Example
80AA8205.324461539293581241.65500.00293Present Invention Example
81AB8134.53247151270405831.05500.00183Comparative Example
82AC8344.835459505413281391.05500.00183Comparative Example
83AD7864.236472505443271301.05500.00183Comparative Example
101BA8163.87149852716281721.44500.00314Present Invention Example
102BA8274.57441359430279643.5800.04214Present Invention Example
103BA8052.05347251822306805.0150.254Comparative Example
104BB8393.37246053413275662.71500.01774Present Invention Example
105BB8161.51844850445291911.84500.00404Present Invention Example
106BB8232.92545950827297852.0without0.00000Comparative Example
working
107BC8281.24147451816354721.02500.00405Present Invention Example
108BC8337.14536947330274831.02250.00445Present Invention Example
109BC8565.04841551136290980.825000.00033Comparative Example
110BD7973.71042756429281691.03700.00275Present Invention Example
111BD8122.72244158114269662.9800.03475Present Invention Example
112BD8113.21542952825297952.4150.145Comparative Example
113BA8192.33643455233280860.810000.0086Present Invention Example
114BB8192.43543550625277731.0450.2172Present Invention Example
115BC8182.24044554731279771.0450.2176Present Invention Example
116BD8212.64144450319278890.88000.00106Present Invention Example
TABLE 9 — Microstructure Observation Results Volume Fraction
ExperimentChemicalFBBFTMMRetained γOthers
ExampleComponent%%%%%%%
1A49181118040Present Invention Example
2A24322317130Present Invention Example
3A33191531020Present Invention Example
4A14262530041Comparative Example
5A870000013Comparative Example
6A6114109006Comparative Example
7B49102015060Present Invention Example
8B5551420051Present Invention Example
9B47030120110Present Invention Example
10B6441012136Comparative Example
11B5621612077Comparative Example
12B3212742160Comparative Example
13C6901214050Present Invention Example
14C53420120110Present Invention Example
15C59310161110Comparative Example
16C6351213070Comparative Example
17C36028201141Comparative Example
18C2373519367Comparative Example
19D31232417050Present Invention Example
20D4762221040Present Invention Example
21D6741018100Comparative Example
22D723915001Comparative Example
23D705136006Comparative Example
24D6251513140Comparative Example
25E23381029000Present Invention Example
26E14441029021Present Invention Example
27E1638733141Present Invention Example
28F74688130Present Invention Example
29F6912106030Present Invention Example
30G18163523170Present Invention Example
TABLE 10 — Microstructure Observation Results Volume Fraction
ExperimentChemicalFBBFTMMRetained γOthers
ExampleComponent%%%%%%%
31G21143918080Present Invention Example
32G31438160101Present Invention Example
33H4020632020Present Invention Example
34H28321027012Present Invention Example
35H15241246030Present Invention Example
36I10341338041Present Invention Example
37I11521517140Present Invention Example
38J32333120191Present Invention Example
39J151735190140Present Invention Example
40K16313016070Present Invention Example
41K18202332070Present Invention Example
42L21213022240Present Invention Example
43L5651719030Present Invention Example
44L22112539030Present Invention Example
45M19281631051Present Invention Example
46M16311631042Present Invention Example
47N673615081Present Invention Example
48N4852513153Present Invention Example
49O5223518110Present Invention Example
50O4830417010Present Invention Example
51P52101320050Present Invention Example
52P10114625080Present Invention Example
53Q5661613270Present Invention Example
54Q35103216070Present Invention Example
55R121738220110Present Invention Example
56R21202426090Present Invention Example
57S38415260170Present Invention Example
58S39823130170Present Invention Example
59T7101171100Present Invention Example
60T57316112101Present Invention Example
TABLE 11 — Microstructure Observation Results Volume Fraction
ExperimentChemicalFBBFTMMRetained γOthers
ExampleComponent%%%%%%%
61U51025121101Present Invention Example
62U59115140101Present Invention Example
63V42191222230Present Invention Example
64V5916913030Present Invention Example
65V16332328010Comparative Example
66V20241336151Comparative Example
67W38202315040Present Invention Example
68W5171522140Present Invention Example
69W13133038051Comparative Example
70W16242630040Comparative Example
71W45151521031Comparative Example
72W19203525010Comparative Example
73X4062521260Present Invention Example
74X714126061Present Invention Example
75Y4322721070Present Invention Example
76Y4771523062Present Invention Example
77Z5916712150Present Invention Example
78Z6810610150Present Invention Example
79AA131127380101Present Invention Example
80AA40141918081Present Invention Example
81AB95020003Comparative Example
82AC47019240100Comparative Example
83AD6941011150Comparative Example
101BA4119926041Present Invention Example
102BA34192512082Present Invention Example
103BA4928125060Comparative Example
104BB44261014060Present Invention Example
105BB7213110040Present Invention Example
106BB4027222090Comparative Example
107BC6613811020Present Invention Example
108BC24171439231Present Invention Example
109BC29213117020Comparative Example
110BD3125316430Present Invention Example
111BD46131516082Present Invention Example
112BD4592513080Comparative Example
113BA6410169010Present Invention Example
114BB5913170272Present Invention Example
115BC5128412401Present Invention Example
116BD635205340Present Invention Example
TABLE 12
Results of Analysis ofBending Test
Plated Layer ComponentsTensile TestAppearance
ExperimentChemicalAverage|ΔFe %|Coating AmountYSTSELTS × ElBendabilityEvaluation
ExampleComponentFe % %%g/m2MPaMPa%MPa · %(Steel Sheet)(Plated Layer)
1A10.80.4375489432422632∘∘Present
Invention
Example
2A9.60.43776310012020020∘∘Present
Invention
Example
3A10.90.9397349992120979∘∘Present
Invention
Example
4A7.54.4338089492321827∘xComparative
Example
5A11.41.532540698139074x∘Present
Invention
Example
6A9.40.8385429081715436x∘Present
Invention
Example
7B10.72.34177112501518750∘∘Present
Invention
Example
8B10.11.73867811481921812∘∘Present
Invention
Example
9B8.70.93773312191923161∘∘Present
Invention
Example
10B13.22.43589611501213800xxComparative
Example
11B10.10.73268310231616368x∘Present
Invention
Example
12B10.41.339120013311013310x∘Present
Invention
Example
13C10.82.54162312401619840∘∘Present
Invention
Example
14C10.20.93766011981821564∘∘Present
Invention
Example
15C7.35.14267612891721913∘xComparative
Example
16C10.30.434607124389944∘∘Comparative
Example
17C7.22.33588313451621520∘xComparative
Example
18C13.63.73495611111213332xxComparative
Example
19D9.60.5346879762120496∘∘Present
Invention
Example
20D9.90.9375739662221252∘∘Present
Invention
Example
21D10.53.53548510911415274∘∘Comparative
Example
22D9.23.23558810601515900∘xComparative
Example
23D10.91.5357969331312129x∘Present
Invention
Example
24D9.43.9334239272321321∘xComparative
Example
25E10.00.53490311111516665∘∘Present
Invention
Example
26E11.81.43594611261415764∘∘Present
Invention
Example
27E10.30.34194511031718751∘∘Present
Invention
Example
28F9.91.1404429792221538∘∘Present
Invention
Example
29F8.91.9403599512119971∘∘Present
Invention
Example
30G9.31.33588911501820700∘∘Present
Invention
Example
TABLE 13
Results of Analysis ofBending Test
Plated Layer ComponentsTensile TestAppearance
ExperimentChemicalAverage Fe %|ΔFe %|Coating AmountYSTSELTS × ElBendabilityEvaluation
ExampleComponent%%g/m2MPaMPa%MPa·%(Steel Sheet)(Plated Layer)
31G8.71.43684711492022980∘∘Present
Invention
Example
32G9.61.94086711801618880∘∘Present
Invention
Example
33H9.40.635106314551217460∘∘Present
Invention
Example
34H10.90.73496212581417612∘∘Present
Invention
Example
35H9.21.842112512651518975∘∘Present
Invention
Example
36I10.81.035110612751316575∘∘Present
Invention
Example
37I10.50.43498412231518345∘∘Present
Invention
Example
38J10.21.74097514651420510∘∘Present
Invention
Example
39J9.60.94097912521923788∘∘Present
Invention
Example
40K9.11.33794912571620112∘∘Present
Invention
Example
41K10.70.93299311721517580∘∘Present
Invention
Example
42L10.60.5357589962019920∘∘Present
Invention
Example
43L10.71.33554210392323897∘∘Present
nvention
Example
44L11.01.6398369962019920∘∘Present
Invention
Example
45M10.31.03897212041619264∘∘Present
Invention
Example
46M9.80.83796911601719720∘∘Present
Invention
Example
47N8.11.63860212671721539∘∘Present
Invention
Example
48N9.71.53675012021821636∘∘Present
Invention
Example
49O11.31.33965510731617168∘∘Present
Invention
Example
50O10.90.83366511351415890∘∘Present
Invention
Example
51P9.01.83869211131617808∘∘Present
Invention
Example
52P10.41.133100011831720111∘∘Present
Invention
Example
53Q10.70.34255310931920767∘∘Present
Invention
Example
54Q9.41.63383011871720179∘∘Present
Invention
Example
55R9.91.741104213301621280∘∘Present
Invention
Example
56R9.31.041110113521418928∘∘Present
Invention
Example
57S10.40.741111415271624432∘∘Present
Invention
Example
58S9.40.73887313221519830∘∘Present
Invention
Example
59T10.21.63757213621419068∘∘Present
Invention
Example
TABLE 14
Results of Analysis ofBending Test
Plated Layer ComponentsTensile TestAppearance
ExperimentChemicalAverage Fe %|ΔFe %|Coating AmountYSTSELTS × ElBendabilityEvaluation
ExampleComponent%%g/m2MPaMPa%MPa·%(Steel Sheet)(Plated Layer)
60T10.50.93665112781620448∘∘Present
Invention
Example
61U9.80.53466411622023240∘∘Present
Invention
Example
62U10.11.24260811642225608∘∘Present
Invention
Example
63V11.11.04167710331818594∘∘Present
Invention
Example
64V10.10.93656611461618336∘∘Present
Invention
Example
65V9.73.63694411691416366∘xComparative
Example
66V10.53.43487310111717187∘xComparative
Example
67W10.02.54287413131519695∘∘Present
Invention
Example
68W10.11.13582514001521000∘∘Present
Invention
Example
69W6.85.241110012201821960∘xComparative
Example
70W7.51.733104112431619888∘xComparative
Example
71W9.24.73883012441518660∘xComparative
Example
72W10.53.532113314291115719∘xComparative
Example
73X10.20.33980512641721488∘∘Present
Invention
Example
74X9.61.13746312161720672∘∘Present
Invention
Example
75Y9.31.13686213921520880∘∘Present
Invention
Example
76Y10.31.03685413611723137∘∘Present
Invention
Example
77Z11.81.03357811221617952∘∘Present
Invention
Example
78Z10.71.53355211771416478∘∘Present
Invention
Example
79AA8.90.5367809022421648∘∘Present
Invention
Example
80AA10.40.4396369372119677∘∘Present
Invention
Example
81AB11.10.2393394653918135∘∘Comparative
Example
82AC3.84.54163510012525025∘xComparative
Example
83AD4.74.03745410762021520∘xComparative
Example
101BA11.21.12870410361919691∘∘Present
Invention
Example
102BA10.71.6456459692019378∘∘Present
Invention
Example
103BA11.61.947——————Comparative
Example
104BB9.82.76169511022022043∘∘Present
Invention
Example
105BB11.81.23453210482121999∘∘Present
Invention
Example
106BB9.83.8375759212220257∘xComparative
Example
107BC8.60.92589514271521404∘∘Present
Invention
Example
108BC10.91.03190011741517613∘∘Present
Invention
Example
109BC9.74.030104514301318594∘xComparative
Example
110BD11.81.64687612541417553∘∘Present
Invention
Example
111BD10.42.5595549082018157∘∘Present
Invention
Example
112BD11.51.444——————Comparative
Example
113BA11.42.84150310171919323∘∘Present
Invention
Example
114BB8.50.73958310782425872∘∘Present
Invention
Example
115BC11.61.3386379172018340∘∘Present
Invention
Example
116BD8.62.4426059652423160∘∘Present
Invention
Example
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12 claims

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Classifications

10 codes
IPC · International Patent Classification
Section B — Performing operations; transporting
  • B32B15/01
  • B32B15/00
Section C — Chemistry; metallurgy
  • C21D8/04
  • C22C38/04
  • C23C2/28
  • C22C38/02
  • C22C38/06
  • C22C38/00
  • C23C2/06
  • C22C18/00

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1,642 days filing → grant
Office actions
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Responses
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1 RCE
Examiner
Humera Sheikh
art unit 1784 · TC 1700
Citations: 30 back · 0 forward

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