FERRITE-BASED STAINLESS STEEL PLATE, STEEL PIPE, AND PRODUCTION METHOD THEREFOR

Abstract
A ferritic stainless steel sheet and a steel pipe as a material suitable for a heat-resistant component that is required to have especially excellent formability are provided. The ferritic stainless steel sheet contains 10 to 20 mass % of Cr and a predetermined amount of C, Si, Mn, P, S, Al and one or both of Ti and Nb, a {111}-orientation intensity being 5 or more and {411}-orientation intensity being less than 3 at a portion in the vicinity of a sheet-thickness central portion of the ferritic stainless steel sheet. Further, with similar composition and by setting {111}<110>-orientation intensity at 4.0 or more and {311}<136>-orientation intensity at less than 3.0, a relationship rm≥−1.0t+3.0 (t(mm): sheet thickness, rm: average r-value) is satisfied, thereby providing a ferritic stainless steel sheet and a steel pipe with excellent formability.
Description
TECHNICAL FIELD

The present invention relates to a ferritic stainless steel sheet and a steel pipe that are especially suitably usable for a heat-resistant component that is required to have excellent formability and for a molding article that is required to have excellent formability, and a manufacturing method thereof.


BACKGROUND ART

Ferritic stainless steel sheet is used in a variety of applications including household electronic appliances, kitchen instrument and electronic devices. For instance, studies have recently been made for the use of stainless steel sheet for exhaust pipes, fuel tanks and pipes of automobiles and motorcycles. These components require high formability for shape forming, as well as corrosion resistance and heat resistance in an environment in which the components contact with exhaust-gas or fuel. However, the ferritic stainless steel sheet is, though less expensive, inferior in formability to austenitic stainless steel sheet. Accordingly, the usage and shape of the component to which the ferritic stainless steel sheet is applicable tend to be limited. Especially, in order to meet environmental regulations and complication of component arrangement in accordance with demand for weight reduction, the shape of the components have recently come to be complicated. Further, various measures for reducing forming and welding steps during the production of the components have been studied in order to reduce the cost of the components. In one of the measures studied, a component typically provided by welding is produced in a one-piece component without welding. In the above method, for instance, in contrast to a conventional method in which a steel sheet or a steel pipe is shaped and subsequently welded with other component(s), the steel sheet or steel pipe is subjected to various processing (e.g. deep-drawing, bulge-forming, bending, and tube expansion) for forming the one-piece component.


Some studies have been made in order to overcome the above disadvantages of the ferritic stainless steel sheet or steel pipe in view of formability and processability. For instance, Patent Literature 1 discloses a method of defining a linear pressure during a finish rolling process in a hot rolling process and a method for defining hot-rolled sheet annealing conditions in order to produce components which are difficult to be processed. Patent Literature 2 discloses a method in which X-ray integral intensity ratio and temperature and rolling reduction during a rough rolling in a hot rolling process are defined and an intermediate annealing is applied in addition to annealing of hot-rolled sheet.


Patent Literatures 3 to 6 disclose methods in which r-value or breaking elongation is defined. In addition, Patent Literatures 7 and 8 disclose techniques for defining hot rolling conditions. Specifically, Patent Literatures 7 and 8 disclose that a rolling reduction in a final pass of rough rolling during hot rolling is set at 40% or more, or the rolling reduction in at least one pass is set at 30% or more.


Further, Patent Literature 9 discloses a technique in which texture ({111}<112>, {411}<148>) in sheet-thickness central area of ferritic stainless steel containing 0.5% or more of Mo is controlled to obtain a high r-value steel material. Patent Literature 10 discloses a technique in which intermediate annealing texture of the ferritic stainless steel containing 0.5% or more of Mo is controlled without subjecting the ferritic stainless steel to annealing of hot-rolled sheet, thereby obtaining a high r-value steel material.


Patent Literatures 11 to 12 disclose a ferritic stainless steel whose formability is enhanced by reducing carbon and adjusting the components. However, the formability obtained by the disclosures of the above Patent Literatures is short for 2D pipe expansion and thus is insufficient.


Patent Literature 13 discloses that formability is enhanced by conditioning an annealing temperature, annealing time, rolling ratio and the like during a hot rolling process. In the above arrangement, the r-value is approximately 1.6 at the maximum.


Patent Literature 14 discloses that formability is enhanced by performing annealing of hot-rolled sheet. In the above arrangement, it is supposed that the steel sheet is 0.8 mm thick. Further, the r-value is at most approximately 1.8.


Patent Literature 15 discloses a steel pipe subjected to a two-stage annealing to exhibit more than 100% of tube expansion rate. In the above arrangement, it is supposed that the r-value is approximately 1.6 and the thickness of the material is 0.8 mm.


Patent Literature 16 discloses a ferritic stainless steel in which Si and Mn contents are reduced to improve elongation and Mg is contained to reduce grain size of solidified texture to reduce roping and ridging of the product. However, Patent Literature 16 discloses both instances where the annealing of hot-rolled sheet is performed and where the annealing of hot-rolled sheet is not performed, and does not disclose any hot rolling conditions for the instance where the annealing of hot-rolled sheet is not performed.


Patent Literature 17 discloses a ferritic stainless steel sheet with less surface roughness due to working and excellent formability. In Patent Literature 17, the contents of Si and Mn are reduced in order to restrain reduction in elongation. Further, the finish hot rolling temperature and coiling temperature are lowered to reduce the surface roughness due to working and cold rolling process is performed in two stages by omitting the annealing of hot-rolled sheet to control the texture.


CITATION LIST
Patent Literature(s)


















Patent Literature 1
JP 2002-363712 A



Patent Literature 2
JP 2002-285300 A



Patent Literature 3
JP 2002-363711 A



Patent Literature 4
JP 2002-97552 A



Patent Literature 5
JP 2002-60973 A



Patent Literature 6
JP 2002-60972 A



Patent Literature 7
JP 4590719 B2



Patent Literature 8
JP 4065579 B2



Patent Literature 9
JP 4624808 B2



Patent Literature 10
JP 4397772 B2



Patent Literature 11
JP 2012-112020 A



Patent Literature 12
JP 2005-314740 A



Patent Literature 13
JP 2005-325377 A



Patent Literature 14
JP 2009-299116 A



Patent Literature 15
JP 2006-274419 A



Patent Literature 16
JP 2004-002974 A



Patent Literature 17
JP 2008-208412 A










SUMMARY OF THE INVENTION
Problem(s) to be Solved by the Invention

A first object of the invention is to solve problems of the related art and to efficiently manufacture a ferritic stainless steel sheet and steel pipe having excellent formability that are especially suitable for automobile exhaust components.


The inventors of the present application have found the following problems in the related arts.


The method for enhancing r-value disclosed in Patent Literature 2 is effective for a product having approximately 0.8 mm thickness and capable of providing relatively large cold rolling reduction, but is not sufficient for a thick product having thickness of more than 1 mm. It is supposed that this is because, when an annealing of hot-rolled sheet is applied, the grain size is coarsened and grain size reduction effect of the texture of pre-cold-rolling cannot be exhibited. Further, efficient manufacture of a steel sheet cannot be achieved by these manufacturing methods.


The methods disclosed in Patent Literatures 3 to 6 only increases the r-value and may cause cracks during processing. Specifically, the cracks are likely to occur due to surface irregularities called ridging generated during the processing. Herein, an instance with low level of ridging will be sometimes referred to as “having good ridging characteristics.”


The technique for defining the hot rolling conditions disclosed in Patent Literatures 7 and 8 cannot sufficiently restrain surface flaws and ridging.


It has been found that the technique for setting the rough rolling reduction and finish rolling reduction during hot rolling at 0.8 to 1.0 disclosed in Patent Literature 9 deteriorates the ridging characteristics due to growth of {411}<148>-orientated grains and, especially, satisfactory formability after the product is formed into a steel pipe cannot be obtained.


In the technique for controlling the texture during intermediate annealing by omitting the annealing of hot-rolled sheet disclosed in Patent Literature 10, since the intermediate annealing is applied at a relatively low temperature, the hot rolling texture is not sufficiently modified and ridging may occur on the product sheet. Further, it is supposed that a thin sheet with less than 1 mm thickness is processed by the method and, since a high cold rolling reduction cannot be ensured for a steel sheet with relatively large thickness of more than 1 mm, the solution disclosed in Patent Literature 10 is insufficient.


A second object of the invention is to solve disadvantages of the related art and to provide a ferritic stainless steel sheet and steel pipe having excellent formability. An efficient manufacture is also a problem. When the disclosures of the related arts are applied, a steel sheet and a steel pipe having formability sufficient to provide a steel pipe made of a relatively thick steel sheet having more than 1 mm thickness and capable of enduring 2D pipe expansion processing (a processing expanding an end diameter D of the pipe to 2D (i.e. double the diameter)) cannot be provided.


Means for Solving the Problem(s)

In order to solve achieve the above first object, the inventors have performed detailed study on the formability of a ferritic stainless steel sheet and a ferritic stainless steel pipe made from the ferritic stainless steel sheet in view of the steel composition, textures during the production process of the steel sheet and crystal orientation. As a result, it is found that, when the ferritic stainless steel sheet is subjected to extremely severe forming process applied for forming a one-piece exhaust component with a complicated shape, it is possible to significantly improve the freedom of formation by controlling a difference in the crystal orientations in a sheet-thickness center layer of the ferritic stainless steel sheet to apply an excellent r-value and ridging characteristics.


A summary of the invention capable of achieving the above first object is as follows.


(1) A ferritic stainless steel sheet with excellent formability, including: 0.001 to 0.03 mass % of C; 0.01 to 0.9 mass % of Si; 0.01 to 1.0 mass % of Mn; 0.01 to 0.05 mass % of P; 0.0003 to 0.01 mass % of S; 10 to 20 mass % of Cr, 0.001 to 0.03 mass % of N; 0.05 to 1.0 mass % of one or both of Ti and Nb; and a residual amount of Fe and inevitable impurities, in which {111}-orientation intensity of a portion in a vicinity of a sheet-thickness central portion is 5 or more and {411}-orientation intensity of the portion in the vicinity of the sheet-thickness central portion is less than 3.


(2) The ferritic stainless steel sheet with excellent formability according to the above aspect of the invention, in which a Cr content in the ferritic stainless steel sheet is 10.5 mass % or more and less than 14 mass %.


(3) The ferritic stainless steel sheet with excellent formability according to the above aspect of the invention, further including one or more of elements selected from the group consisting of: 0.0002 to 0.0030 mass % of B; 0.005 to 0.3 mass % of Al, 0.1 to 1.0 mass % of Ni, 2.0 mass % or less of Mo, 0.1 to 3.0 mass % of Cu, 0.05 to 1.0 mass % of V, 0.0002 to 0.0030 mass % of Ca, 0.0002 to 0.0030 mass % of Mg, 0.01 to 0.3 mass % of Zr, 0.01 to 3.0 mass % of W, 0.01 to 0.3 mass % of Co, 0.003 to 0.50 mass % of Sn, 0.005 to 0.50 mass % of Sb, 0.001 to 0.20 mass % of REM, 0.0002 to 0.3 mass % of Ga, 0.001 to 1.0 mass % of Ta, and 0.001 to 1.0 mass % of Hf.


(4) The ferritic stainless steel sheet with excellent formability according to the above aspect of the invention, in which a Mo content in the ferritic stainless steel sheet is less than 0.5 mass %.


(5) The ferritic stainless steel sheet with excellent formability according to the above aspect of the invention, in which a grain size number is 5.5 or more.


(6) A manufacturing method of a ferritic stainless steel sheet with excellent formability, the method including: hot-rolling a stainless steel slab of a composition according to the above aspect of the invention at a slab heating temperature in a range from 1100 to 1200 degrees C., the hot-rolling being a continuous rolling including rough rolling steps performed for (n) pass numbers and a finish rolling, at least (n−2) numbers of the rough rolling steps being performed under a 30% or more of rolling reduction and at a rough rolling end temperature of 1000 degrees C. or more, finishing temperature of the finish rolling being 900 degrees C. or less; winding the stainless steel slab at a temperature of 700 degrees C. or less; and without performing a annealing of hot-rolled sheet, subjecting the stainless steel slab to: intermediate cold rolling in which the stainless steel slab is cold-rolled at least once using a roller with a diameter of 400 mm or more and at a rolling reduction of 40% or more; intermediate annealing in which the stainless steel slab is heated at a temperature in a range from 820 to 880 degrees C.; finish cold rolling; and finish annealing in which the stainless steel slab is heated at a temperature in a range from 880 to 950 degrees C.


(7) The manufacturing method of ferritic stainless steel sheet with excellent formability according to the above aspect of the invention, in which, in the intermediate annealing, a grain size number is made to be 6 or more and a {111}-orientation intensity at a portion in the vicinity of the sheet-thickness center layer is made to be 3 or more.


(8) The manufacturing method of ferritic stainless steel sheet with excellent formability according to the above aspect of the invention, in which, in the final annealing, a grain size number is made to be 5.5 or more.


(9) A ferritic stainless steel pipe with excellent formability, in which the ferritic stainless steel pipe is made from a material in a form of the stainless steel sheet according to the above aspect of the invention.


(10) A ferritic stainless steel sheet for an automobile exhaust component, in which the ferritic stainless steel sheet for an automobile exhaust component is made from a material in a form of the stainless steel sheet according to the above aspect of the invention.


As is clear from the above description, a ferritic stainless steel sheet with excellent formability can be efficiently provided without introducing new equipment according to the above aspect of the invention.


According to the above aspect of the invention, it is possible to provide a ferritic stainless steel sheet with excellent r-value and ridging characteristics. With the use of the material embodying the above aspect of the invention, especially for components of automobiles and motorcycles, the freedom of formation improves and integral molding without requiring welding between components is possible, thereby enabling efficient production of the components. In other words, the invention is industrially extremely useful.


A summary of the invention capable of achieving the above second object is as follows.


(11) A ferritic stainless steel sheet with excellent formability, including: 0.03 mass % or less of C; 0.03 mass % or less of N; 1.0 mass % or less of Si; 3.0 mass % or less of Mn; 0.04 mass % or less of P; 0.0003 to 0.0100 mass % of S; 10 to 30 mass % of Cr, 0.300 mass % or less of Al; one or both of 0.05 to 0.30 mass % of Ti and 0.01 to 0.50 mass % of Nb, a sum of Ti and Nb being in a range from smaller one of 8(C+N) and 0.05 to 0.75 mass % and a residual amount of Fe and inevitable impurities, in which {111}<110>-orientation intensity is 4.0 or more and {311}<136>-orientation intensity is less than 3.0.


(12) The ferritic stainless steel sheet with excellent formability according to the above aspect of the invention, further including one or more of elements selected from the group consisting of: 0.0002 to 0.0030 mass % of B, 0.1 to 1.0 mass % of Ni, 0.1 to 2.0 mass % of Mo, 0.1 to 3.0 mass % of Cu, 0.05 to 1.00 mass % of V, 0.0002 to 0.0030 mass % of Ca, 0.0002 to 0.0030 mass % of Mg, 0.005 to 0.500 mass % of Sn, 0.01 to 0.30 mass % of Zr, 0.01 to 3.0 mass % of W, 0.01 to 0.30 mass % of Co, 0.005 to 0.500 mass % of Sb, 0.001 to 0.200 mass % of REM, 0.0002 to 0.3 mass % of Ga, 0.001 to 1.0 mass % of Ta, and 0.001 to 1.0 mass % of Hf.


(13) The ferritic stainless steel sheet with excellent formability according to the above aspect of the invention, in which a grain size number is 6 or more.


(14) The ferritic stainless steel sheet with excellent formability according to the above aspect of the invention, in which, when a sheet thickness is represented by t (mm) and an average r-value is represented by rm, rm satisfies a relationship of rm≥−1.0t+3.0.


(15) The ferritic stainless steel sheet with excellent formability according to the above aspect of the invention, in which the ferritic stainless steel pipe is suitable for use in an automobile component or a motorcycle component.


(16) The ferritic stainless steel sheet with excellent formability according to the above aspect of the invention, in which the ferritic stainless steel pipe is suitable for use in an automobile exhaust pipe, fuel tank or a fuel pipe.


(17) A manufacturing method of a ferritic stainless steel sheet with excellent formability, the method including: hot-rolling a stainless steel slab of a composition according to the above aspect of the invention, the hot-rolling including rough rolling and finish rolling, the rough rolling being performed at a slab heating temperature in a range from 1100 to 1200 degrees C., the finish rolling being performed at a start temperature of 900 degrees C. or more and an end temperature of 800 degrees C. or more so that a difference between the start temperature and the end temperature is 200 degrees C. or less; winding the stainless steel slab at a temperature of 600 degrees C. or more; and subsequently subjecting the stainless steel slab to intermediate cold rolling, intermediate annealing, finish cold rolling, and finish annealing without applying annealing of hot-rolled sheet, in which the cold rolling is at least once performed at 40% or more of rolling reduction using a roller having a diameter of 400 mm or more, the stainless steel slab is heated to a temperature in a range from 800 to 880 degrees C. in the intermediate annealing, the stainless steel slab is cold-rolled in the finish cold rolling at a rolling reduction of 60% or more, and in the final annealing, the stainless steel slab is heated to a temperature in a range from 850 to 950 degrees C.


(18) The manufacturing method of ferritic stainless steel sheet with excellent formability according to the above aspect of the invention, in which a texture immediately before completion of recrystallization or a minute texture of a grain size number of 6 or more is obtained in the intermediate annealing.


(19) A ferritic stainless steel pipe with excellent formability, in which the ferritic stainless steel pipe is made from a material in a form of the stainless steel sheet according to the above aspect of the invention.


According to the above aspect of the invention, a ferritic stainless steel sheet with excellent formability can be efficiently provided without introducing new equipment. The ferritic stainless steel sheet of the above aspect of the invention can endure 2D pipe expansion even when the ferritic stainless steel sheet having relatively large thickness (e.g. more than 1 mm) is made into a steel pipe.


According to the above aspect of the invention, it is possible to provide a ferritic stainless steel sheet with excellent r-value. With the use of the material embodying the above aspect of the invention, especially for components of automobiles and motorcycles (e.g. an exhaust pipe such as muffler and exhaust manifold, a fuel tank and fuel pipe), the freedom of formation improves and integral molding without requiring welding between components is possible, thereby enabling efficient production of the components. In other words, the invention is industrially extremely useful.





BRIEF DESCRIPTION OF DRAWING(S)


FIG. 1 illustrates a relationship between an average r-value, and {111}-orientation intensity and {411}-orientation intensity of a product sheet.



FIG. 2 illustrates a relationship between a ridging height, and the {111}-orientation intensity and the {411}-orientation intensity of the product sheet.



FIG. 3 illustrates a relationship between a sheet thickness and an average r-value (rm) of the product sheet.



FIG. 4 illustrates a relationship between the average r-value {rm}, and {311}<136>-orientation intensity of a product sheet.





DESCRIPTION OF EMBODIMENT(S)

A first exemplary embodiment adapted to achieve the above-described first object will be described below.


The invention is defined for the following reasons. Indexes of formability of ferritic stainless steel sheet include an r-value (index for deep drawability), a total elongation (index for bulging formability) and ridging (surface flaw caused after press forming). Among the above, the r-value and ridging are primarily dependent on crystal orientation of the steel, whereas the total elongation is primarily dependent on the composition of the steel. The formable size increases as these properties get better. The r-value increases as more {111}-crystal orientations (i.e. crystal grains having {111} crystal face parallel to a sheet face of the steel sheet in a body-centered cubic crystal structure) are present. In the exemplary embodiment, it is found that the r-value cannot be determined based solely on the {111}-crystal orientation but is also dependent on {411}-crystal orientation. On the other hand, ridging is formed on the surface of the steel sheet in a form of irregularities due to difference in plastic deformability between the colonies when colonies of crystal grains having different crystal orientations are stretched in a rolling direction. In general, it is supposed that the reduction of colonies of the {100}-crystal orientation and {111}-crystal orientation is effective for preventing ridging. Since the {111}-crystal orientation improves the r-value, it is conventionally suggested that the improvement in the r-value and the reduction in the ridging cannot be simultaneously achieved. In order to achieve both of the above, microstructural studies on the texture formation, development of the r-value, and generation mechanism of the ridging have been made in detail. Consequently, it is found in the invention that {411}-crystal orientation has more to do with the characteristics of ridging of the ferritic stainless steel sheet than the {100}-crystal orientation. Thus, it is found that a ferritic stainless steel sheet that is excellent in the r-value and ridging characteristics and has extremely excellent formability, and a steel pipe made of the ferritic stainless steel sheet can be provided. Specifically, it is defined in the invention that {111}-orientation intensity is 5 or more and {411}-orientation intensity is less than 3 in the vicinity of a sheet-thickness central portion, thereby providing a ferritic stainless steel sheet excellent in both of the r-value and ridging characteristics and providing excellent formability.


Herein, the {111}-orientation intensity and {411}-orientation intensity in the vicinity of the sheet-thickness central portion can be measured by: obtaining (200), (110) and (211) pole figures of the sheet-thickness central area using an X-ray diffractometer and Mo-Kα ray, and obtaining three-dimensional crystallographic orientation distribution function based on the dot diagrams using a spherical harmonics method. The portion in the vicinity of the sheet-thickness central portion specifically refers to an area 0.2 mm with respect to the sheet-thickness center in view of the accuracy in collecting a sample.


A cold rolled steel sheet of 1.2 mm thickness was made from a ferritic stainless steel sheet containing 0.004% of C, 0.42% of Si, 0.32% of Mn, 0.02% of P, 0.0005% of S, 10.7% of Cr, 0.16% of Ti and 0.007% of N. Results of examination on the relationship between a texture, r-value and ridging characteristics on the prepared ferritic stainless steel sheet are shown in FIGS. 1 and 2. Herein, in order to evaluate the texture, (200), (110) and (211) pole figures of the sheet-thickness central area (exposing the central area by a combination of mechanical polishing and electropolishing) are obtained using an X-ray diffractometer (manufactured by Rigaku Corporation) and Mo-Kα ray to obtain a three-dimensional crystallographic orientation distribution function based on the dot diagrams using a spherical harmonics method. In order to evaluate the r-value, JIS13B tensile test pieces were taken from a cold rolled annealing sheet and an average r-value was calculated using formulae (1) and (2) below after applying 15% distortions in a rolling direction, 45-degree direction with respect to the rolling direction and a direction perpendicular to the rolling direction.






r=ln(W0/W)/ln(t0/t)  (1)


In the formula (1), W0 represents a sheet width before applying a tensile force, W represents a sheet width after applying the tensile force, t0 represents a sheet thickness before applying the tensile force and t represents a sheet thickness after applying the tensile force.





Average r-value=(r0+2r45+r90)/4  (2)


In the formula (2), r0 represents an r-value in the rolling direction, r45 represents an r-value in 45-degree direction with respect to the rolling direction and r90 represents an r-value in a direction perpendicular to the rolling direction. The higher average r-value represents more excellent deep drawability of the steel sheet, and more excellent bendability and pipe expansivity of the steel pipe. In order to evaluate the ridging, JISS tensile test pieces were taken from a cold rolled annealing sheet and 16% distortion was applied on the test pieces in the rolling direction. Subsequently heights of irregularities caused on the surface of the steel sheet were measured using a two-dimensional roughness gauge to obtain a ridging height. The lower ridging height indicates more excellent ridging characteristics. As described above, an object of the invention is to provide a ferritic stainless steel sheet and a steel pipe having extremely excellent formability. The parameters of average r-value of 1.7 or more and ridging height of less than 10 μm suggest a material capable of being subjected to severe processing.


As shown in FIGS. 1 and 2, the average r-value becomes 1.7 or more when the {111}-orientation intensity is 5 or more. The ridging height becomes less than 10 μm when the {411}-orientation intensity is less than 3. Accordingly, the scope of an aspect of the invention is defined as {111}-orientation intensity of 5 or more and {411}-orientation intensity of less than 3. Though the r-value increases in accordance with an increase in the {111}-orientation intensity, {411}-crystal orientation lowers the r-value. Further, since the {411}-crystal orientation is low in the r-value as compared to {111}-crystal orientation, a large sheet thickness reduction occurs when the sheet is deformed, so that dents of the ridging is likely to be formed. In the above aspect of the invention, in addition to the conventionally-known increase in the r-value by increasing the {111}-crystal orientation, it is newly found that the r-value can be increased and the ridging can be reduced by reducing the {411}-crystal orientation. The plots having respective [{111}-orientation intensity, and {411}-orientation intensity] of [6.7, 2.4] and [11.9, 2.4] in FIGS. 1 and 2 are favorable in both of the average r-value and ridging height.


Next, a composition of the steel will be described below. In the description of the composition, % refers to mass %.


C deteriorates formability and corrosion resistance. Especially, the growth in the {111}-crystal orientation is greatly affected by solid solution C, where, when more than 0.03% C is added, the {111}-orientation intensity does not reach 5. Accordingly, the upper limit of the C content is defined at 0.03%. However, excessive reduction in the C content results in increase in refining cost. Accordingly, the lower limit of the C content is defined at 0.001%. In addition, the C content is preferably 0.002% or more in view of the production cost. The C content is preferably 0.01% or less in view of boundary corrosivity at a welded part.


Si is sometimes added as deoxidizing element. In addition, Si improves oxidation resistance. However, since Si is a solid solution strengthening element, the Si content is preferably as small as possible in order to ensure total elongation. Further, much amount of added Si causes change in a slip system to promote the growth in the {411}-crystal orientation and restrain the {111}-crystal orientation. Accordingly, the upper limit of the Si content is defined at 0.9%. On the other hand, in order to ensure oxidation resistance, the lower limit of the Si content is defined at 0.01%. However, in view of the fact that excessive reduction in the content of Si results in increase in refining cost and also in view of weldability, the Si content is preferably 0.2% or more. For similar reasons, Si content is preferably 0.5% or less.


Since Mn is a solid solution strengthening element similarly to Si, the Mn content in the material is preferably as small as possible. However, the upper limit of the Mn content is defined at 1.0% in view of oxidation peelability. On the other hand, excessive reduction in the Mn content results in increase in refining cost. Accordingly, the lower limit of the Mn content is defined at 0.01%. In addition, the Mn content is preferably 0.5% or less in view of the material. The Mn content is preferably 0.1% or more in view of the production cost.


Since P is a solid solution strengthening element similarly to Mn and Si, the P content in the material is preferably as small as possible. Further, much amount of added P causes change in a slip system to promote the growth in the {411}-crystal orientation. Accordingly, the upper limit of the P content is defined at 0.05%. However, excessive reduction in the P content results in increase in the material cost. Accordingly, the lower limit of the P content is defined at 0.01%. In addition, the P content is preferably 0.02% or less in view of the production cost and corrosion resistance.


S forms Ti4C2S2 in Ti-containing steel at a high temperature to contribute to the growth in the texture effective for improving the r-value. The formation of Ti4C2S2 is exhibited when S is contained at an amount of 0.0003% or more. Accordingly, the lower limit of the S content is defined at 0.0003%. However, when S is added at an amount of more than 0.01%, {411}-crystal orientation grows so that the intensity in the {411}-crystal orientation exceeds 3 and corrosion resistance deteriorates. Accordingly, the upper limit of the S content is defined at 0.01%. In addition, the S content is preferably 0.0005% or more in view of the refining cost. The S content is preferably 0.0060% or less in view of boundary corrosivity in produced components.


Cr is an element that improves corrosion resistance and oxidation resistance. In view of environment in which exhaust components are provided, 10% or more of Cr is necessary in order to restrain abnormal oxidation. The Cr content is preferably 10.5% or more. On the other hand, excessive addition of Cr hardens the steel to deteriorate the formability, restrains the growth of the {111}-oriented grains and promotes the growth of the {411}-oriented grains. Further, in fear of increase in the production cost, the upper limit of the Cr content is defined at 20%. It should be noted that, in view of the production cost, sheet breakage due to deterioration in toughness during production of the steel sheet and formability, the upper limit of the Cr content is preferably less than 14%.


Similarly to C, N deteriorates formability and corrosion resistance. In addition, the growth in the {111}-crystal orientation is greatly affected by solid solution C, where, when more than 0.03% N is added, the {111}-orientation intensity does not reach 5. Accordingly, the upper limit of the N content is defined at 0.03%. However, excessive reduction in the N content results in increase in refining cost. Accordingly, the lower limit of the N content is defined at 0.001%. In addition, the N content is preferably 0.005% or more in view of the production cost. The N content is preferably 0.015% or less in view of formability and corrosion resistance.


In the exemplary embodiment, 0.05 to 1.0% of one or more of Ti and Nb is contained.


Ti is an element added to be bonded to C, N and S to improve the corrosion resistance, intercrystalline corrosion resistance and deep drawability. The function for fixing C and/or N is exhibited at Ti content of 0.05% or more. Accordingly, lower limit of the Ti content is defined at 0.05%. The Ti content is preferably 0.06% or more. Further, when more than 1.0% of Ti is added, the product is hardened due to solid solution Ti to cause the growth of the {411}-orientated grains and deterioration of toughness. Accordingly, the upper limit of the Ti content is defined at 1.0%. Further, the Ti content is preferably 0.25% or less in view of the production cost.


Nb is added as necessary because Nb is effective for improvement in formability and high-temperature strength due to the growth in the {111}-oriented grains and for inhibition of crevice corrosion and promotion of repassivation. The function due to the addition of Nb is exhibited at Nb content of 0.05% or more. Accordingly, the lower limit of the Nb content is defined at 0.05%. However, when more than 1.0% of Nb is added, the {411}-orientation intensity becomes more than 3 on account of coarse Nb (C,N) and hardening also occurs. Accordingly, the upper limit of the Nb content is defined at 1.0%. It should be noted that the Nb content is preferably 0.55% or less in view of the material cost.


The stainless steel sheet according to the exemplary embodiment may further optionally contain the following elements.


B is an element that enhances secondary formability by segregation at grain boundaries. In order to restrain vertical crack of an exhaust pipe when the exhaust pipe is subjected to a secondary processing, especially in winter, 0.0002% or more of B has to be added. The B content is preferably 0.0003% or more. However, addition of excessive addition of the B content restrains the growth of the {111}-oriented grains and reduces formability and corrosion resistance. Accordingly, the upper limit of the B content is defined at 0.0030%. In addition, the B content is preferably 0.0015% or less in view of the refining cost and decrease in ductility.


Al is added as a deoxidizing element and, in addition, is adapted to restrain oxide scales from being peeled off. Since the function of Al is exhibited at an amount of 0.005% or more, the lower limit of the Al content is defined at 0.005%. On the other hand, addition of 0.3% or more of Al results in less than 5 of the {111}-orientation intensity due to precipitation of coarse AlN and also causes reduction in elongation and deterioration in weld compatibility and surface quality. Accordingly, the upper limit of the Al content is defined at 0.3%. Further, the Al content is preferably 0.15% or less in view of the refining cost. The Al content is preferably 0.01% or more in view of pickling capability during production of the steel sheet.


Ni is added as necessary in order to restrain crevice corrosion and promote repassivation. The function due to the addition of Ni is exhibited at the Ni content of 0.1% or more. Accordingly, the lower limit of the Ni content is defined at 0.1%. The Ni content is preferably 0.2% or more. However, when the Ni content exceeds 1.0%, a change in the slip system occurs to grow the {411}-crystal orientation, so that the {411}-orientation intensity exceeds 3. Further, when the Ni content exceeds 1.0%, hardening and stress corrosion crack are likely to occur. Accordingly, the upper limit of the Ni content is defined at 1.0%. It should be noted that the Ni content is preferably 0.8% or less in view of the material cost.


Mo is an element that improves corrosion resistance, which, especially when there is a crevice structure, restrains crevice corrosion. When the Mo content exceeds 2.0%, significant deterioration in formability and productivity occurs. Accordingly, the upper limit of the Mo content is defined at 2.0%. Further, in order to restrain the growth of the {411}-oriented grains and to sharply grow the {111}-orientated grains, and in view of alloy cost and productivity, the Mo content is preferably less than 0.5%. The above effects of the Mo content is exhibited at Mo content of 0.01% or more. Accordingly, the lower limit of the Mo content is preferably defined at 0.01%. The lower limit of the Mo content content is further preferably defined at 0.1%.


Cu is added as necessary in order to restrain crevice corrosion and promote repassivation. The function due to the addition of Cu is exhibited at Cu content of 0.1% or more. Accordingly, the lower limit of the Cu content is defined at 0.1%. The C content is preferably 0.3% or more. However, addition of excessive amount of Cu causes hardening of the steel and restrains the growth of the {111}-oriented grains to reduce formability. Accordingly, the upper limit is defined at 3.0%. It should be noted that the Cu content is preferably 1.5% or less in view of the productivity.


V is added as necessary in order to restrain crevice corrosion. The function due to the addition of V is exhibited at V content of 0.05% or more. Accordingly, the lower limit of the V content is defined at 0.05%. The V content is preferably 0.1% or more. However, when more than 1.0% of V is added, the {111}-orientation intensity does not reach 5 on account of formation of coarse VN and hardening also occurs to deteriorate formability. Accordingly, the upper limit of the V content is defined at 1.0%. It should be noted that the V content is preferably 0.5% or less in view of the material cost.


Ca is added as necessary for desulfurization. The function due to the addition of Ca is not exhibited at Ca content of less than 0.0002%. Accordingly, the lower limit of the Ca content is defined at 0.0002%. On the other hand, water-soluble inclusion in a form of CaS is generated when more than 0.0030% of Ca is added to restrain the growth in the {111}-crystal orientation and promote growth in the {411}-orientation, thereby reducing the r-value. Further, in order not to considerably reduce the corrosion resistance, the upper limit of the Ca content is defined at 0.0030%. In addition, the C content is preferably 0.0015% or less in view of surface quality.


Mg is sometimes added as deoxidizing element. Further, Mg is an element that miniaturizes slab structure to contribute to growth of texture that enhances formability. The function due to the addition of Mg is exhibited at the Mg content of 0.0002% or more. Accordingly, the lower limit of the Mg content is defined at 0.0002%. The Mg content is preferably 0.0003% or more. However, when more than 0.0030% of Mg is added, the {111}-orientation intensity does not reach 5 on account of formation of coarse MgO and weldability and corrosion resistance deteriorate. Accordingly, the upper limit of the Mg content is defined at 0.0030%. The Mg content is preferably 0.0010% or more in view of the refining cost.


0.01% or more of Zr is added as necessary because Zr is bonded with C or N to promote the growth of the texture. However, when more than 0.3% of Zr is added, coarse ZrN is generated to inhibit the {111}-orientation intensity from reaching 5, production cost increases and productivity considerably deteriorates. Accordingly, the upper limit of the Zr content is defined at 0.3%. The Zr content is preferably 0.1% or less in view of the refining cost and productivity.


W is an element that contributes to improvement in corrosion resistance and high-temperature strength. Accordingly, 0.01% or more of W is added as necessary. However, when more than 3.0% of W is added, the {111}-orientation intensity does not reach 5 on account of formation of coarse WC, toughness deteriorate during the production of steel sheet and the production cost is increased. Accordingly, the upper limit of the W content is defined at 3.0%. The W content is preferably 2.0% or less in view of the refining cost and productivity.


Co is an element that contributes to improvement in high-temperature strength. Accordingly, 0.01% or more of Co is added as necessary. However, when more than 0.3% of Co is added, the {111}-orientation intensity does not reach 5 on account of formation of coarse CoS2 and deterioration in toughness during the production of steel sheet and increase in the production cost are caused. Accordingly, the upper limit of the Co content is defined at 0.3%. The Co content is preferably 0.1% or less in view of the refining cost and productivity.


Sn is an element that contributes to improvement in corrosion resistance and high-temperature strength. Accordingly, 0.003% or more of Sn is added as necessary. The Sn content is preferably 0.005% or more. However, when more than 0.50% of Sn is added, the {111}-orientation intensity does not reach 5 on account of prominent segregation of Sn at grain boundaries and the slab may be cracked during the production of steel sheet. Accordingly, the upper limit of the Sn content is defined at 0.50%. The Sn content is preferably 0.30% or less in view of the refining cost and productivity. Further, the Sn content is preferably 0.15% or less.


Sb is an element that enhances high-temperature strength by segregation at grain boundaries. In order to achieve the effect of addition, the amount of added Sb is 0.005% or more. However, when more than 0.50% of Sb is added, the {111}-orientation intensity does not reach 5 on account of prominent segregation of Sb at grain boundaries and cracks may be caused during welding process. Accordingly, the upper limit of the Sb content is defined at 0.50%. The Sb content is preferably 0.03% or more in view of high-temperature characteristics. The Sb content is more preferably 0.05% or more. The Sb content is preferably 0.30% or less in view of the production cost and toughness. The Sb content is more preferably 0.20% or less.


REM (Rare Earth Metal) is a group of elements that contributes to improvement in oxidation resistance. Accordingly, 0.001% or more of REM is added as necessary. The lower limit of the REM content is preferably defined at 0.002%. Even when more than 0.20% of REM is added, the effect of the addition of REM is saturated and the growth in the {111}-crystal orientation is restrained due to formation of coarse oxide. Further, corrosion resistance deteriorates due to REM grains. Accordingly, added amount of REM is in a range from 0.001 to 0.20%. The upper limit of the content of REM is preferably 0.10% in view of formability of the product and production cost. The REM (Rare Earth Metal) refers to those elements according to general definition. Specifically, REM refers to a group of elements consisting of: two elements of scandium (Sc) and yttrium (Y); and fifteen elements (lanthanoid) from lanthanum (La) to lutetium (Lu). REM may be singly added or may be added in a form of a mixture.


0.3% or less of Ga may be added in order to improve corrosion resistance and restrain hydrogen embrittlement. When more than 0.3% of Ga is added, coarse sulfide is generated to restrain the increase in the {111}-orientation intensity and deteriorate the r-value. The lower limit of the Ga content is defined at 0.0002% in view of formation of sulfides and hydrides. In addition, the Ga content is preferably 0.0020% or more in view of the productivity and production cost.


0.001 to 1.0% of Ta and/or Hf may be added in order to improve the high-temperature strength. Further, though the other components are not specifically defined in the exemplary embodiment, 0.001 to 0.02% of Bi may be added as necessary. It should be noted that the content of common detrimental elements (e.g. As and Pb) and impurity elements should be as small as possible.


Next, a manufacturing method will be described below. A manufacturing method of steel sheet of the exemplary embodiment includes steps of steelmaking, hot rolling, pickling, cold rolling and annealing. In the steelmaking, steel containing the above-described essential components and component(s) added as necessary are suitably melted in a converter furnace and subsequently subjected to a secondary smelting. The melted steel is formed into a slab according to known casting process (continuous casting). The slab is heated to a predetermined temperature and is hot-rolled to have a predetermined thickness through a continuous rolling procedure.


In the exemplary embodiment, the slab is subjected to pickling without applying annealing of hot-rolled sheet and is subjected to the cold rolling process as a cold rolling material. The above process is different from a typical procedure (typically, the annealing of hot-rolled sheet is applied). Though the annealing of hot-rolled sheet is applied to obtain a granulated recrystallization texture in the typical procedure, it is difficult in the typical procedure to significantly reduce the size of the crystal grains before the cold rolling. It is found in the exemplary embodiment that when the size of the crystal grains before the cold rolling is large, grain boundary area reduces so that the {111}-crystal orientation improving the r-value does not grow in a product sheet but the {411}-crystal orientation grows, so that the texture should be miniaturized by promoting the recrystallization during the hot rolling process.


The cast slab is heated at 1100 to 1200 degrees C. When the slab is heated at a temperature of more than 1200 degrees C., the crystal grains are coarsened so that the texture is not miniaturized during the hot rolling process. Thus, the {111}-crystal orientation does not grow but the {411}-crystal orientation grows to reduce the r-value. Further, if the temperature is less than 1100 degrees C., since only deformation texture develops without causing recrystallization, the ridging of the product sheet becomes unfavorable. Thus, the slab heating temperature is defined in a range from 1100 to 1200 degrees C. In addition, the heating temperature is preferably 1120 degrees C. or more in view of the productivity and surface flaw. For similar reasons, the heating temperature is preferably 1160 degrees C. or less.


After the slab is heated, a plurality of passes of rough rolling are applied. It is found in the invention that, by applying at least 30% of rolling reduction in at least (n−2) times of rough rolling (total pass number n), recrystallization eminently progresses to miniaturize the texture. This is because the recrystallization progresses in a period from the rough rolling to the finish rolling due to strain during the rough rolling. Since the growth of the {411}-oriented grains occurs in the typically known method of applying a high rolling reduction only in a final pass or defining the rolling reduction ratio between the rough rolling and the finish rolling, the formation of recrystallization orientation contributing both of improvement in the r-value and the reduction of ridging is insufficient. This is because, only by defining rolling reduction ratio between the rough rolling and the finish rolling, the desired orientation intensity cannot be sufficiently controlled under the influence of nucleus generation of the crystal grains and dependency of the crystal grain growth on crystal orientation between passes. In the invention, it is found that recrystallization repeatedly occurs by applying rolling with 30% or more of rolling reduction as much times as possible in the passes of the rough rolling. Accordingly, after the pass number and the action of the recrystallization are studied in detail, it is found that 30% or more of rolling reduction should be applied in (n−2) or more number of the passes of the rough rolling in the invention. Further, since it is difficult to control the recrystallization and grain growth between passes only by defining the rolling reduction in each of passes in the rough rolling, the end temperature of the rough rolling is defined at 1000 degrees C. or more in the invention. This is because, when the end temperature is less than 1000 degrees C., the recrystallization after the rough rolling does not progress but deformation texture mainly in the {411}-crystal orientation remains, whereby the {411}-oriented grains grow in a period between the rough rolling and the finish rolling to exert adverse influence on the r-value and ridging of a product sheet. In the invention, in order to restrain the generation and growth of the {411}-oriented grains in the period between the rough rolling and the finish rolling, the end temperature of the rough rolling is defined at 1000 degrees C. or more.


After the rough rolling, finish rolling is unidirectionally applied using a device including a plurality of stands. In the invention, the finishing temperature is 900 degrees C. or less. After the finish rolling, the product is wound. The coiling temperature is 700 degrees C. or less. In this winding step, recrystallization is not promoted but the deformation texture grows in order to miniaturize the recrystallization texture in the cold rolling and annealing after the hot rolling. Accordingly, the finish rolling temperature is set at 900 degrees C. or less and the coiling temperature is set at 700 degrees C. or less, so that restoration and recrystallization are restrained during this period to intentionally introduce the deformed strain. The finish rolling temperature is preferably 700 degrees C. or more and the coiling temperature is 500 degrees C. or more in view of surface flaw and sheet-thickness accuracy. Similarly, the finish rolling temperature is preferably 850 degrees C. or less and the coiling temperature is 650 degrees C. or less in view of surface flaw and sheet-thickness accuracy. It should be noted that, though partial recrystallization sometimes occurs depending on the composition in this step, the size of the generated recrystallized grains is extremely small and thus is not a problem.


In the exemplary embodiment, the product is subjected to pickling without applying the annealing of hot-rolled sheet and is subjected to the cold rolling process. The above process is different from a typical procedure (typically, the annealing of hot-rolled sheet is applied), which, in combination with the above-described conditions for hot rolling, provides minute recrystallized grains during the cold rolling to achieve both of the improvement in the r-value and the reduction of ridging,


In the cold rolling process, intermediate cold rolling, intermediate annealing, finish cold rolling, and finish annealing are performed in this order.


In the intermediate cold rolling, cold rolling is at least once performed at 40% or more of rolling reduction using a roller having a diameter of 400 mm or more. The roll diameter of 400 mm or more restrains shear strains during the cold rolling and also restrains the generation of crystal orientation (e.g. {411}<148>) that reduces the r-value during the subsequent annealing process.


In the intermediate annealing performed in the middle stage of the cold rolling, a recrystallization texture having grain size number of 6 or more is obtained. When the grain size number is less than 6, since the grain size is large, {111}-oriented grains are unlikely to be generated from the grain boundary but the {411}-oriented grains are formed. The grain size number is preferably less than 6.5. Further, it is found in the invention that, in addition to miniaturization of the texture during the production process, it is effective for improvement in the formability of the product to grow the {111}-crystal orientation and restrain the {411}-crystal orientation. Accordingly, the intensity in the {111}-crystal orientation in the intermediate annealing step is set at 3 or more. The {111}-orientation intensity after the intermediate annealing is set at 3 or more in the exemplary embodiment because it is found that {111}-crystal orientation is more frequently generated based on the {111}-oriented grains and the worked grains in the formation of texture during the subsequent finish cold rolling and finish annealing steps. The intensity is preferably 3.5 or more. In order to satisfy the above intensity conditions, the intermediate annealing temperature is set in a range from 820 to 880 degrees C. Though the annealing is applied at a temperature of more than 880 degrees C. in order to grow the size of the recrystallized grains in a typical intermediate annealing, the annealing is applied at a temperature lower than that in the typical intermediate annealing in order to obtain minute textures immediately after the recrystallization in the exemplary embodiment. Since the intermediate annealing temperature of less than 820 degrees C. does not grow the {111}-orientation intensity on account of failure in recrystallization but the {411}-orientation intensity increases, the lower limit of the intermediate annealing temperature is defined at 820 degrees C. On the other hand, when the intermediate annealing temperature exceeds 880 degrees C., the grain growth is already caused and the {411}-crystal grains are preferentially grown. Accordingly, the upper limit of the intermediate annealing temperature is defined at 880 degrees C. In addition, the intermediate annealing temperature is preferably 830 degrees C. or more in view of the productivity and pickling capability. In addition, the intermediate annealing temperature is preferably 875 degrees C. or less in view of the productivity and pickling capability.


The annealing temperature in the finish annealing after the finish cold rolling is set in a range from 880 to 950 degrees C. to adjust the grain size number at 5.5 or more. When the grain size number is less than 5.5, ridging or surface roughness (so-called orange peel) becomes prominent. Accordingly, the upper limit of the grain size number is defined at 5.5. Since the annealing temperature satisfying the above requirement is 950 degrees C. or less, the upper limit of the annealing temperature is defined at 950 degrees C. On the other hand, since the non-recrystallized texture sometimes partially remains when the annealing temperature is less than 880 degrees C., the lower limit of the annealing temperature is defined at 880 degrees C. Further, the annealing temperature is preferably 910 degrees C. or less and the grain size number is 6.5 or more in view of the productivity, pickling capability and surface quality.


Other conditions in the manufacture process may be determined as desired. For instance, slab thickness, hot-rolling sheet thickness and the like may be determined as desired. The roll roughness, roll diameter, rolling oil, rolling pass number, rolling speed, rolling temperature and the like in the cold rolling may be determined as desired within a range compatible with an object of the invention. When the intermediate annealing is performed during the cold rolling, any one of batch annealing and continuous annealing may be employed. The annealing may be performed in a low-oxygen atmosphere (e.g. hydrogen gas or nitrogen gas) (bright annealing) or may be performed in the atmospheric air as needed. Further, lubrication painting may be applied to the product sheet to further enhance pressing formability. In such an arrangement, the type of the lubrication film may be determined as desired.


The stainless steel sheet according to the above exemplary embodiment exhibits a high r-value and low ridging height and is excellent in pressing formability. Accordingly, the ferritic stainless steel pipe made of the stainless steel sheet of the exemplary embodiment is excellent in pipe expansivity and formability. The method for manufacturing the steel pipe may be determined as desired, where any welding process may be used (e.g. ERW, laser welding, TIG).


A ferritic stainless steel sheet for an automobile exhaust component can be provided using the stainless steel sheet of the exemplary embodiment. Especially, with the use of the stainless steel sheet for exhaust components of automobiles or motorcycles, degree of freedom for molding is enhanced and integral molding and the like without requiring welding between components becomes possible, thereby enabling efficient manufacture of components.


A second exemplary embodiment adapted to achieve the above-described second object will be described below.


Examples of indexes for formability include the r-value indicating deep drawability. The r-value is influenced by the crystal orientation of the steel and increases as more {111}-crystal orientations (so-called Y-fiber, i.e. crystal grains having {111} crystal face parallel to a sheet face of the steel sheet in a body-centered cubic crystal structure) are present.


In the invention, it is found that the {111}-orientation intensity of a product sheet increases and generation of the {311}<136> texture that reduces formability can be restrained by applying the intermediate annealing between the intermediate cold rolling and the finish cold rolling in the steel sheet manufacturing process.


The average r-value (rm) of the steel sheet of the exemplary embodiment is rm≥−1.0t+3.0, which shows excellent formability. FIG. 3 shows average r-values of Examples manufactured in accordance with the present exemplary embodiment (white squares in FIG. 3) and average r-values of steel sheets (Comparative Example: black squares in FIG. 3) manufactured in accordance with processes not satisfying the conditions of the exemplary embodiment, with reference to the sheet thickness. When the sheet thickness is t (mm) and the average r-value is rm, since the average r-value of the ferritic stainless steel sheet manufactured according to the exemplary embodiment satisfies −rm≥−1.0t+3.0, the relationship between the average r-value and the sheet thickness is represented by rm≥−1.0t+3.0. Further, considering that 1.8 or more of average r-value is necessary in order to perform a 2D pipe expansion of a steel pipe when the sheet thickness t is 1.2 mm or more, it is desirable that, when t≥1.2 mm, rm≥−1.0t+3.0.



FIG. 4 illustrates a relationship between the average r-value and {311}<136>-orientation intensity. In order for the average r-value to be 1.8 or more (i.e. a value capable of enduring 2D pipe expansion), it is necessary for the {111}<110>-orientation intensity to be 4.0 or more. The data plotted in FIG. 4 all show {111}<110>-orientation intensity of 4.0 or more. Further, as is clear from FIG. 4, when the {311}<136>-orientation intensity is 3.0 or more, the average r-value becomes extremely small. Based on the above, {111}<110>-orientation intensity is defined at 4.0 or more and {311}<136>-orientation intensity is defined at less than 3.0 in the invention. More preferably, {111}<110>-orientation intensity is defined at 7 or more and {311}<136>-orientation intensity is defined at less than 2.


In the invention, without relying on the conventionally known increase in the r-value by increasing the {111}<110>-orientation intensity, a high r-value is achieved by reducing the {311}<136>-orientation intensity.


Further, the grain size number of the steel sheet of the invention is preferably adjusted to be 6 or more. When the grain size number is less than 6, ridging or surface roughness (so-called orange peel) becomes prominent. Accordingly, the lower limit of the grain size number is defined at 6. Further preferably, the grain size number is 6.5 or more.


Next, a composition of the steel will be described below. It should be noted that the percentages used in indicating the composition all represent mass %.


C deteriorates formability and corrosion resistance. Especially, the development in the {311}-crystal orientation is greatly affected by solid solution C. Accordingly, the C content is preferably as small as possible and the upper limit of the C content is defined at 0.03%. However, excessive reduction of the C content results in increase in refining cost. Accordingly, the lower limit of the C content is defined at 0.001%. In addition, the C content is preferably 0.002% or more in view of the production cost. The C content is preferably 0.01% or less in view of boundary corrosivity at a welded part.


Similarly to C, N deteriorates formability and corrosion resistance. In addition, the growth of the {311}-orientated grains is greatly affected by solid solution N. Accordingly, the N content is preferably as small as possible and the upper limit of the N content is defined at 0.03%. However, excessive reduction in the N content results in increase in refining cost. Accordingly, the lower limit of the N content is defined at 0.001%. In addition, the N content is preferably 0.005% or more in view of the production cost. The N content is preferably 0.015% or less in view of formability and corrosion resistance.


Si is sometimes added as a deoxidizing element. In addition, Si improves the oxidation resistance. On the other hand, since Si is a solid solution strengthening element, the Si content is preferably 1.0% or less in order to ensure total elongation. Further, much amount of added Si causes change in a slip system to promote the growth in the {311}-crystal orientation. Accordingly, the upper limit of the Si content is defined at 1.0%. In addition, the Si content is preferably 0.2% or more in view of the corrosion resistance. The Si content is more preferably 0.3% or more. The Si content is further preferably 0.32% or more. The Si content is still further preferably 0.4% or more. The Si content is preferably 0.5% or less in view of the production cost.


Similarly to Si, Mn is a solid solution strengthening element. Accordingly, the upper limit of the Mn content is defined at 3.0% in view of the material. In addition, the Mn content is preferably 0.1% or more in view of the corrosion resistance. The Mn content is more preferably 0.3% or more. The Mn content is further preferably 0.32% or more. The Mn content is still further preferably 0.4% or more. The Mn content is preferably 0.5% or less in view of the production cost.


Since P is a solid solution strengthening element similarly to Mn and Si, the P content in the material is preferably as small as possible. Further, much amount of added P causes change in the slip system to promote the growth in the {311}-crystal orientation. Accordingly, the upper limit of the P content is defined at 0.04%. In addition, the P content is preferably 0.01% or more in view of the production cost. The P content is preferably 0.02% or less in view of the corrosion resistance.


S is an element that deteriorates corrosion resistance. Accordingly, the upper limit of the S content is defined at 0.01%. On the other hand, S forms Ti4C2S2 in Ti-containing steel at a high temperature to contribute to the growth in the texture effective for improving the r-value. The formation of Ti4C2S2 is exhibited when S is contained at an amount of 0.0003% or more. Accordingly, the lower limit of the S content is defined at 0.0003%. In addition, the S content is preferably 0.0005% or more in view of the production cost. The S content is preferably 0.0050% or less in view of boundary corrosivity in produced components.


Cr is an element that improves corrosion resistance and oxidation resistance. In view of environment in which exhaust components are provided, 10% or more of Cr is necessary in order to restrain abnormal oxidation. The Cr content is still further preferably 10.5% or more. On the other hand, excessive addition of Cr hardens the steel to deteriorate the formability, restrains the growth of the {111}-oriented grains and promotes the growth of the {311}-oriented grains. Further, in fear of increase in the production cost, the upper limit of the Cr content is defined at 30%. It should be noted that, in view of the production cost, sheet breakage due to deterioration in toughness and formability during the production of steel sheet, the upper limit of the Cr content is preferably less than 15%. When the Cr content is 15% or more, the steel hardens to promote the growth of the {311}-oriented grains. The upper limit of the Cr content is preferably 13% or less.


Al is sometimes added as a deoxidizing element. In addition, Al restrains the oxide scales from peeling. The Al content is preferably 0.01% or more. On the other hand, the added Al content exceeding 0.300% causes reduction in elongation, and deterioration in weld compatibility and surface quality. Accordingly, the upper limit of the Al content is defined at 0.300%. Further, the Al content is preferably 0.15% or less in view of the refining cost and pickling capability during steel sheet production.


The stainless steel sheet of the exemplary embodiment contains one or more of Ti and Nb.


Ti is an element added to be bonded to C, N and S to improve the corrosion resistance, intercrystalline corrosion resistance and deep drawability. The fixing function for C and/or N appears at a Ti concentration of 0.05% or more. When the Ti concentration is less than 0.05%, solid solution C and solid solution N that greatly contributes to the growth of the {311}-crystal orientation cannot be sufficiently fixed. Accordingly, the lower limit of the Ti content is defined at 0.05%. The Ti content is preferably 0.06% or more. Further, when more than 0.30% of Ti is added, the product is hardened due to solid solution Ti to cause the growth of the {311}-orientated grains and deterioration of toughness. Accordingly, the upper limit of the Ti content is defined at 0.30%. Further, the Ti content is preferably 0.25% or less in view of the production cost and the like.


Similarly to Ti, Nb is an element added to be bonded to C, N and S to improve the corrosion resistance, intercrystalline corrosion resistance and deep drawability. Nb is added as necessary because Nb is effective for improvement in formability and high-temperature strength due to the growth in the {111}-oriented grains and for inhibition of crevice corrosion and promotion of repassivation. The function due to the addition of Nb is exhibited at a Nb concentration of 0.01% or more. Accordingly, the lower limit of the Nb content is defined at 0.01%. The Nb content is preferably 0.05% or more. However, excessive addition of Nb hardens the steel to deteriorate the formability, restrains the growth of the {111}-oriented grains and promotes the growth of the {311}-oriented grains. Accordingly, the upper limit of the Nb content is defined at 0.50%. Further, the Nb content is preferably 0.3% or less in view of the production cost.


Further, the addition of Ti and Nb is scarcely effective when the sum of the contents of Ti and Nb is less than 8(C+N) (i.e. Theight times as much as the sum of C and N contents: when much amounts of C and N are present) or less than 0.05% (when the amounts of C and N are small). When the sum of the contents of Ti and Nb exceeds 0.75%, the solid solution Ti and solid solution Nb unfavorably increase to raise the recrystallization temperature. The sum of the contents of Ti and Nb are defined to be smaller one of 8(C+N) and 0.05% or more, and 0.75% or less.


The stainless steel sheet according to the exemplary embodiment may further optionally contain the following elements.


B is an element that enhances secondary formability by segregation at grain boundaries. In order to restrain vertical crack of an exhaust component when the exhaust component is subjected to a secondary processing, especially in winter, 0.0002% or more of B has to be added. The B content is preferably 0.0003% or more. However, addition of excessive amount of B restrains the growth of the {111}-oriented grains and reduces formability and corrosion resistance. Accordingly, the upper limit of the B content is defined at 0.0030%. In addition, the B content is preferably 0.0015% or less in view of the refining cost and decrease in ductility.


Ni is added as necessary in order to restrain crevice corrosion and promote repassivation. The function due to the addition of Ni is exhibited at Ni content of 0.1% or more. Accordingly, the lower limit of the Ni content is defined at 0.1%. The Ni content is more preferably 0.2% or more. However, since the excessive addition of Ni causes hardening of the steel to deteriorate the formability and is likely to cause stress corrosion crack, the upper limit of the Ni content is defined at 1.0%. It should be noted that the Ni content is preferably 0.8% or less in view of the material cost. The Ni content is more preferably 0.5% or less.


Mo is an element that improves corrosion resistance, which, especially when there is a crevice structure, restrains crevice corrosion. The function due to the addition of Mo is exhibited at Mo content of 0.1% or more. Accordingly, the lower limit of the Mo content is defined at 0.1%. When the Mo content exceeds 2.0%, significant deterioration in formability and productivity occurs. Further, though an appropriate amount of Mo restrains the growth of the {311}-oriented grains and promotes sharp growth of the {111}-crystal orientation, excessive addition of Mo causes hardening due to solid solution Mo and growth in the {311}-oriented grains. Accordingly, the upper limit of the Mo content is defined at 2.0%. It should be noted that the Mo content is preferably 0.5% or less in view of the alloy cost and productivity.


Cu is added as necessary in order to restrain crevice corrosion and promote repassivation. The function due to the addition of Cu is exhibited at Cu content of 0.1% or more. Accordingly, the lower limit of the Cu content is defined at 0.1%. The Cu content is preferably 0.15% or more. However, addition of excessive amount of Cu causes hardening of the steel and deteriorates formability. Accordingly, the upper limit of the Cu content is defined at 3.0%. The Cu content is preferably 1.0% or less.


V is added as necessary in order to restrain crevice corrosion. The function due to the addition of V is exhibited at V content of 0.05% or more. Accordingly, the lower limit of the V content is defined at 0.05%. The V content is preferably 0.1% or more. However, addition of excessive amount of V causes hardening of the steel and deteriorates formability. Accordingly, the upper limit of the V content is defined at 1.0%. It should be noted that the V content is preferably 0.5% or less in view of the material cost.


Ca is added as necessary for desulfurization. The function due to the addition of Ca is not exhibited at Ca content of less than 0.0002%. Accordingly, the lower limit of the Ca content is defined at 0.0002%. On the other hand, water-soluble inclusion in a form of CaS is generated when more than 0.0030% of Ca is added to reduce the r-value. Further, the corrosion resistance is considerably reduced. Accordingly, the upper limit of the Ca content is defined at 0.0030%. In addition, the Ca content is preferably 0.0015% or less in view of surface quality.


Mg is sometimes added as deoxidizing element. Further, Mg is an element that miniaturizes slab structure to contribute to growth of texture that enhances formability. The function due to the addition of Mg is exhibited at Mg content of 0.0002% or more. Accordingly, the lower limit of the Mg content is defined at 0.0002%. The Mg content is preferably 0.0003% or more. However, addition of excessive amount of Mg deteriorates weldability and corrosion resistance. Accordingly, the upper limit of the Mg content is defined at 0.0030%. The Mg content is preferably 0.0010% or more in view of the refining cost.


Sn is an element that contributes to improvement in corrosion resistance and high-temperature strength. Accordingly, 0.005% or more of Sn is added as necessary. The Sn content is preferably 0.003% or more. However, addition of more than 0.50% of Sn may cause slab cracking during the production of steel sheets. Accordingly, the upper limit of the Sn content is defined at 0.50%. The Sn content is preferably 0.30% or less in view of the refining cost and productivity.


Zr is an element that is bonded with C and/or N to promote growth in texture. Accordingly, 0.01% or more of Zn is added as necessary. The Zr content is preferably 0.03% or more. However, the addition of more than 0.30% of Zr results in increase in the production cost and considerable deterioration in productivity. Accordingly, the upper limit of the Zr content is defined at 0.30%. The Zr content is preferably 0.20% or less in view of the refining cost and productivity.


W is an element that contributes to improvement in corrosion resistance and high-temperature strength. Accordingly, 0.01% or more of W is added as necessary. However, addition of more than 3.0% of W results in deterioration in toughness during the production of steel sheets and increase in the production cost. Accordingly, the upper limit of the W content is defined at 3.0%. The W content is preferably 0.10% or less in view of the refining cost and productivity.


Co is an element that contributes to improvement in high-temperature strength. Accordingly, 0.01% or more of Co is added as necessary. However, addition of more than 0.30% of Co results in deterioration in toughness during the production of steel sheets and increase in the production cost. Accordingly, the upper limit of the Co content is defined at 0.30%. The Co content is preferably 0.10% or less in view of the refining cost and productivity.


Sb is an element that enhances high-temperature strength by segregation at grain boundaries. The function due to the addition of Sb is exhibited at Sb content of 0.005% or more. Accordingly, the lower limit of the Sb content is defined at 0.005%. The Sb content is preferably 0.03% or more. The Sb content is more preferably 0.05% or more. However, when more than 0.50% of Sb is added, cracks may be caused during welding process due to segregation of Sb. Accordingly, the upper limit of the Sb content is defined at 0.50%. The Sb content is preferably 0.30% or less in view of high-temperature characteristics, production cost and toughness. The Sb content is more preferably 0.20% or less.


REM (Rare Earth Metal) is a group of elements that contributes to improvement in oxidation resistance. Accordingly, 0.001% or more of REM is added as necessary. Even when more than 0.20% of REM is added, the effect of the addition of REM is saturated and the corrosion resistance is reduced due to sulfide of REM. Accordingly, REM is added in an amount ranging from 0.001 to 0.20%. The lower limit of the REM content is preferably defined at 0.002%. The upper limit of the content of REM is preferably 0.10% in view of formability of the product and production cost. The REM refers to those elements according to general definition. Specifically, REM refers to a group of elements consisting of: two elements of scandium (Sc) and yttrium (Y); and fifteen elements (lanthanoid) from lanthanum (La) to lutetium (Lu). REM may be singly added or may be added in a form of a mixture.


0.3% or less of Ga may be added in order to improve corrosion resistance and restrain hydrogen embrittlement. When more than 0.3% of Ga is added, coarse sulfide is generated to restrain the increase in the {111}<110>-orientation intensity. The lower limit of the Ga content is defined at 0.0002% in view of formation of sulfides and hydrides. In addition, the Ga content is preferably 0.0020% or more in view of the productivity and production cost.


0.001% to 1.0% of Ta and/or Hf may be added in order to improve the high-temperature strength. 0.01% or more of Ta and/or Hf is effective and 0.1% or more of Ta and/or Hf further enhances the strength. In addition, 0.001 to 0.02% of Bi may be added as necessary. It should be noted that the content of common detrimental impurity element (e.g. As and Pb) should be as small as possible.


The stainless steel sheet of the above exemplary embodiment may be preferably used as a ferritic stainless steel sheet with excellent formability suitable for automobile or motorcycle components. More specifically, the stainless steel sheet of the above exemplary embodiment may be preferably used as a ferritic stainless steel sheet with excellent formability suitable for exhaust pipe, fuel tank or fuel pipe for automobiles. With the use of the stainless steel sheet for producing automobile or motorcycle components (specifically, exhaust pipes, fuel tank or fuel pipe of automobiles), degree of freedom for molding is enhanced and integral molding and the like without requiring welding between components becomes possible, thereby enabling efficient manufacture of components.


The ferritic stainless steel pipe with excellent formability made of the stainless steel sheet of the above exemplary embodiment has formability sufficient to provide a steel pipe made of a relatively thick steel sheet having more than 1 mm thickness and capable of enduring 2D pipe expansion processing (a processing expanding an end diameter D of the pipe to 2D (i.e. double the diameter).


Next, a manufacturing method will be described below. A manufacturing method of steel sheet of the exemplary embodiment includes steps of steelmaking, hot rolling, pickling, and subsequent repetitions of cold rolling and annealing. In the steelmaking, steel containing the above-described essential components and component(s) added as necessary are suitably melted in a converter furnace and subsequently subjected to a secondary smelting. The melted steel is formed into a slab according to known casting process (continuous casting). The slab is heated to a predetermined temperature and is hot-rolled to have a predetermined thickness through a continuous rolling procedure.


In the exemplary embodiment, the slab is subjected to pickling without applying annealing of hot-rolled sheet and is subjected to the cold rolling process as a cold rolling material. The above process is different from a typical procedure (typically, the annealing of hot-rolled sheet is applied). Though the annealing of hot-rolled sheet is applied to obtain a granulated recrystallization texture in the typical procedure, it is difficult in the typical procedure to significantly reduce the size of the crystal grains before the cold rolling. When the size of the crystal grain before the cold rolling is large, a grain boundary area reduces so that the {111}-crystal orientation improving the r-value does not grow in a product sheet but the {311}-crystal orientation grows. Accordingly, it is found in the exemplary embodiment that texture should be miniaturized by promoting the recrystallization during the hot rolling process without applying the hot-rolling sheet annealing.


The cast slab is heated at 1100 to 1200 degrees C. When the slab is heated at a temperature more than 1200 degrees C., the crystal grains are coarsened so that the texture is not miniaturized during the hot rolling process. Thus, the {111}-crystal orientation does not grow but the {311}-crystal orientation unfavorably grows to reduce the r-value. When the slab is heated at a temperature less than 1100 degrees C., only the deformation texture is grown without causing the recrystallization. Thus, the {111}-crystal orientation does not grow but the {311}-crystal orientation grows to reduce the r-value. In addition, ridging characteristics of the product sheet becomes unfavorable. Thus, the favorable slab heating temperature is defined in a range from 1100 to 1200 degrees C. In addition, the heating temperature is preferably 1160 degrees C. or less in view of the productivity. The heating temperature is preferably 1120 degrees C. or more in view of surface scar.


In the hot rolling process after heating the slab, a plurality of passes of rough rolling and unidirectional finish rolling using a plurality of stands are applied. After the rough rolling, finish rolling is applied at a high speed and the product is wound in a coil. In the exemplary embodiment, in order to obtain minute recrystallized texture during the winding step, rough rolling temperature and coiling temperature are defined. In order to improve formability, it is important to recrystallize the product to form minute textures after the product is wound. Formation of the minute textures after the product is wound can restrain shear deformation during the subsequent cold rolling process, can reduce the formation of the {311}-texture and further can grow the {111}-texture. When the coiling temperature is excessively low, since the recrystallization does not occur during the winding process, it is necessary to perform the finish rolling at a high temperature and a high speed. Accordingly, the finish rolling process is defined so that a start temperature is 900 degrees C. or more and end temperature is 800 degrees C. or more, a difference between the start and end temperatures is 200 degrees C. or less and the coiling temperature is also defined to be 600 degrees C. or more. It is preferable that the start temperature is 950 degrees C. or more, the end temperature is 820 degrees C. or more and the difference between the start and end temperatures is 150 degrees C. or less.


In the exemplary embodiment, the product is subjected to pickling without applying the annealing of hot-rolled sheet and is subjected to the cold rolling process. The above process is different from a typical procedure (typically, the annealing of hot-rolled sheet is applied), which, in combination with the above-described conditions for hot rolling, provides minute recrystallized grains during the cold rolling to achieve the improvement in the r-value, In the cold rolling process, intermediate cold rolling, intermediate annealing, finish cold rolling, and finish annealing are performed in this order.


The cold rolling may be performed using a reversible 20-stage Sendzimir rolling mill or a 6 or 12-stage tandem rolling mill configured to continuously roll a plurality of passes. It should be noted, however, the cold rolling is at least once performed at 40% or more of rolling reduction using a roller having a diameter of 400 mm or more. The roll diameter of 400 mm or more restrains shear strains during the cold rolling and also restrains the generation of crystal orientation (e.g. {311}<136>) that reduces the r-value during the subsequent annealing process. The above large-roller rolling is preferably performed during the intermediate cold rolling.


In the intermediate annealing performed in the middle stage of the cold rolling, a recrystallization texture or a texture immediately before completion of recrystallization is obtained. The grain size number of the texture immediately before completion of recrystallization is preferably 6 or more. When the grain size number is less than 6, since the grain size is large, {111}-oriented grains are unlikely to be generated from the grain boundary, which hinders improvement in the r-value especially in a thick material. The grain size number is further preferably 6.5 or more. In order to satisfy the above conditions, the intermediate annealing temperature is set in a range from 800 to 880 degrees C. Though the annealing is applied at a temperature of more than 880 degrees C. in order to grow the size of the recrystallized grains in a typical intermediate annealing, the annealing is applied at a temperature lower than that in the typical intermediate annealing in order to obtain minute textures immediately before the recrystallization or immediately after the recrystallization in the exemplary embodiment. The intermediate annealing temperature of less than 800 degrees C. causes non-recrystallized textures. Accordingly, the lower limit of the intermediate annealing temperature is defined at 800 degrees C. In addition, the intermediate annealing temperature is preferably 825 degrees C. or more in view of the productivity and pickling capability. Further, the intermediate annealing temperature is preferably less than 870 degrees C. in view of the productivity and pickling capability. Herein, the recrystallization completion texture refers to a texture in which all of the grains are equiaxially recrystallized and the texture immediately before the completion of recrystallization refers to a texture in which slightly stretched non-recrystallized texture remains in addition to the equiaxial crystal grains.


In the finish cold rolling, since high rolling reduction results in increase in accumulated energy as a driving force of recrystallization so that it is likely that nucleus of the {111}-crystal orientation is preferentially generated and the {111}-crystal orientation is selectively grown. Accordingly, at least 60% rolling reduction is applied during the cold rolling.


The annealing temperature in the finish annealing after the finish cold rolling is set in a range from 850 to 950 degrees C. to adjust the grain size number at 6 or more. When the grain size number is less than 6, ridging or surface roughness (so-called orange peel) becomes prominent. Accordingly, the lower limit of the grain size number is preferably defined at 6. The grain size number is preferably 6.5 or more. In addition, the annealing temperature is preferably 880 degrees C. or more in view of the productivity, pickling capability and surface quality. Furthermore, the annealing temperature is preferably 910 degrees C. or less in view of the productivity, pickling capability and surface quality.


EXAMPLES

Examples for the above-described first exemplary embodiment will be described below.


Steels of compositions shown in Tables 1-1 and 1-2 were melted and cast into a slab. Ten, the steels were subjected to hot rolling, (without applying the annealing of hot-rolled sheet), cold rolling, intermediate annealing, finish cold rolling and finish annealing to obtain a product sheet having 1.2 mm thickness. It should be noted that, regarding the conditions for the hot rolling, rough rolling reduction and finish rolling reduction were also studied, where the characteristics of each of the steels were examined. The steels were manufactured under the conditions shown in Tables 2-1, 2-2 and 2-3. Evaluation methods for the {111}-orientation intensity, {411}-orientation intensity, average r-value and ridging in the vicinity of the sheet-thickness central portion are as described above.












TABLE 1-1









Steel
Content (mass %)




















No.
C
Si
Mn
P
S
Cr
N
Ti
Nb
B
Al





Exemplary
A1
0.005
0.45
0.12
0.02
0.0007
11.1
0.009
0.17





Embodiment
A2
0.008
0.25
0.18
0.02
0.0008
17.3
0.013

0.28





A3
0.003
0.43
0.42
0.03
0.0012
13.9
0.010
0.19

0.0010
0.05



A4
0.009
0.22
0.12
0.03
0.0023
11.1
0.014
0.22

0.0005
0.07



A5
0.002
0.44
0.35
0.03
0.0043
17.9
0.006
0.22

0.0011
0.04



A6
0.006
0.43
0.12
0.02
0.0018
17.5
0.006
0.08

0.0005




A7
0.004
0.21
0.15
0.03
0.0005
11.7
0.011
0.19
0.12
0.0004
0.03



A8
0.003
0.33
0.23
0.03
0.0032
14.2
0.010
0.09

0.0010
0.05



A9
0.008
0.11
0.12
0.03
0.0007
17.5
0.009
0.14

0.0004
0.08



A10
0.005
0.32
0.27
0.02
0.0007
11.8
0.016
0.25

0.0006
0.12



A11
0.009
0.34
0.10
0.03
0.0008
14.4
0.014
0.07

0.0006
0.09



A12
0.005
0.28
0.18
0.01
0.0031
17.3
0.006
0.18
0.25
0.0004
0.02



A13
0.006
0.44
0.15
0.03
0.0009
12.3
0.006
0.17

0.0004
0.07



A14
0.005
0.35
0.12
0.02
0.0005
11.5
0.009
0.17






A15
0.007
0.24
0.28
0.02
0.0008
17.3
0.013
0.24






A16
0.003
0.43
0.33
0.03
0.0012
13.9
0.010
0.19






A17
0.007
0.43
0.15
0.03
0.0008
13.5
0.015
0.16






A18
0.009
0.47
0.23
0.02
0.0006
13.4
0.013
0.23






A19
0.008
0.24
0.32
0.03
0.0006
12.5
0.008
0.25






A20
0.005
0.46
0.22
0.02
0.0006
11.5
0.013
0.19






A21
0.025
0.54
0.33
0.04
0.0013
19.7
0.027
0.28
0.45





A22
0.011
0.88
0.93
0.04
0.0006
13.9
0.013

0.85

0.18



A23
0.016
0.56
0.25
0.03
0.0025
17.1
0.013
0.19
0.39
0.0009
0.11



A24
0.007
0.16
0.15
0.03
0.0019
13.5
0.015

0.16
0.0025
0.25



A25
0.019
0.75
0.12
0.01
0.0088
11.5
0.013
0.23






A26
0.009
0.28
0.32
0.03
0.0006
17.3
0.019
0.12
0.53
0.0005
0.10



A27
0.013
0.22
0.35
0.05
0.0035
17.1
0.013

0.51
0.0009
0.09













Steel
Content (mass %)


















No.
Ni
Mo
Cu
V
Mg
Sn
Others







Exemplary
A1










Embodiment
A2











A3











A4


1.2
0.12







A5
0.2 










A6

0.8









A7


0.3








A8



0.19
0.0005






A9





0.11





A10






Zr: 0.03




A11






W: 1.5




A12


 1.30



Co: 0.05




A13
0.13
 0.12
 0.11
0.13
0.0003






A14





0.01





A15






Sb: 0.01




A16






REM: 0.005




A17






Ca: 0.0010




A18






Ga: 0.0020




A19






Hf: 0.006




A20






Ta: 0.005




A21











A22











A23



0.81







A24




0.0022






A25
0.80
1.8









A26
0.10
0.3
1.2
0.10







A27

1.8
1.5



W: 2.8




















TABLE 1-2









Steel
Content (mass %)




















No.
C
Si
Mn
P
S
Cr
N
Ti
Nb
B
Al





Comparative
B1
0.035*
0.24
0.37
0.02
0.0009
10.7
0.011

0.22 




Example
B2
0.005
0.95*
0.25
0.02
0.0009
17.3
0.006
0.18

0.0009
0.09



B3
0.013
0.32
1.53*
0.02
0.0012
14.5
0.010
0.22






B4
0.003
0.42
0.43
0.06*
0.0003
16.3
0.010
0.12

0.0007
0.05



B5
0.007
0.26
0.32
0.02
0.0192*
18.8
0.013
0.16






B6
0.012
0.31
0.34
0.04
0.0026
22.3*
0.005
0.08

0.0005




B7
0.004
0.25
0.36
0.02
0.0015
17.5
0.04*
0.22






B8
0.003
0.26
0.12
0.03
0.0053
14.1
0.015
1.55*






B9
0.008
0.39
0.12
0.03
0.0035
16.2
0.005
0.23

 0.0100*




B10
0.009
0.29
0.26
0.01
0.0015
19.5
0.005
0.17


 0.44*



B11
0.006
0.36
0.33
0.04
0.0033
11.1
0.007
0.10






B12
0.002
0.42
0.42
0.02
0.0032
13.8
0.006
0.10






B13
0.003
0.17
0.26
0.03
0.0013
16.5
0.012
0.07
1.60*

0.04



B14
0.011
0.25
0.27
0.02
0.0023
11.9
0.006
0.11






B15
0.005
0.31
0.21
0.01
0.0016
13.5
0.010
0.14


0.03



B16
0.009
0.39
0.12
0.04
0.0022
14.5
0.013
0.22






B17
0.006
0.21
0.33
0.03
0.0007
17.3
0.016
0.19






B18
0.005
0.32
0.17
0.05
0.0011
13.6
0.013
0.09


0.06



B19
0.005
0.21
0.25
0.01
0.0025
16.3
0.009
0.15


0.13



B20
0.009
0.33
0.13
0.02
0.0016
10.8
0.015
0.12






B21
0.005
0.32
0.17
0.05
0.0011
13.6
0.013
0.09






B22
0.005
0.21
0.25
0.01
0.0025
16.3
0.009
0.15






B23
0.009
0.33
0.13
0.02
0.0016
10.8
0.015
0.12






B24
0.006
0.26
0.42
0.01
0.0026
14.2
0.009
0.33






B25
0.011
0.23
0.31
0.02
0.0025
11.1
0.015
0.25
















Steel
Content (mass %)


















No.
Ni
Mo
Cu
V
Mg
Sn
Others







Comparative
B1










Example
B2











B3











B4











B5











B6











B7











B8











B9











B10











B11
1.3*










B12

2.5*









B13











B14


3.1*








B15



1.12*







B16




0.0045*






B17





0.62*





B18






Zr: 0.53*




B19






W: 3.1*




B20






Co: 0.48*




B21





0.7* 





B22






Sb: 0.8*




B23






REM: 0.3*




B24






Ca: 0.004*




B25






Ga: 0.5*







*Out of the scope of the invention
















TABLE 2-1










Hot-Rolling





Condition
























rolling pass













number with







rolling
rolling
Rough

Rough






total
pass
reduction
Rolling
total
rolling





heating
rolling
number
of 30% or
End
rolling
reduction/
Finish
Coiling





temper-
reduction
in
more in
temper-
reduction
finish
Temper-
Temper-




Steel
ature
in Rough
Rough
Rough
ature
in finish
rolling
ature
ature



No.
No.
° C.
rolling %
rolling
rolling
° C.
rolling %
reduction
° C.
° C.





Exemplary
1
A1
1120
89
7
5
1020
82
1.1
830
640


Embodiment
2
A2
1120
87
7
5
1005
81
1.1
850
600



3
A3
1160
90
7
5
1020
78
1.2
820
580



4
A4
1160
89
7
6
1050
80
1.1
750
550



5
A5
1160
89
7
6
1010
75
1.2
800
630



6
A6
1120
89
7
5
1030
79
1.1
840
640



7
A7
1200
88
5
3
1060
82
1.1
830
600



8
A8
1120
89
7
5
1010
82
1.1
830
640



9
A9
1120
93
7
5
1010
80
1.2
850
600



10
A10
1160
88
7
5
1020
82
1.1
820
580



11
A11
1160
89
7
6
1030
78
1.1
750
550



12
A12
1160
92
7
5
1050
82
1.1
820
580



13
A13
1200
85
5
3
1050
80
1.1
850
610



14
A14
1120
89
7
5
1060
82
1.1
830
640



15
A15
1120
89
7
5
1010
80
1.1
850
600



16
A16
1160
90
7
5
1010
78
1.2
820
580



17
A17
1120
89
7
5
1070
82
1.1
830
640



18
A18
1120
91
7
5
1030
70
1.3
850
600



19
A19
1160
89
5
5
1020
80
1.1
770
650



20
A20
1150
88
5
4
1050
77
1.1
780
620



21
A21
1200
88
7
5
1010
81
1.1
830
500



22
A22
1160
87
7
5
1030
82
1.1
820
580



23
A23
1200
89
5
3
1020
80
1.1
850
450



24
A24
1160
90
7
5
1030
78
1.2
820
580



25
A25
1160
90
7
5
1020
78
1.2
820
580



26
A26
1200
91
7
5
1050
78
1.2
850
430



27
A27
1200
88
7
5
1010
81
1.1
830
500

















Intermediate
Final




Intermediate
Annealing
Annealing













Rolling
Annealing

Annealing


















Roll

Temper-
(111)Orient-
Grain
Temper-
Grain




Diameter
Rolling
ature
ation
size
ature
size



No.
mm
Reduction %
° C.
Intensity
number
° C.
number





Exemplary
1
500
44
850
3.1
7.2
900
7.2


Embodiment
2
500
44
870
4.2
7.3
910
6.5



3
500
55
870
3.3
7.5
900
5.9



4
500
55
850
7.2
8.1
890
7.5



5
450
46
830
5.4
7.5
900
7.9



6
450
46
835
3.2
6.5
920
6.8



7
400
44
850
6.1
6.8
925
6.3



8
500
44
850
3.1
7.2
900
7.0



9
500
44
870
4.3
7.5
910
6.5



10
500
55
870
3.1
7.5
900
5.9



11
500
55
850
7.2
8.1
890
7.5



12
500
55
870
3.2
7.5
900
5.9



13
400
44
850
8.1
7.2
940
7.0



14
500
44
850
3.4
7.2
900
7.2



15
500
44
870
4.4
7.3
910
6.5



16
500
55
870
3.2
7.5
900
5.9



17
500
44
850
3.3
7.2
900
7.2



18
500
44
870
4.1
7.3
910
6.5



19
500
45
840
5.2
7.7
900
6.8



20
450
55
840
6.6
8.1
890
7.6



21
500
44
870
4.1
7.5
950
6.3



22
500
55
870
3.1
7.5
910
6.6



23
500
44
880
3.8
7.6
950
7.1



24
500
55
840
6.8
7.4
950
5.8



25
500
55
880
3.2
7.4
900
6.2



26
500
44
880
4.5
7.8
950
6.3



27
500
44
870
4.1
7.5
950
6.3
















Characteristics of





Product Sheet





















Result





(111)Orient-
(411)Orient-

Ridging
of Pipe





ation
ation
Average
Height
Expansion




No.
Intensity
Intensity
r-value
μm
Test







Exemplary
1
7.2
1.1
1.7
5
A



Embodiment
2
8.1
1.1
1.8
7
A




3
7.0
2.1
1.7
5
A




4
9.2
1.2
1.8
6
A




5
10.3
2.3
1.9
3
A




6
6.0
2.1
1.7
2
A




7
7.2
2.2
1.7
5
A




8
10.1
1.1
1.9
5
A




9
14.3
1.1
2.0
6
A




10
8.0
2.1
1.8
8
A




11
12.1
1.1
2.1
9
A




12
7.2
2.1
1.7
5
A




13
6.0
1.1
1.8
4
A




14
7.1
1.1
1.7
5
A




15
8.3
1.1
1.8
7
A




16
7.0
2.2
1.7
5
A




17
7.4
1.3
1.7
5
A




18
8.1
1.4
1.8
7
A




19
11.5
2.3
2.0
8
A




20
13.2
1.2
1.9
8
A




21
7.2
1.2
1.8
4
A




22
8.0
2.1
1.8
8
A




23
8.8
1.6
1.9
4
A




24
15.3
1.0
2.2
2
A




25
7.0
2.1
1.9
5
A




26
7.5
1.1
1.9
3
A




27
7.2
1.2
1.8
4
A




















TABLE 2-2










Hot-Rolling





Condition
























rolling pass













number with







rolling
rolling


Rough






total
pass
reduction
Rough
total
rolling





heating
rolling
number
of 30% or
Rolling
rolling
reduction/
Finish
Coiling





temper-
reduction
in
more in
End
reduction
finish
Temper-
Temper-




Steel
ature
in Rough
Rough
Rough
temper-
in finish
rolling
ature
ature



No.
No.
° C.
rolling %
rolling
rolling
ature° C.
rolling %
reduction
° C.
° C.





Comparative
28
B1
1120
89
7
5
1020
82
1.1
830
640


Example
29
B2
1120
87
7
5
1050
80
1.1
850
600



30
B3
1160
90
7
5
1050
82
1.1
820
580



31
B4
1160
89
7
6
1060
78
1.1
750
550



32
B5
1160
89
7
6
1010
82
1.1
800
630



33
B6
1120
89
7
5
1010
80
1.1
840
640



34
B7
1200
88
5
3
1020
82
1.1
830
600



35
B8
1120
89
7
5
1030
80
1.1
830
640



36
B9
1120
93
7
5
1020
78
1.2
850
600



37
B10
1160
88
7
5
1050
82
1.1
820
580



38
B11
1160
89
7
6
1010
70
1.3
750
550



39
B12
1160
92
7
5
1050
82
1.1
820
580



40
B13
1200
85
5
3
1010
80
1.1
850
610



41
B14
1200
89
5
3
1030
82
1.1
830
600



42
B15
1120
89
7
5
1060
78
1.1
830
640



43
B16
1120
90
7
5
1010
82
1.1
850
600



44
B17
1200
89
5
3
1030
82
1.1
830
600



45
B18
1120
91
7
5
1020
80
1.1
830
640



46
B19
1120
93
7
5
1030
82
1.1
850
600



47
B20
1120
88
7
5
1060
78
1.1
850
600



48
B21
1120
89
7
5
1050
82
1.1
830
640

















Intermediate
Final




Intermediate
Annealing
Annealing













Rolling
Annealing

Annealing


















Roll

Temper-
(111)Orient-
Grain
Temper-
Grain




Diameter
Rolling
ature
ation
size
ature
size



No.
mm
Reduction %
° C.
Intensity
number
° C.
number





Comparative
28
500
44
850
3.2
7.1
900
7.5


Example
29
500
44
870
4.2
7.5
910
6.5



30
500
55
870
3.1
7.7
900
6.1



31
500
55
850
7.2
6.5
890
5.6



32
450
46
830
5.4
7.4
900
5.7



33
450
46
835
3.3
6.3
920
6.2



34
400
44
850
6.1
6.8
925
6.0



35
500
44
850
3.2
7.2
900
7.2



36
500
44
870
4.1
7.5
910
6.5



37
500
55
870
3.2
7.5
900
5.2



38
500
55
850
7.1
8.1
890
7.5



39
500
55
870
2.1
5.5
900
5.4



40
400
44
850
3.0
7.2
940
7.0



41
400
44
835
2.3
6.5
900
7.0



42
500
44
850
1.0
6.2
910
6.5



43
500
44
850
3.2
6.1
900
5.2



44
400
44
870
4.1
6.3
900
7.0



45
500
44
870
2.3
6.5
910
4.5



46
500
44
835
3.1
6.0
900
5.9



47
500
44
850
2.0
4.5
900
4.8



48
500
44
850
2.1
6.5
910
4.5
















Characteristics of





Product Sheet





















Result





(111)Orient-
(411)Orient-

Ridging
of Pipe





ation
ation
Average
Height
Expansion




No.
Intensity
Intensity
r-value
μm
Test







Comparative
28
4.0*
1.1
1.4*
4
X



Example
29
3.1*
1.2
1.2*
25*
X




30
3.0*
5.4*
1.0*
20*
X




31
6.0
4.3*
1.5*
23*
X




32
7.4
4.3*
1.4*
5
X




33
6.0
3.4*
1.6*
5
X




34
2.0*
1.1
1.0*
6
X




35
4.3*
4.3*
1.0*
8
X




36
3.0*
4.3*
0.8*
12*
X




37
3.0*
4.2*
0.8*
21*
X




38
6.1
4.2*
1.2*
4
X




39
4.0*
1.1
1.3*
25*
X




40
10.1
7.0*
0.8*
20*
X




41
2.1*
4.0*
1.1*
20*
X




42
3.3*
2.2
1.2*
18*
X




43
3.0*
1.3
1.2*
6
X




44
2.3*
1.2
1.1*
8
X




45
2.1*
1.0
0.9*
10*
X




46
1.0*
1.1
0.7*
5
X




47
2.0*
2.0
0.8*
10*
X




48
2.1*
1.3
0.9*
10*
X







*Out of the scope of the invention
















TABLE 2-3










Hot-Rolling





Condition
























rolling pass













number with







rolling
rolling
Rough

Rough






total
pass
reduction
Rolling
total
rolling





heating
rolling
number
of 30% or
End
rolling
reduction/
Finish
Coiling





temper-
reduction
in
more in
temper-
reduction
finish
Temper-
Temper-




Steel
ature
in Rough
Rough
Rough
ature
in finish
rolling
ature
ature



No.
No.
° C.
rolling %
rolling
rolling
° C.
rolling %
reduction
° C.
° C.





Comparative
49
B22
1120
92
7
5
1020
80
1.2
850
600


Example
50
B23
1160
85
7
5
1060
80
1.1
820
580



51
B24
1200
89
5
3
1010
80
1.1
830
600



52
B25
1120
89
7
5
1010
78
1.1
830
640



53
A1
 1250*
90
7
5
1020
82
1.1
830
630



54
A1
 1050*
89
7
5
1020
80
1.1
850
620



55
A1
1120
85
7
 4*
1020
95
0.9
770
580



56
A1
1120
89
7
 4*
1020
90
1.0
800
590



57
A1
1160
90
7
 1*
1020
82
1.1
800
630



58
A1
1160
89
7
 4*
1020
80
1.1
830
640



59
A1
1120
91
7
5
1020
82
1.1
 940*
650



60
A1
1120
93
7
5
1020
80
1.2
820
 750*



61
A1
1160
88
5
4
1020
78
1.1
800
550



62
A1
1120
89
7
5
1020
82
1.1
840
630



63
A1
1200
92
7
6
1020
80
1.2
830
640



64
A1
1120
89
7
6
1020
82
1.1
850
600



65
A1
1120
92
7
5
1020
78
1.2
830
590



66
A1
1160
85
7
5
1020
80
1.1
850
630



67
A1
1120
89
7
5
 980*
82
1.1
830
640

















Intermediate
Final




Intermediate
Annealing
Annealing













Rolling
Annealing

Annealing


















Roll

Temper-
(111)Orient-
Grain
Temper-
Grain




Diameter
Rolling
ature
ation
size
ature
size



No.
mm
Reduction %
° C.
Intensity
number
° C.
number





Comparative
49
500
44
870
3.0
6.0
900
5.9


Example
50
500
55
870
2.3
4.7
900
4.8



51
400
44
835
1.0
6.5
900
7.0



52
500
44
850
1.1
6.2
910
6.5



53
500
44
850
3.4
7.7
900
7.1



54
500
44
850
6.2
7.3
900
6.5



55
500
50
870
5.4
6.9
900
5.8



56
500
50
870
4.3
8.5
910
7.3



57
450
55
840
6.1
7.5
890
7.7



58
450
55
840
7.2
7.5
920
7.2



59
400
55
830
5.2
7.1
890
6.5



60
400
55
850
3.1
7.3
900
5.4



61
 100*
44
850
4.0
7.9
920
5.8



62
500
 35*
850
8.0
7.8
925
6.3



63
500
55
 900*
2.0
5.5
940
6.2



64
450
46
 770*
1.1
4.8
900
7.5



65
500
44
850
3.1
7.5
 960*
5  



66
500
50
850
3.0
8.5
 800*
non-










recrys-










tallized



67
500
44
850
2.6
7.0
900
7.0
















Characteristics of





Product Sheet





















Result





(111)Orient-
(411)Orient-

Ridging
of Pipe





ation
ation
Average
Height
Expansion




No.
Intensity
Intensity
r-value
μm
Test







Comparative
49
1.2*
1.1
0.7*
5
X



Example
50
2.3*
2.1
0.8*
10*
X




51
2.0*
4.1*
0.9*
21*
X




52
3.0*
2.1
1.1*
19*
X




53
4.4*
1.1
1.5*
5
X




54
6.1
4.0*
1.2*
13*
X




55
6.2
4.0*
1.5*
12*
X




56
4.0*
4.0*
1.4*
21*
X




57
3.0*
1.1
1.1*
20*
X




58
3.0*
1.2
1.1*
20*
X




59
6.1
5.2*
1.4*
18*
X




60
7.3
4.1*
1.6*
25*
X




61
3.0*
2.2
1.4*
10*
X




62
4.0*
1.1
1.2*
5
X




63
7.2
5.1*
1.4*
4
X




64
4.1*
1.1
1.2*
25*
X




65
10.1
4.0*
1.7
20*
X




66
2.0*
2.1
1.1*
23*
X




67
5.5
3.3*
1.6*
11*
X







*Out of the scope of the invention






It is clear that the steel according to the above exemplary embodiment exhibits a high r-value and low ridging height and is excellent in pressing formability. Tables 2-1 to 2-3 show the results of pipe expansion test of an ERW steel pipe made of the steel sheet. The pipe expansion test was performed using a 60 degrees cone, where an end of the pipe is expanded to a double of a diameter of the non-expanded pipe (2D pipe expansion). When the pipe is not cracked, the test result is evaluated as A. When the pipe is cracked, the test results is evaluated as X. The results show that the steel pipes of the first exemplary embodiment have excellent formability.


Examples for the above-described second exemplary embodiment will be described below.


Steels of compositions shown in Tables 3-1 and 3-2 were melted and cast into a slab. After the slab was subjected to hot rolling until the thickness of the slab became 5 mm thick, the steels were subjected to hot rolling, (without applying the annealing of hot-rolled sheet: annealing of hot-rolled sheet was applied in some of Comparative Examples), intermediate cold rolling, intermediate annealing, finish cold rolling and finish annealing to obtain product sheets having various thicknesses. The steels were manufactured under the conditions shown in Tables 4-1 to 4-3.


Herein, in order to measure the texture, (200), (110) and (211) pole figures of the sheet-thickness central area (exposing the central area by a combination of mechanical polishing and electropolishing) were obtained using an X-ray diffractometer (manufactured by Rigaku Corporation) and Mo-Kα ray to obtain an ODF (Orientation Distribution Function) based on the dot diagrams using a spherical harmonics method. Based on the measurement results, {111}<110>-orientation intensity and {311}<136>-orientation intensity were calculated.


In order to evaluate the average r-value (rm), JIS13B tensile test pieces were taken from a product sheet and the average r-value was calculated using formulae (3) and (4) below after applying 14.4% distortions in a rolling direction, a 45-degree direction with respect to the rolling direction and a direction perpendicular to the rolling direction.






r=ln(W0/W)/ln(t0/t)  (3)


In the formula (3), W0 represents a sheet width before applying a tensile force, W represents a sheet width after applying the tensile force, t0 represents a sheet thickness before applying the tensile force and t represents a sheet thickness after applying the tensile force.






r
m=(r0+2r45+r90)/4  (4)


In the formula (4), rm represents an average r-value, r0 represents an r-value in the rolling direction, r45 represents an r-value in the 45-degree direction with respect to the rolling direction and r90 represents an r-value in the direction perpendicular to the rolling direction.


Tables 4-1 to 4-3 show the results of pipe expansion test of an ERW steel pipe made of the steel sheet. The pipe expansion test was performed using a 60 degrees cone, where an end of the pipe is expanded to a double of a diameter of the non-expanded pipe (2D pipe expansion). When the pipe is not cracked, the test result is evaluated as A. When the pipe is cracked, the test results is evaluated as X.











TABLE 3-1







Steel
Composition (mass %)



















No.
C
N
Si
Mn
P
S
Cr
Ti
Nb
B
Al






















Exemplary
1
0.004
0.007
0.42
0.32
0.02
0.0005
10.7
0.16


0.05


Embodiment
2
0.005
0.003
0.45
1.41
0.01
0.0008
10.9
0.19

0.0002
0.05



3
0.005
0.004
0.42
0.66
0.02
0.0004
11.3
0.21


0.07



4
0.005
0.004
0.32
0.66
0.03
0.0004
10.9
0.21

0.002 
0.07



5
0.012
0.002
0.41
1.43
0.02
0.0009
19.0
0.12
0.28

0.06



6
0.012
0.002
0.41
1.43
0.02
0.0009
19.0

0.32

0.06



7
0.004
0.004
0.28
0.67
0.02
0.0009
11.0
0.19


0.06



8
0.017
0.002
0.41
0.65
0.03
0.0009
14.2
0.19


0.08



9
0.007
0.004
0.43
0.27
0.02
0.0010
11.0
0.22


0.21



10
0.009
0.003
0.44
0.64
0.03
0.0013
13.1
0.20


0.12



11
0.011
0.005
0.42
0.57
0.04
0.0010
11.0
0.22


0.06



12
0.005
0.009
0.45
0.37
0.02
0.0008
14.3
0.15


0.07



13
0.004
0.003
0.43
0.35
0.01
0.0013
25.1
0.29


0.13



14
0.006
0.005
0.66
2.52
0.03
0.0080
27.0
0.14
0.45

0.09



15
0.011
0.011
0.80
0.33
0.02
0.0032
18.1
0.14


0.09



16
0.011
0.026
0.62
1.57
0.02
0.0017
11.5
0.24
0.44

0.09



17
0.025
0.015
0.62
0.64
0.03
0.0013
18.1
0.14


0.09



18
0.004
0.008
0.41
0.31
0.03
0.0005
10.7
0.17


0.05



19
0.005
0.007
0.43
0.33
0.03
0.0005
10.8
0.15


0.05



20
0.004
0.007
0.41
0.30
0.03
0.0005
10.6
0.19


0.05



21
0.005
0.007
0.42
0.21
0.03
0.0005
10.9
0.19


0.05













Steel
Composition (mass %)















No.
Ni
Mo
Cu
V
Mg
Others




















Exemplary
1









Embodiment
2










3
0.16









4










5










6

1.50








7
0.35

0.78







8



0.19
0.0005





9





Sn: 0.1




10





Zr: 0.03




11





W: 1.5




12





Co: 0.05




13





Sb: 0.45




14





REM: 0.11




15



0.7 
0.0022
W: 2.6




16
0.7 




Co: 0.23




17


2.6 







18





Ca: 0.0010




19





Ga: 0.0020




20





Hf: 0.005




21





Ta: 0.006


















TABLE 3-2







Steel
Composition (mass %)


















No.
C
N
Si
Mn
P
S
Cr
Ti
Nb
B
Al






















Comparative
22
0.004
0.007
0.42
0.32
0.02
0.0006
10.7
0.16

*0.0101 
0.05


Example
23
0.007
0.005
0.46
0.27
0.03
0.0005
10.8
0.17


0.06



24
0.011
0.007
0.43
0.32
0.02
0.0012
14.2
0.16
0.32

0.06



25
0.004
0.003
0.42
0.32
0.02
0.0005
10.9
0.12


0.06



26
0.005
0.003
0.41
0.70
0.01
0.0008
10.7
0.16


0.06



27
0.004
0.007
0.54
0.51
0.04
0.0010
17.3
0.15


0.05



28
0.021
0.003
0.42
0.32
0.02
0.0013
11.3

0.38

0.07



29
0.005
0.004
0.98
0.27
0.02
0.0010
13.6
0.18


0.05



30
0.007
0.007
0.59
0.50
0.03
0.0020
14.1
0.21


0.12



31
0.004
0.007
0.42
0.38
0.02
0.0011
13.4
0.16


0.08



32
0.005
0.004
0.42
0.32
0.03
0.0014
11.4
*— 
*— 

0.07



33
0.007
0.005
*2.17
0.66
0.02
0.0020
14.1
0.22
0.48

0.13



34
0.004
0.006
0.61
0.53
0.04
0.0011
21.4
*0.19 
*0.56 

0.11



35
0.005
0.004
0.46
*3.52
0.03
0.0006
13.4
0.21


0.06



36
*0.031
0.021
0.72
0.65
0.03
0.0011
11.1
0.16
0.21

0.08



37
0.025
*0.033
0.68
0.51
*0.05
0.0013
10.2
0.15
0.22

0.06



38
0.010
0.008
0.28
0.26
0.02
0.0018
19.1

*0.82 
0.0003
0.05



39
0.009
0.010
0.68
0.12
0.04
0.0011
17.2
*1.21 

0.0002
0.06













Steel
Composition (mass %)















No.
Ni
Mo
Cu
V
Mg
Others




















Comparative
22









Example
23
*1.5 









24

*2.5








25


*3.1 







26



*1.23






27




*0.0145





28





Sn: *0.51




29





Zr: *0.51




30





W: *3.1




31





Co: *0.48




32










33
0.1

1.5







34


0.2







35
 0.35









36










37










38

 1.1








39













*Out of the scope of the invention
















TABLE 4-1









Hot-













Hot-Rolling Condition
Rolling
Intermediate
Intermediate



















Finish Rolling

Annealing
Cold
Annealing





Heating
Temperature
Coiling
Annealing
Rolling
Annealing















Temper-
(° C.)
Temper-
Temper-
Roll

Temper-




















Steel
ature


Differ-
ature
ature
Diameter
Rolling
ature



No
No.
° C.
Start
End
ence
° C.
° C.
mm
Reduction %
° C.





Exemplary
A1
1
1135
960
810
150
630

500
44
825


Embodiment
A2
1
1135
960
810
150
630

500
44
850



A3
1
1135
960
810
150
630

500
44
875



A4
1
1135
960
810
150
630

500
44
850



A5
1
1135
960
810
150
630

500
44
850



A6
1
1135
960
810
150
630

500
44
850



A7
1
1135
960
810
150
630

105
44
850



A8
2
1135
960
840
120
640

500
44
850



A9
3
1120
950
820
130
620

500
45
875



A10
4
1135
960
840
120
630

500
44
875



A11
5
1135
960
840
120
630

500
44
875



A12
6
1160
980
880
100
650

500
51
880



A13
7
1160
980
880
100
650

500
46
880



A14
8
1160
980
880
100
650

500
52
880



A15
9
1135
960
840
120
630

500
44
845



A16
10
1120
950
830
120
620

500
50
845



A17
11
1135
960
840
120
630

500
50
875



A18
12
1140
970
890
80
660

500
50
875



A19
13
1180
980
880
100
650

100
44
825



A20
14
1180
980
880
100
650

500
51
850



A21
15
1180
980
880
100
680

105
44
850



A22
16
1190
990
880
110
710

500
51
875



A23
17
1170
980
870
110
650

500
51
850



A24
18
1135
960
810
150
630

500
44
825



A25
19
1135
960
810
150
630

500
44
825



A26
20
1135
960
810
150
630

500
44
825



A27
21
1135
960
810
150
630

500
44
825



















Final





Intermediate
Finish
Annealing
Orientation













Annealing
Cold rolling
Annealing

Intensity


















(111)Orient-
Grain
Roll

Temper-
Grain
(111)Orient-
(311)Orient-




ation
size
Diameter
Rolling
ature
size
ation
ation



No
Intensity
number
mm
Reduction %
° C.
number
Intensity
Intensity





Exemplary
A1
5

100
61
900
8
5.2
2.0


Embodiment
A2
5

100
61
900
8
6.3
2.0



A3
5
6
100
60
900
8
6.6
2.1



A4
5

100
71
900
8
9.1
2.1



A5
5

105
82
900
8
16.3
2.2



A6
5

105
89
900
9
23.6
2.3



A7
4
7
400
62
925
7
5.3
2.0



A8
5
6
80
60
900
8
6.2
2.1



A9
6
6
80
60
900
8
6.0
2.0



A10
6
7
80
60
950
7
5.0
1.4



A11
6
7
100
60
950
7
6.3
2.0



A12
5
7
80
70
900
8
6.9
2.1



A13
5
7
80
63
900
8
7.1
2.3



A14
5

80
71
900
8
9.0
2.1



A15
5
7
80
64
900
8
6.7
2.5



A16
5
7
100
64
900
8
8.3
2.2



A17
5
7
100
64
925
8
9.2
2.0



A18
5
6
100
64
925
8
8.1
2.0



A19
5

400
70
900
8
6.7
2.2



A20
5
7
80
70
900
8
6.0
2.6



A21
5
7
400
82
900
8
10.3
2.8



A22
6

400
60
900
8
7.4
2.4



A23
5
7
105
82
900
8
12.1
2.6



A24
5

100
61
900
8
5.3
2.0



A25
5

100
61
900
8
5.2
2.1



A26
5

100
61
900
8
5.1
2.1



A27
5

100
61
900
8
5.1
2.1

















Characteristics






of Product Sheet
Result

















Sheet

of Pipe





Average
Thickness

Expansion




No
r-value rm
t mm
“−t + 3”
Test







Exemplary
A1
1.8
1.2
1.8
A



Embodiment
A2
1.9
1.2
1.8
A




A3
1.9
1.2
1.8
A




A4
2.3
0.8
2.2
A




A5
2.6
0.5
2.5
A




A6
3.1
0.3
2.7
A




A7
1.8
1.2
1.8
A




A8
2.3
1.2
1.8
A




A9
1.8
1.2
1.8
A




A10
2.3
1.2
1.8
A




A11
1.9
1.2
1.8
A




A12
2.3
0.8
2.2
A




A13
2.5
1.0
2.0
A




A14
2.3
0.8
2.2
A




A15
1.9
1.0
2.0
A




A16
2.1
1.0
2.0
A




A17
2.2
1.0
2.0
A




A18
2.3
1.0
2.0
A




A19
2.2
0.8
2.2
A




A20
1.9
1.2
1.8
A




A21
2.7
0.5
2.5
A




A22
2.0
1.2
1.8
A




A23
2.8
0.5
2.5
A




A24
1.7
1.2
1.8
A




A25
1.7
1.2
1.8
A




A26
1.7
1.2
1.8
A




A27
1.7
1.2
1.8
A




















TABLE 4-2









Hot-












Rolling

Intermediate












Hot-Rolling Condition
Annealing
Intermediate
Annealing














Heating
Finish Rolling
Coiling
Annealing
Cold Rolling
Annealing















Temper-
Temperature (° C.)
Temper-
Temper-
Roll

Temper-




















Steel
ature


Differ-
ature
ature
Diameter
Rolling
ature



No
No.
° C.
Start
End
ence
° C.
° C.
mm
Reduction %
° C.





Comparative
B1
1
1135
960
810
150
630
 *950
*105 
44
*1000 


Example
B2
1
1135
960
810
150
630
*1000
400
44
875



B3
1
1135
960
810
150
630

*—
*—
*—



B4
1
1135
960
810
150
630

500
44
*750 



B5
1
1135
960
810
150
630

500
44
*900 



B6
1
1135
960
810
150
630

500
44
*1000 



B7
1
1135
990
810
180
650

500
44
850



B8
12
1140
970
890
 80
660

*100 
50
875



B9
12
*1050 
*880 
*790 
 90
*580 

400
50
850



B10
3
*1080 
900
*770 
130
600

500
45
875



B11
3
*1250 
1100 
880
*220 
720

500
45
875



B12
3
1200
1060 
840
*220 
670

500
45
875



















Final





Intermediate
Finish
Annealing
Orientation













Annealing
Cold rolling
Annealing

Intensity


















(111)Orient-
Grain
Roll

Temper-
Grain
(111)Orient-
(311)Orient-




ation
size
Diameter
Rolling
ature
size
ation
ation



No
Intensity
number
mm
Reduction %
° C.
number
Intensity
Intensity





Comparative
B1
4
5
*100 
61
900
6
*3.3 
 2.1


Example
B2
5
5
100
61
900
8
*3.8 
 2.3



B3


400
76
900
9
9.0
*4.2



B4
6

100
61
900
8
4.1
*3.4



B5
4
5
100
61
900
7
*3.3 
 2.0



B6
6
5
100
61
900
6
*2.4 
 1.0



B7
5

 80
61
*825 

4.3
*3.2



B8
5
6
*60
64
925
7
6.5
*4.1



B9
4

 80
64
900
8
6.1
*3.0



B10
4

 80
60
900
8
5.1
*3.4



B11
3

 80
60
900
8
*3.9 
*3.1



B12
4

 80
60
900
8
5.5
*3.1

















Characteristics






of Product Sheet
Result

















Sheet

of Pipe





Average
Thickness

Expansion




No
r-value rm
t mm
“−t + 3”
Test







Comparative
B1
1.4
1.2
1.8
X



Example
B2
1.7
1.2
1.8
X




B3
1.7
1.2
1.8
X




B4
1.5
1.2
1.8
X




B5
1.6
1.2
1.8
X




B6
1.6
1.2
1.8
X




B7
1.4
1.2
1.8
X




B8
1.8
1.0
2.0
X




B9
1.8
1.0
2.0
X




B10
1.6
1.2
1.8
X




B11
1.5
1.2
1.8
X




B12
1.6
1.2
1.8
X







*Out of the scope of the invention

















TABLE 4-3









Hot-Rolling

Intermediate












Hot-Rolling Condition
Annealing
Intermediate
Annealing














Heating
Finish Rolling
Coiling
Annealing
Cold Rolling
Annealing















Temper-
Temperature (° C.)
Temper-
Temper-
Roll

Temper-




















Steel
ature


Differ-
ature
ature
Diameter
Rolling
ature



No
No.
° C.
Start
End
ence
° C.
° C.
mm
Reduction %
° C.





Comparative
B13
*22
1135
950
830
120
630

500
50
850


Example
B14
*23
1160
990
840
150
630

500
44
875



B15
*24
1160
980
840
140
630

500
44
850



B16
*25
1135
990
870
120
650

400
46
880



B17
*26
1135
990
880
110
650

500
44
880



B18
*27
1135
960
840
120
630

*105 
44
880



B19
*28
1180
970
850
120
640
*1050
400
45
875



B20
*29
1170
960
850
110
640

500
53
875



B21
*30
1135
960
830
130
630

400
46
825



B22
*31
1140
960
830
130
630

400
44
825



B23
*32
1135
960
830
130
630

500
44
850



B24
*33
1200
1050
920
130
780

400
44
850



B25
*34
1200
1050
930
120
790

400
63
875



B26
*35
1200
1050
930
120
790

400
63
875



B27
*36
1160
980
880
100
650

400
51
880



B28
*37
1160
990
880
110
660

400
52
880



B29
*38
1180
1020
940
80
790

400
44
880



B30
*39
1180
1010
920
90
790

500
44
880



















Final





Intermediate
Finish
Annealing
Orientation













Annealing
Cold rolling
Annealing

Intensity


















(111)Orient-
Grain
Roll

Temper-
Grain
(111)Orient-
(311)Orient-




ation
size
Diameter
Rolling
ature
size
ation
ation



No
Intensity
number
mm
Reduction %
° C.
number
Intensity
Intensity





Comparative
B13
4

100 
82
950
5
5.8
*5.5


Example
B14
5
6
100 
82
925
5
4.9
*6.7



B15
5
7
80
82
950
5
6.2
*4.0



B16
5
6
100 
61
900
6
*3.4
2.4



B17
4
6
80
61
900
6
4.0
*3.5



B18
5
5
*80 
64
950
5
5.0
*4.1



B19
5

80
64
925
6
4.3
*5.0



B20
5
6
80
64
900
5
4.7
*3.2



B21
5

80
82
900
6
5.1
*4.3



B22
4

80
82
900
5
6.6
*5.6



B23
3

100 
61
900
4
4.1
*3.2



B24
5

105 
*44 
*1050 
5
8.2
*5.5



B25
6

105 
63
*1000 
6
11.1
*6.1



B26
6

105 
63
950
7
18.3
*11.2



B27
5
7
80
70
975
7
5.1
*4.7



B28
4

80
70
975
7
5.3
*4.3



B29
6

60
60
*1100 
5
6.0
*4.1



B30
5

80
61
975
7
5.3
*4.6

















Characteristics






of Product Sheet
Result

















Sheet

of Pipe





Average
Thickness

Expansion




No
r-value rm
t mm
“−t + 3”
Test







Comparative
B13
1.4
0.8
2.2
X



Example
B14
1.6
1.0
2.0
X




B15
1.8
0.8
2.2
X




B16
1.5
1.2
1.8
X




B17
1.1
1.2
1.8
X




B18
1.3
1.0
2.0
X




B19
1.4
1.0
2.0
X




B20
1.2
1.0
2.0
X




B21
1.4
0.8
2.2
X




B22
1.7
0.8
2.2
X




B23
1.4
1.2
1.8
X




B24
1.5
0.8
2.2
X




B25
1.7
0.3
2.7
X




B26
1.9
0.3
2.7
X




B27
1.5
1.0
2.0
X




B28
1.6
1.0
2.0
X




B29
1.3
1.2
1.8
X




B30
1.4
1.2
1.8
X







*Out of the scope of the invention






As is clear from Tables 3-1, 3-2 and 4-1 to 4-3, the steel of the exemplary embodiments of the invention satisfy a relationship between the average r-value and the sheet thickness of rm≥−1.0t+3.0, showing excellent press formability. Further, all of the results of 2D pipe expansion test are “A”, which shows that the steel pipe of the exemplary embodiments of the invention have excellent formability.

Claims
  • 1. A ferritic stainless steel sheet with excellent formability, comprising: 0.03 mass % or less of C;0.03 mass % or less of N;1.0 mass % or less of Si;3.0 mass % or less of Mn;0.04 mass % or less of P;0.0003 to 0.0100 mass % of S;10 to 30 mass % of Cr,0.300 mass % or less of Al;one or both of 0.05 to 0.30 mass % of Ti and 0.01 to 0.50 mass % of Nb, a sum of Ti and Nb being in a range from smaller one of 8(C+N) and 0.05 to 0.75 mass %and a residual amount of Fe and inevitable impurities, wherein{111}<110>-orientation intensity is 4.0 or more and {311}<136>-orientation intensity is less than 3.0.
  • 2. The ferritic stainless steel sheet with excellent formability according to claim 1, further comprising one or more of elements selected from the group consisting of: 0.0002 to 0.0030 mass % of B, 0.1 to 1.0 mass % of Ni, 0.1 to 2.0 mass % of Mo, 0.1 to 3.0 mass % of Cu, 0.05 to 1.00 mass % of V, 0.0002 to 0.0030 mass % of Ca, 0.0002 to 0.0030 mass % of Mg, 0.005 to 0.500 mass % of Sn, 0.01 to 0.30 mass % of Zr, 0.01 to 3.0 mass % of W, 0.01 to 0.30 mass % of Co, 0.005 to 0.500 mass % of Sb, 0.001 to 0.200 mass % of REM, 0.0002 to 0.3 mass % of Ga, 0.001 to 1.0 mass % of Ta, and 0.001 to 1.0 mass % of Hf.
  • 3. The ferritic stainless steel sheet with excellent formability according to claim 1, wherein a grain size number is 6 or more.
  • 4. The ferritic stainless steel sheet with excellent formability according to claim 1, wherein, when a plate thickness is represented by t (mm) and an average r-value is represented by rm, rm satisfies a relationship of rm≥−1.0t+3.0.
  • 5. The ferritic stainless steel sheet with excellent formability according to claim 1, wherein the ferritic stainless steel pipe is suitable for use in an automobile component or a motorcycle component.
  • 6. The ferritic stainless steel sheet with excellent formability according to claim 1, wherein the ferritic stainless steel pipe is suitable for use in an automobile exhaust pipe, fuel tank or a fuel pipe.
  • 7. A ferritic stainless steel pipe with excellent formability, wherein the ferritic stainless steel pipe is made from a material in a form of the stainless steel sheet according to claim 1.
  • 8. The ferritic stainless steel sheet with excellent formability according to claim 2, wherein a grain size number is 6 or more.
  • 9. The ferritic stainless steel sheet with excellent formability according to claim 2, wherein, when a plate thickness is represented by t (mm) and an average r-value is represented by rm, rm satisfies a relationship of rm≥−1.0t+3.0.
  • 10. The ferritic stainless steel sheet with excellent formability according to claim 2, wherein the ferritic stainless steel pipe is suitable for use in an automobile component or a motorcycle component.
  • 11. The ferritic stainless steel sheet with excellent formability according to claim 2, wherein the ferritic stainless steel pipe is suitable for use in an automobile exhaust pipe, fuel tank or a fuel pipe.
  • 12. A ferritic stainless steel pipe with excellent formability, wherein the ferritic stainless steel pipe is made from a material in a form of the stainless steel sheet according to claim 2.
  • 13. The ferritic stainless steel sheet with excellent formability according to claim 3, wherein, when a plate thickness is represented by t (mm) and an average r-value is represented by rm, rm satisfies a relationship of rm≥−1.0t+3.0.
  • 14. The ferritic stainless steel sheet with excellent formability according to claim 8, wherein, when a plate thickness is represented by t (mm) and an average r-value is represented by rm, rm satisfies a relationship of rm≥−1.0t+3.0.
Priority Claims (2)
Number Date Country Kind
2014-222202 Oct 2014 JP national
2014-236113 Nov 2014 JP national
CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a Divisional of copending application Ser. No. 15/521,465, filed on Apr. 24, 2017, which is the national stage entry of and claims priority under 35 U.S.C. § 371 of International Application No. PCT/JP2015/080268, filed on Oct. 27, 2015, and which claims the benefit under 35 U.S.C. § 119(a) to Japanese Patent Application No. JP 2014-222202, filed in Japan on Oct. 31, 2014, and Japanese Patent Application No. JP 2014-236113, filed in Japan on Nov. 21, 2014, all of which are hereby expressly incorporated by reference into the present application.

Divisions (1)
Number Date Country
Parent 15521465 Apr 2017 US
Child 17130634 US