High tensile cold rolled steel sheet and high tensile hot dip galvanized steel sheet having improved stretch flanging property and process for producing same

Abstract

A high tensile cold rolled steel sheet improved in stretch flanging property, containing 0.03% to 0.15% by weight of C, 0.05% or less by weight of Si, 0.5% to 1.2% by weight of Mn, 0.005% to 0.045% by weight of Nb, and 0.10% or less by weight of Al, the remainder being iron and unavoidable impurities, and the steel sheet having a uniform and fine recrystallized ferrite structure having a mean grain diameter of 20 .mu.m or less and an area fraction of 95% or more having improving ductility and a process for its preparation.

Description

BACKGROUND OF THE INVENTION

1. Field of the Invention

This invention relates to a cold rolled steel sheet and a hot dip galvanized steel sheet which have a tensile strength (hereinafter abbreviated as T.S.) of more than 40 kgf/mm.sup.2 and are improved in ductility, particularly, in stretch flanging property, and processes for producing same.

2. Description of the Related Art

There has been an increasing demand for high tensile cold rolled steel sheets having a T.S. of more than 40 kgf/mm.sup.2, e.g., in automobile industry, to enhance the safety and reduce weight for fuel economy, as well as for hot dip galvanized steel sheets using a high tensile cold rolled sheet to improve the rustproof property. Further, there is a demand for construction materials having a smaller thickness to reduce the cost, and also in this field, high tensile cold rolled steel sheets are greatly demanded.

In these applications, high tensile steel sheets are required to have satisfactory workability, such as in pressing.

To meet these requirements, a process for producing high Mn--Si steel as a material has been proposed, e.g., in Japanese Patent Disclosure No. 57-63634 and No. 56-13437. In this process, however, an increased tensile strength is achieved chiefly by solution hardening, and therefore, a large quantity of Si, which serves to increase the strength, must be admixed, thus posing problems in surface properties and effectiveness of phosphatizing and hot dipping.

As a process which does not rely upon the alloy composition, unlike the above process, a process utilizing a annealed recovery structure is proposed, e.g., in Japanese Patent Disclosure No. 60-33318. However, this process has problems, such as fluctuation in properties, low ductility, and large planar anisotropy, and although the cost is low, the process is not efficient enough to permit a mass production.

This invention relates to a high tensile cold rolled steel sheet and a high tensile hot dip galvanized steel sheet which have a T.S. of more than 40 kgf/mm.sup.2 and solves the problems associated with the prior art, and an object thereof is to provide a high tensile cold rolled steel sheet and a high tensile hot dip galvanized steel sheet, both satisfying the below-mentioned conditions and having an excellent stretch flanging property, and processes for producing same.

(1) Eliminates the need for the admixture of Si which deteriorates the surface properties and the effectiveness of hot dipping, and provides a low alloy system.

(2) Improves the ductility, in particular, the stretch flanging property

(3) Achieves stable properties with less planar anisotropy.

(4) Imposes no restrictions on particularly severe operating conditions.

SUMMARY OF THE INVENTION

To solve the above-described problems, the inventors comprehensively examined steels of various component systems and various producing conditions, focusing their attention on the properties and structures, and found that a remarkably excellent stretch flanging property can be obtained by reducing the percentage of the second phase e.g., pearlite, to obtain a recrystallized ferrite structure consisting of uniformly fine grains, and that such a desirable structure can be obtained mainly by optimizing the combination of steel composition, cold rolling condition, and annealing condition.

This invention is based on the above findings.

This invention provides a high tensile cold rolled steel sheet improved in stretch flanging property, which contains 0.03% to 0.15% by weight of C, 0.05% or less by weight of Si, 0.5% to 1.2% by weight of Mn, 0.005% to 0.045% by weight of Nb, and 0.10% or less by weight of Al, the remainder being iron and unavoidable impurities, and the steel sheet having a uniform and fine recrystallized ferrite structure having a mean grain diameter of 20 .mu.m or less and an area fraction of 95% or more.

According to this invention, there is also provided a process for producing a high tensile cold rolled steel sheet improved in stretch flanging property, which comprises the steps of: preparing, as a material, steel containing 0.03% to 0.15% by weight of C, 0.05% or less by weight of Si, 0.5% to 1.2% by weight of Mn, 0.005% to 0.045% by weight of Nb, and 0.10% or less by weight of Al, the remainder being iron and unavoidable impurities; subjecting the material to hot rolling; effecting cold rolling at a reduction rate in thickness of more than 50%; and effecting annealing in which the material is heated at a heating rate of 5.degree. C./sec or more and retained in a temperature range of 720.degree. to 780.degree. C. for 20 to 60 seconds in a continuous annealing line, and then cooling the material.

Further, the invention provides a high tensile hot dip galvanized steel sheet improved in stretch flanging property, which contains 0.03% to 0.15% by weight of C, 0.05% or less by weight of Si, 0.5% to 1.2% by weight of Mn, 0.005% to 0.045% by weight of Nb, and 0.10% or less by weight of Al, the remainder being iron and unavoidable impurities, and the steel sheet having a uniform and fine recrystallized ferrite structure having a mean grain diameter of 20 .mu.m or less and an area fraction of 95% or more.

Furthermore, a process is provided for producing a high tensile hot dip galvanized steel sheet improved in stretch flanging property, which comprises the steps of: preparing, as a material, steel containing 0.03% to 0.15% by weight of C, 0.05% or less by weight of Si, 0.5% to 1.2% by weight of Mn, 0.005% to 0.045% by weight of Nb, and 0.10% or less by weight of Al, the remainder being iron and unavoidable impurities; subjecting the material to hot rolling; effecting cold rolling at a reduction rate in thickness of more than 50%; and effecting annealing in which the material is heated at a heating rate of 5.degree. C./sec or more and retained in a temperature range of 720.degree. to 780.degree. C. for 20 to 60 seconds in an in-line anneal type continuous hot dip galvanizing line, and then cooling and hot-dipping the material.

Moreover, the invention provides a process for producing a high tensile hot dip galvanized steel sheet improved in stretch flanging property, which comprises the steps of: preparing, as a material, steel containing 0.03% to 0.15% by weight of C, 0.05% or less by weight of Si, 0.5% to 1.2% by weight of Mn, 0.005% to 0.045% by weight of Nb, and 0.10% or less by weight of Al, the remainder being iron and unavoidable impurities; subjecting the material to hot rolling; effecting cold rolling at a reduction rate in thickness of more than 50%; and effecting annealing in which the material is heated at a heating rate of 5.degree. C./sec or more and retained in a temperature range of 720.degree. to 780.degree. C. for 20 to 60 seconds in an in-line anneal type continuous hot dip galvanizing line, and then cooling, galvanizing and galvannealing the material.

DETAILED DESCRIPTION OF THE INVENTION

First, the reason for defining the aforementioned ranges for the components of the steel according to this invention will be described.

C: 0.03% to 0.15%

C is most effective as a component for increasing the strength and is also a desirable component because it is inexpensive. However, if C is added in excess of 0.15%, the percentage of the second phase, e.g., pearlite, is significantly increased, and the ductility, in particular, the stretch flanging property, is extremely lowered. Moreover, the weldability is significantly lowered. On the other hand, with a C content smaller than 0.03%, a sufficiently high T.S. cannot be attained even if other elements are added. For this reason, C is added in the range of 0.03% to 0.15%.

Si: 0.05% or less

Si is effective for increasing the strength of steel and has a little influence on the deterioration of ductility, and thus is an element which may desirably be contained in a large quantity in consideration of mechanical properties. However, Si is at the same time an element which extremely deteriorates the surface properties due to scales and the effectiveness of hot dipping. Therefore, to obtain a fine appearance in the surface, the Si content must be 0.05% or less.

Mn: 0.5% to 1.2%

Mn is less effective in solution hardening than C, Si, or the like, and yet serves to increase the strength. Further, Mn has the property of restraining the pearlite from being produced excessively and coarsened and thus making the grains fine. To achieve these effects, more than 0.5% of Mn must be admixed. If, however, Mn is added in excess of 1.2%, its property of increasing the strength becomes saturated, and the stretch flanging property is lowered because the second phase becomes likely to distribute in the form of stratum, thus deteriorating the effectiveness of hot dipping. Accordingly, the range for the Mn content is set from 0.5% to 1.2%.

Nb: 0.005% to 0.045%

The addition of Nb and the control of the Nb content constitute one of important factors of this invention. According to this invention, the strength and the ductility, particularly the stretch flanging property, are improved by finally obtaining a very fine and uniform recrystallized ferrite structure due to the effect of Nb. These advantageous effects are supposedly attained because Nb is precipitated as carbo-nitride, but the cause is not known in detail. The advantages can be achieved only by adding more than 0.005% by weight of Nb, and the effects become saturated when Nb is added in excess of 0.045%, and thus excessive addition is not economical. Moreover, an excessive addition of Nb makes a stable production of steel difficult. Therefore, Nb must be added in the range of 0.005% to 0.045%.

Al: 0.10% or less

The addition of Al is indispensable because Al acts as a deoxidizer and serves to clean the steel, and to this end, Al is preferably added in an amount of 0.005% at least. If, however, Al is admixed in excess of 0.10%, the possibility of a surface defect being caused due to alumina cluster, etc., increases, and therefore, Al is added in an amount of 0.10% or less.

In addition to the aforementioned elements, this invention allows unavoidable impurities of N, O and S in amounts of 0.0050%, 0.0070% and 0.010%, respectively. Particularly, the stretch flanging properly can be remarkably increased by reducing the S content, and this effect is conspicuous in a T.S. range of as high as 45 kgf/mm.sup.2. Accordingly, the reduction of S becomes more effective in improving mechanical properties with increase in tensile strength.

Now, the reason for defining the crystal structure will be described.

As mentioned above, the object of this invention is to improve the ductility, in particular, the stretch flanging property.

An extremely excellent stretch flanging property can be obtained by reducing the percentage of the second phase, e.g., pearlite, and thereby increasing the percentage of the recrystallized ferrite to 95% or more, and by making the structure uniformly fine with a mean grain diameter of 20 .mu.m or less.

In this case, an increased percentage of the pearlite (particularly a coarse one) at which a flange crack may be caused is unfavorable, and non-uniformity and coarseness of the recrystallized ferrite structure similarly bring about a disadvantageous effect. Accordingly, the percentage of the recrystallized ferrite should be 95% or more and the mean grain diameter of the recrystallized ferrite should be 20 .mu.m or less.

Next, the conditions for production will be described.

An ordinary process may be employed for the producing steps from steelmaking to hot rolling, without any particular restrictions. Typical hot rolling conditions comprise a heating temperature of 1280.degree. to 1180.degree. C., a hot rolling finishing temperature of 900.degree. to 800.degree. C., and a coiling temperature of 650.degree. to 500.degree. C.

As for the cold rolling, generally, the reduction rate in thickness should desirably be high in order to obtain a fine recrystallized structure after annealing. In view of this, the lower limit for the reduction rate in thickness is set to 50%. If, however, the reduction rate in thickness is higher than required, an increase in the thickness of a hot rolled mother sheet is caused although it poses no particular problem in the properties.

With regard to a continuous annealing line for cold rolled steel sheets and an in-line anneal type continuous hot dip galvanizing line, the heating rate for annealing should desirably be high to obtain fine recrystallized grains, and to obtain uniform and fine recrystallized grains, the rate should be higher than 5.degree. C./sec, preferably 10.degree. C./sec or higher. The upper limit for the heating rate is about 100.degree. C./sec, from technical and economical viewpoints for the installation of heating equipment.

The annealing temperature is in the range of 720.degree. to 780.degree. C. If the temperature is lower than 720.degree. C., the recrystallization does not satisfactorily progress and the elongation and the stretch flanging property are lowered, thus making it impossible to obtain satisfactory properties. On the other hand, if the annealing temperature is higher than 780.degree. C., a softening disadvantageously occurs due to the grain growth. According to this invention, since Nb is added, an abnormal growth of recrystallized grains is suppressed by the carbo-nitride of Nb, and thus a uniform and fine recrystallized ferrite structure can be obtained over a relatively wide range of temperature.

The retention time for the annealing may substantially be zero, but more advantageously be 20 seconds or longer in view of the stability of properties. If the retention time is longer than 60 seconds, however, the properties may be deteriorated due to an abnormal growth of grains, and therefore, the retention time is set to 20 to 60 seconds.

As for the application of steel sheets according to this invention, since the yield stress of original sheets is the most important factor as the strength of articles after the forming, a yield ratio (Y.R.=YS/TS) of 70% or higher is sometimes required at the expense of formability. Therefore, to obtain such a high strength and a suitable yield ratio, a rapid cooling at 20.degree. C./sec or more is preferably effected in a temperature range of 700.degree. to 500.degree. C., in the cooling step subsequent to the annealing.

For the production of hot dip galvanized steel sheets, no particular restriction is imposed on the hot dip galvanizing step subsequent to the annealing, and an ordinary hot dip galvanizing process may be effected. In this invention, whether or not a galvanneal process is carried out does not arise any problem. The galvanneal process causes a little change in properties, and substantially identical properties are obtained regardless of whether or not the galvanneal process is effected.

EXAMPLE 1

Steel slabs of various compositions as shown in TABLE 1 were produced in accordance with a conventional procedure.

TABLE 1__________________________________________________________________________Steel Chemical Composition (%)type C Si Mn Nb Al N O S Remarks__________________________________________________________________________A 0.07 0.02 0.80 0.015 0.025 0.0020 0.0020 0.010 PresentB 0.12 0.02 0.55 0.010 0.055 0.0015 0.0025 0.008 inventionC 0.05 0.01 1.00 0.025 0.070 0.0035 0.0030 0.015D 0.02 0.02 0.80 0.010 0.035 0.0030 0.0020 0.012 ComparativeE 0.18 0.03 0.70 0.015 0.040 0.0025 0.0025 0.010 exampleF 0.07 0.02 0.30 0.025 0.025 0.0030 0.0020 0.010G 0.07 0.02 1.50 0.030 0.025 0.0040 0.0020 0.010H 0.07 0.10 1.00 0.020 0.030 0.0035 0.0030 0.005I 0.07 0.02 0.80 tr 0.025 0.0020 0.0020 0.010J 0.03 0.02 1.00 0.015 0.025 0.0020 0.0020 0.007 PresentK 0.15 0.03 0.50 0.015 0.030 0.0020 0.0020 0.008 inventionL 0.07 0.05 0.80 0.015 0.025 0.0020 0.0030 0.010M 0.05 0.01 1.20 0.025 0.040 0.0020 0.0025 0.007N 0.07 0.01 1.20 0.005 0.040 0.0015 0.0020 0.005O 0.07 0.01 0.80 0.045 0.025 0.0020 0.0015 0.007P 0.05 0.01 0.80 0.025 0.100 0.0030 0.0025 0.015__________________________________________________________________________

These steel slabs were subjected to hot rolling and cold rolling, under the conditions shown in TABLE 2, and then subjected to annealing in a continuous annealing line.

The steel sheets thus obtained were measured as to tensile properties, and side bend elongation property corresponding to stretch flanging property, the evaluation results being shown in TABLE 3. The tensile test was conducted by means of test pieces according to JIS 5. The side bend elongation property was evaluated in accordance with the method disclosed in Japanese Patent Publication No. 50-35438. Namely, rectangular test pieces of 40 mm wide and 170 mm long were prepared by shearing, such that a proper clearance is obtained, and the sheared faces were lightly finished with sandpaper before being subjected to test. The test pieces were subjected to in-plane deformation, and the elongation at the flange was measured immediately after the occurrence of a crack.

TABLE 2__________________________________________________________________________Slab Heating Rolling Finishing Coiling Reduction Heating Annealing Annealing CoolingTemperature Temperature Temperature Rate Rate Temperature Time Rate(.degree.C.) (.degree.C.) (.degree.C.) (%) .degree.C./s .degree.C. s .degree.C./s__________________________________________________________________________1280 900 600 50 10 740 20 25.intg. .intg. .intg.1220 780 520__________________________________________________________________________ TABLE 3__________________________________________________________________________ Side Bend Percentage of Mean Diameter ofSteel Y.S. T.S. El. Y.R. Elongation Second Phase Ferrite Grainstype kgf/mm.sup.2 kgf/mm.sup.2 % % % % .mu.m Remarks__________________________________________________________________________A 40 46 37 87 >60 3 14 PresentB 39 47 37 83 >60 4 14 inventionC 40 48 35 83 >60 2 12D 34 36 35 94 58 <1 26 ComparativeE 36 49 32 73 45 8 13 exampleF 42 43 25 98 45 3 25G 38 45 33 84 50 2 11H 39 43 30 91 48 2 12I 34 38 25 89 60 7 25J 39 47 37 83 >60 2 13 PresentK 39 49 37 80 >60 4 14 inventionL 39 48 37 81 >60 3 14M 41 50 35 82 >60 3 14N 41 47 37 87 >60 3 14O 42 50 35 84 >60 2 13P 42 49 35 86 >60 2 12__________________________________________________________________________

From TABLE 3, it will be understood that, as far as the contents of the elements fall within the respective ranges as defined in this invention, the steel sheets exhibit a high strength (T.S..gtoreq.40 kgf/mm.sup.2) and yet an excellent elongation (El.) and a side bend elongation (i.e., stretch flanging property). Moreover, a proper yield ratio is attained.

EXAMPLE 2

Using the steel A having the composition shown in TABLE 1, cold rolled steel sheets were produced under various conditions shown in TABLE 4, and the obtained sheets were examined in respect of tensile property and side bend elongation property, as in EXAMPLE 1.

TABLE 4__________________________________________________________________________ Reduction Annealing Annealing Rate Heating Rate Temperature Time Cooling RateNo. (%) (.degree.C./s) (.degree.C.) (s) (.degree.C./s) Remarks__________________________________________________________________________1 60 12 740 20 25 Present2 70 10 730 40 27 Invention3 45 10 740 20 30 Comparative4 60 3 740 40 22 Example5 60 20 760 20 32 Present invention6 60 12 700 40 28 Comparative7 60 12 800 40 30 example8 55 15 725 5 259 50 15 725 40 30 Present10 60 5 740 30 30 invention11 60 12 780 30 2512 55 10 720 40 2513 60 10 725 60 20__________________________________________________________________________ TABLE 5__________________________________________________________________________ Side Bend Percentage of Mean Diameter of Y.S. T.S. Y.R. El. Elongation Second Phase Ferrite GrainsNo. kgf/mm.sup.2 kgf/mm.sup.2 % % % % .mu.m__________________________________________________________________________1 39 47 83 38 >60 1.8 192 38 46 83 39 >60 1.7 173 66 71 93 9 20 2.1 244 38 40 95 38 >60 3.2 235 39 47 83 36 >60 2.1 196 55 65 85 12 28 1.8 partially non- recrystallized7 33 35 94 35 >60 3.1 228 49 56 87 19 30 3 partially non- recrystallized9 37 46 80 38 >60 2.2 1710 40 48 83 38 >60 1.7 1711 37 46 80 38 >60 1.5 1712 40 49 81 37 >60 2.2 1713 39 46 85 38 >60 1.5 17__________________________________________________________________________

As is clearly seen from TABLE 5, a satisfactory balance between strength and elongation and a satisfactory stretch flanging property can be obtained as far as the conditions for production according to this invention are fulfilled.

EXAMPLE 3

To examine the influence of the structure on the ductility and the stretch flanging property, specimens having the compositions shown in TABLE 6 were prepared under the conditions also shown in the same table, and the relationship between these properties was observed. The results are summarized in TABLE 7.

From TABLE 7 it follows that satisfactory properties can be obtained by properly controlling the percentage of the second phase, the mean diameter of recrystallized ferrite grains, and the area fraction of recrystallized ferrite. Among the Comparative Examples, Comparative Example E, has a T.S. lower than 40 kgf/mm.sup.2 and is excellent in elongation and side bend elongation property, but the mean grain diameter of ferrite is greater than 20 .mu.m, and therefore, its properties are not of satisfactory degree.

TABLE 6 (1)__________________________________________________________________________ ReductionSteel Chemical Composition (%) Ratetype C Si Mn Nb Al N O S (%)__________________________________________________________________________A' 0.05 0.01 0.80 0.015 0.025 0.0020 0.0020 0.008 60B' 0.07 0.01 0.80 0.015 0.015 0.0015 0.0020 0.005 70C' 0.05 0.01 1.20 0.070 0.045 0.0020 0.0030 0.008 55D' 0.18 0.01 0.90 0.015 0.035 0.0025 0.0030 0.010 55E' 0.18 0.01 1.00 0.040 0.035 0.0025 0.0040 0.010 55__________________________________________________________________________ TABLE 6 (2)______________________________________ Heating Annealing Annealing CoolingSteel Rate Temperature Time Ratetype (.degree.C./s) (.degree.C.) (s) (.degree.C./s) Remarks______________________________________A' 5 760 30 25 PresentB' 10 780 40 27 InventionC' 7 740 40 20 Compar-D' 7 750 40 25 ativeE' 7 750 40 20 Example______________________________________ TABLE 7__________________________________________________________________________ Area Yield of Percentage of Mean Diameter of Recrystallized Side BendSteel Second Phase Ferrite Grains Ferrite El. Elongationtype (%) (.mu.m) (%) % (%)__________________________________________________________________________A' Pearlite <2% 14 98 38 >60B' Same as Above 17 .about.100 38 >60C' Same as Above 18 90 30 31D' Pearlite 7% 14 93 32 36E' Pearlite 6% 23 94 33 >60__________________________________________________________________________

EXAMPLE 4

Steel slabs having the various compositions as shown in TABLE 1 mentioned above were prepared by a conventional procedure. These steel slabs were subjected to hot rolling and cold rolling under the conditions illustrated in TABLE 8, and then subjected to annealing in an in-line anneal type continuous hot dip galvanizing line. After this, a hot dipping step and a galvannealing step were effected to produce hot dip galvannealed steel sheets.

The steels sheets thus prepared were measured as to the tensile property and the side bend elongation property corresponding to the stretch flanging property, the measurement results being shown in TABLE 9. The tensile test was conducted by means of test pieces according to JIS 5, and the side bend elongation property was evaluated in the same manner as in EXAMPLE 1.

TABLE 8__________________________________________________________________________Slab Heating Rolling Finishing Coiling Reduction Heating Annealing Annealing CoolingTemperature Temperature Temperature Rate Rate Temperature Time Rate(.degree.C.) (.degree.C.) (.degree.C.) (%) .degree.C./s .degree.C. s .degree.C./s Others__________________________________________________________________________1280 900 600 50 10 740 20 5 Galvannealing.intg. .intg. .intg. .intg.1220 780 520 20__________________________________________________________________________ TABLE 9__________________________________________________________________________ Side Bend Percentage of Mean Diameter ofSteel Y.S. T.S. Y.R. El. Elongation Second Phase Ferrite Grainstype kgf/mm.sup.2 kgf/mm.sup.2 % % % Others % .mu.m Remarks__________________________________________________________________________A 39 45 87 38 >60 3 15 PresentB 38 46 83 37 >60 4 17 inventionC 40 48 83 34 >60 2 15D 33 35 94 35 57 <1 28 ComparativeE 35 48 73 33 44 9 13 exampleF 41 42 98 25 44 3 26G 38 45 84 34 51 2 12H 39 43 91 29 49 * 3 12I 34 38 89 24 59 7 25J 38 45 84 36 >60 5 12 PresentK 38 47 81 37 >60 4 15 inventionL 38 46 83 37 >60 4 15M 40 48 83 36 >60 4 13N 40 46 87 37 >60 2 14O 41 48 85 34 >60 3 12P 41 48 85 36 >60 3 13__________________________________________________________________________ *Incomplete hot dipping frequently occurred.

From TABLE 9 it follows that, as far as the contents of the elements are within the respective ranges as defined in this invention, high strength (T.S..gtoreq.40 kgf/mm.sup.2) is achieved while at the same time a satisfactory elongation (El.) and a satisfactory side bend elongation, i.e., stretch flanging property, are obtained.

EXAMPLE 5

Using the steel A having the composition shown in TABLE 1, hot dip galvanized steel sheets and galvannealed steel sheets were prepared under the various conditions shown in TABLE 10, and these sheets were examined as to the tensile property and the side bend elongation property, as in EXAMPLE 1, the results being summarized in TABLE 11.

TABLE 10__________________________________________________________________________ Reduction Annealing Annealing Rate Heating Rate Temperature Time Cooling Rate GalvannealingNo. (%) (.degree.C./s) (.degree.C.) (s) (.degree.C./s) (Yes, No) Remarks__________________________________________________________________________1 60 12 740 20 30 Yes/no Present2 70 10 730 40 30 Yes Invention3 45 10 740 20 35 Yes Comparative4 60 3 740 40 20 Yes Example5 60 20 760 20 30 Yes/no Present invention6 60 12 700 40 29 Yes Comparative7 60 12 800 40 30 Yes example8 55 15 725 5 27 Yes9 50 15 725 40 30 Yes Present10 60 5 740 30 30 Yes invention11 60 12 780 30 25 Yes12 55 10 720 40 20 Yes13 60 10 725 60 25 Yes__________________________________________________________________________ TABLE 11__________________________________________________________________________ Side Bend Percentage of Mean Diameter of Y.S. T.S. Y.R. El. Elongation Second Phase Ferrite GrainsNo. kgf/mm.sup.2 kgf/mm.sup.2 % % % % .mu.m__________________________________________________________________________1 38 46 83 39 >60 1.5 182 38 46 83 38 >60 1.5 173 65 70 93 8 20 2 254 38 40 95 39 >60 3 235 39 47 83 37 >60 2 186 55 65 85 12 28 1.5 partially non- recrystallized7 33 35 94 36 >60 3 228 48 55 87 18 30 3 partially non- recrystallized9 37 46 80 37 >60 2.0 1810 38 46 83 38 >60 1.5 1711 37 46 80 39 >60 1.5 1812 38 47 81 38 >60 2.0 1713 39 46 85 38 >60 1.5 17__________________________________________________________________________

As is seen from TABLE 11, as far as the producing conditions as defined in this invention are fulfilled, a satisfactory balance between strength and elongation and a satisfactory stretch flanging property can be achieved. Whether or not the galvanneal step is effected has a little influence on the properties, and substantially identical properties were obtained.

EXAMPLE 6

To examine the influence of the structure on the ductility and the stretch flanging property, specimens having the compositions shown in TABLE 12 were prepared under the conditions also shown in the same table, and the relationship between these properties was observed. The results are summarized in TABLE 13.

From TABLE 13 it follows that satisfactory properties can be obtained by properly controlling the percentage of the second phase, the mean diameter of recrystallized ferrite grains, and the area fraction of recrystallized ferrite. Among the Comparative Examples, Comparative Example E' has a T.S. lower than 40 kgf/mm.sup.2 and is excellent in elongation and side bend elongation property, but the mean grain diameter of ferrite is greater than 20 .mu.m, and therefore, its properties are not of satisfactory degree.

TABLE 12 (1)__________________________________________________________________________ Reduction HeatingSteel Chemical Composition (%) Rate Ratetype C Si Mn Nb Al N O S (%) (.degree.C./s)__________________________________________________________________________A' 0.05 0.01 0.80 0.015 0.025 0.0020 0.0020 0.008 60 5B' 0.07 0.01 0.80 0.015 0.015 0.0015 0.0020 0.005 70 10C' 0.05 0.01 1.20 0.070 0.045 0.0020 0.0030 0.008 55 7D' 0.18 0.01 0.90 0.015 0.035 0.0025 0.0030 0.010 55 7E' 0.18 0.01 1.00 0.040 0.035 0.0025 0.0040 0.010 55 7__________________________________________________________________________ TABLE 12 (2)__________________________________________________________________________ Annealing Annealing CoolingSteel Temperature Time Rate Galvannealingtype (.degree.C.) (s) (.degree.C./s) (Yes, No) Remarks__________________________________________________________________________A' 760 30 23 Yes PresentB' 780 40 25 Yes InventionC' 740 40 23 Yes ComparativeD' 750 40 20 Yes ExampleE' 750 40 25 Yes__________________________________________________________________________ TABLE 13__________________________________________________________________________ Area Yield of Percentage of Mean Diameter of Recrystallized Side BendSteel Second Phase Ferrite Grains Ferrite El. Elongationtype (%) (.mu.m) (%) % (%)__________________________________________________________________________A' Pearlite <2% 15 98 39 >60B' Same as Above 18 .about.100 37 >60C' Same as Above 18 90 31 30D' Pearlite 8% 15 92 31 35E' Pearlite 7% 25 93 34 >60__________________________________________________________________________

EXAMPLE 7

Using steels having compositions shown in TABLE 14, hot rolling was effected at a hot rolling finishing temperature of 800.degree. to 850.degree. , and cold rolling was effected at a reduction rate in thickness of 65%. Thereafter, the sheets were subjected to annealing at a heating rate of 10.degree. C./sec and then uniformly heated at 740.degree. C. for 30 seconds. After a hot dipping step and a galvannealing step were effected, the stretch flanging property was measured in accordance with the same procedure as in EXAMPLE 1.

TABLE 14______________________________________Steel Chemical Composition (%)type C Si Mn Nb Al N O S______________________________________Q 0.07 0.02 0.85 0.010 0.025 0.020 0.010 0.010R 0.08 0.02 0.80 0.012 0.035 0.025 0.015 0.007S 0.07 0.01 0.75 0.010 0.020 0.025 0.010 0.005T 0.07 0.02 0.75 0.012 0.025 0.025 0.010 0.003U 0.08 0.01 0.85 0.012 0.025 0.025 0.010 0.001______________________________________

When carrying out the test, the shearing was effected such that the clearance is greater than an ordinary one, and the end faces were not finished at all, to conduct the test under stricter conditions than those in EXAMPLE 1. The results of the test are shown in TABLE 15.

TABLE 15______________________________________ Steel Side Bend type Elongation (%)______________________________________ Q 55% R 57% S >60% T >60% U >60%______________________________________

From TABLE 15 it follows that although steel Q has a satisfactory side bend elongation of 55%, compared with a conventional material, this property can be further improved by reducing the S content. In TABLE 15, >60% represents the state in which the test piece was slipped off from the jig and no crack was produced, and thus an extremely excellent side bend elongation property (stretch flanging property).

This invention provides a high tensile cold rolled steel sheet and a hot dip galvanized sheet which, unlike conventional counterparts, have high strength and yet are excellent in ductility and stretch flanging property. Conventional high tensile steel sheets having a T.S. of 40 kgf/mm.sup.2 or higher have problems in that cracks are produced during press working chiefly due to deficiency in stretch flanging property and that they do not have a yield ratio high enough to retain a sufficient strength after being subjected to a forming process to produce, e.g., parts of automobiles. In the case of hot dip galvanized steel sheets, the surface treatment can often hinder the improvement in strength and hot dipping property. These problems are solved by this invention which provides a fine and uniform ferrite phase. The steel sheets of this invention can be used especially for rust-proof reinforcing members in automobiles.

Claims

1. A high tensile cold rolled steel sheet improved in stretch flanging property, consisting essentially of 0.03% to 0.15% by weight of C, 0.05% or less by weight of Si, 0.5% to 1.2% by weight of Mn, 0.005% to 0.045% by weight of Nb, and 0.10% or less by weight of Al, the remainder being iron and unavoidable impurities, and the steel sheet having a uniform and fine recrystallized ferrite structure having a mean grain diameter of 20 .mu.m or less and an area fraction of 95% or more.

2. A process for producing a high tensile cold rolled steel sheet improved in stretch flanging property, comprising the steps of:

preparing, as a material, steel consisting essentially of 0.03% to 0.15% by weight of C, 0.05% or less by weight of Si, 0.5% to 1.2% by weight of Mn, 0.005% to 0.045% by weight of Nb, and 0.10% or less by weight of Al, the remainder being iron and unavoidable impurities;

subjecting the material to hot rolling;

effecting cold rolling at a reduction rate in thickness of more than 50%; and

effecting annealing in which the material is heated at a heating rate of 5.degree. C./sec or more and retained in a temperature range of 720.degree. to 780.degree. C. for 20 to 60 seconds in a continuous annealing line, and then cooling the material.

3. A high tensile hot dip galvanized steel sheet improved in stretch flanging property, consisting essentially of 0.03% to 0.15% by weight of C, 0.05% or less by weight of Si, 0.5% to 1.2% by weight of Mn, 0.005% to 0.045% by weight of Nb, and 0.10% or less by weight of Al, the remainder being iron and unavoidable impurities, and the steel sheet having a uniform and fine recrystallized ferrite structure having a mean grain diameter of 20 .mu.m or less and an area fraction of 95% or more.

4. A process for producing a high tensile hot dip galvanized steel sheet improved in stretch flanging property, comprising the steps of:

preparing, as a material, steel consisting essentially of 0.03% to 0.15% by weight of C, 0.05% or less by weight of Si, 0.5% to 1.2% by weight of Mn, 0.005% to 0.045% by weight of Nb, and 0.10% or less by weight of Al, the remainder being iron and unavoidable impurities;

subjecting the material to hot rolling;

effecting cold rolling at a reduction rate in thickness of more than 50%; and

effecting annealing in which the material is heated at a heating rate of 5.degree. C./sec or more and retained in a temperature range of 720.degree. to 780.degree. C. for 20 to 60 seconds in an in-line anneal type continuous hot dip galvanizing line, and then cooling and hot-dipping the material.

5. A process for producing a high tensile hot dip galvanized steel sheet improved in stretch flanging property, comprising the steps of:

preparing, as a material, steel consisting essentially of 0.03% to 0.15% by weight of C, 0.05% or less by weight of Si, 0.5% to 1.2% by weight of Mn, 0.005% to 0.045% by weight of Nb, and 0.10% or less by weight of Al, the remainder being iron and unavoidable impurities;

subjecting the material to hot rolling;

effecting cold rolling at a reduction rate in thickness of more than 50%; and

effecting annealing in which the material is heated at a heating rate of 5.degree. C./sec or more and retained in a temperature range of 720.degree. to 780.degree. C. for 20 to 60 seconds in an in-line anneal type continuous hot dip galvanizing line, and then cooling, hot-dipping and galvannealing the material.