METHOD OF MANUFACTURING HOT ROLLED STEEL SHEET FOR SQUARE COLUMN FOR BUILDING STRUCTURAL MEMBERS

Abstract
A method of manufacturing a hot rolled steel sheet for a square column for building structural members includes a hot rolling step, a cooling step, and a coiling step performed on a steel to form a hot rolled steel sheet, wherein the steel has a composition containing, in terms of % by mass, C: 0.07 to 0.18%, Mn: 0.3 to 1.5%, P: 0.03% or less, S: 0.015% or less, Al: 0.01 to 0.06%, N: 0.0006% or less, and the balance being Fe and unavoidable impurities.
Description
TECHNICAL FIELD

This disclosure relates to a method of manufacturing a hot rolled steel sheet for a square column for building structural members. In particular, it relates to decreasing the yield ratio of and further improving the toughness of a square column manufactured by cold-rolling a hot rolled steel sheet as a raw material. The term hot rolled steel sheet is used to refer both a hot rolled steel sheet and a hot rolled steel strip.


BACKGROUND

A square column is typically manufactured through cold forming by using a hot rolled steel sheet (hot rolled steel strip) or plate as the raw material. Examples of the cold forming employed in manufacturing a square column include press forming and roll forming. When a square column is to be manufactured through roll forming using a hot rolled steel sheet as a raw material, it is a prevailing practice to first form a hot rolled steel sheet into a round steel pipe and then cold-form the round steel pipe into a square column. This method of manufacturing a square column through roll forming has an advantage of high productivity compared to a method of manufacturing a square column through press forming. However, according to the method of manufacturing a square column through roll forming, large work strain is introduced in the pipe axis direction as the sheet is formed into a round form. Moreover, during the process of cold-forming the round form into a square form, flat portions of the square column are subjected to bend-back forming in a direction opposite the direction in which bending into the round form had been performed. Accordingly, a square column manufactured through roll forming has a problem in that the yield ratio in the pipe axis direction tends to be high and the ductility and toughness tend to be degraded due to the Bauschinger effect or the like.


To address this problem, for example, Japanese Unexamined Patent Application Publication No. 08-246095 describes a method of manufacturing a steel material for a low-yield-ratio, high-toughness square column, the method including hot-rolling a steel at a heating temperature of 1150° C. to 1250° C. and finishing temperature of 800° C. to 870° C. and performing coiling at 500° C. to 650° C., the steel containing, in terms of % by weight, at least one selected from C: 0.03 to 0.25%, Si: 0.10 to 0.50%, Mn: 0.30 to 2.00%, P: 0.020% or less, S: 0.020% or less, O: 50 ppm or less, H: 5 ppm or less, Al: 0.150% or less, Ti: 0.050% or less, V: 0.100% or less, Nb: 0.080% or less, Zr: 0.050% or less, and B: 0.0050% or less, and N to satisfy the relationship N≦(1/5){(1/2)Al+(1/1.5)Ti+(1/3.5)V+(1/6.5)Nb+(1/6.5)Zr+B}.


Japanese Unexamined Patent Application Publication No. 03-219015 describes a method of manufacturing a square pipe with low yield ratio and good low-temperature toughness, in which a low-carbon steel pipe is heated to a temperature of Ac3—250° C. to Ac3—20° C., quenched at a cooling rate of 15° C./s or more, cold-formed into a square pipe, and tempered at 200° C. to 600° C. According to Japanese Unexamined Patent Application Publication No. 03-219015, post-intercritical-anneal quenching, cold-forming, and tempering are sequentially performed to eliminate the effect of work hardening occurred during pipe forming and thus a square pipe with low yield ratio and high toughness can be manufactured.


Japanese Unexamined Patent Application Publication No. 2002-241897 does not explicitly describe a steel sheet for a square column. However, a steel sheet having high formability and low yield ratio is described therein. The steel sheet described in Japanese Unexamined Patent Application Publication No. 2002-241897 contains, on a % by mass basis, C: 0.0002 to 0.1%, Si: 0.003 to 2.0%, Mn: 0.003 to 3.0%, and Al: 0.002 to 2.0%, one or more groups selected from Group 1 including B: 0.0002 to 0.01%, Group 2 including a total of 0.005 to 1.0% of at least one selected from Ti, Nb, V, and Zr, Group 3 including a total of 0.005 to 3.0% of at least one selected from Cr, Mo, Cu, and Ni, and Group 4 including Ca: 0.005% or less and a rare earth element: 0.20% or less, and, as impurities, P: 0.0002 to 0.15%, S: 0.0002 to 0.05%, and N: 0.0005 to 0.015%, in which a mean crystal grain diameter of a ferrite phase is more than 1 μm but not more than 50 μM, the volume ratio of the ferrite phase is 70% or more, the aspect ratio of the ferrite phase is 5 or less, 70% of ferrite grain boundaries are high-angle grain boundaries, and the mean crystal grain diameter of a second phase, whose volume fraction among the rest of the phase is maximum, is 50 μm or less. This steel sheet has little variation in yield strength and yield ratio.


WO 2005/028693 A1 describes a hot rolled steel sheet for processing. The hot rolled steel sheet described in WO2005/028693 A1 has a composition of, on a % by weight basis, C: 0.01 to 0.2%, Si: 0.01 to 0.3%, Mn: 0.1 to 1.5%, Al: 0.001 to 0.1%, and P, S, and N adjusted to a particular value or less, and has a microstructure including a polygonal ferrite primary phase and a hard second phase, the volume fraction of the hard second phase being 3 to 20%, the hardness ratio (hard second phase hardness/polygonal ferrite hardness) being 1.5 to 6, and the grain diameter ratio (polygonal ferrite grain diameter/hard second phase grain diameter) being 1.5 or more. According to WO 2005/028693 A1, a hot rolled steel sheet that obtains a BH amount of 60 MPa or more can be manufactured by introducing strain through pressing and by performing bake hardening, and a press-formed part having a strength comparable to that achieved by a 540-640 MPa-grade steel sheet can be stably manufactured from a 370-490 MPa-grade hot rolled steel sheet.


Japanese Unexamined Patent Application Publication No. 2001-303168 describes a method of manufacturing a steel sheet having a good brittle crack property. According to Japanese Unexamined Patent Application Publication No. 2001-303168, a steel sheet having a microstructure constituted by a ferrite structure and a pearlite structure and having a composition that satisfies C: 0.03 to 0.2%, Si: 0.5% or less, Mn: 1.8% or less, Al: 0.01 to 0.1%, and N: 0.01% or less is obtained by hot-rolling, and that steel sheet is subjected to first cooling that includes cooling a region 5 to 15% in terms of thickness from a front surface of the steel sheet and a region 5 to 15% in terms of thickness from a back surface of the steel sheet at an average cooling rate of 4 to 15° C./s to a temperature of 450 to 650° C. or less. Then, the steel sheet is recuperated to a temperature not more than the Ar3 transformation temperature and subjected to second cooling at an average cooling rate of 1 to 10° C./s. As a result, the regions 5 to 15% in terms of thickness from the front surface and the back surface of the steel sheet come to contain fine ferrite grains with an equivalent circle mean diameter of 4 μm or less and an aspect ratio of 2 or less and the region 50 to 75% of the sheet thickness comes to contain fine ferrite grains with an equivalent circle mean diameter of 7 μm or less and an aspect ratio of 2 or less. Accordingly, a steel sheet having good COD properties, low-temperature toughness, and good brittle crack resistance can be obtained.


However, a steel material manufactured in Japanese Unexamined Patent Application Publication No. 08-246095 has a yield ratio of about 81 to 85% at the lowest and fails to achieve a low yield ratio of 80% or less. Moreover, the absorbed energy at 0° C. is sometimes less than 100 J. Thus, there is a problem in that high toughness cannot be stably achieved. According Japanese Unexamined Patent Application Publication No. 03-219015, two different types of heat treatment, namely, quenching after intercritical annealing and tempering, need to be performed and there is a problem in that the process is thus complicated, resulting in decreased productivity and increased manufacturing cost.


When a steel sheet described in Japanese Unexamined Patent Application Publication No. 2002-241897 is used as a raw material, formed into a round steel pipe, and cold-formed into a square column, the degree of cold working is high at the flat portions of the square column. Thus, there is a problem in that the square column may not always achieve sufficient toughness. When a steel sheet described in WO 2005/028693 A1 is used as a raw material, formed into a round steel pipe, and cold-formed into a square column, the degree of cold working is high at the flat portions of the obtained square column and thus there is a problem in that the yield strength and then the yield ratio are increased, and the toughness is decreased. Moreover, the hot rolled steel sheet described in WO 2005/028693 A1 is susceptible to strain aging and is thus not suitable as a raw material for manufacturing a square column by cold forming.


When a hot rolled steel sheet manufactured in Japanese Unexamined Patent Application Publication No. 2001-303168 is used and cold-formed into a square column, the yield strength of the square column obtained by cold forming increases and, as a result, the yield ratio increases, because the ferrite grains in this hot rolled steel sheet are fine. Accordingly, when a hot rolled steel sheet manufactured by the technology described in Japanese Unexamined Patent Application Publication No. 2001-303168 is used as a raw material, the resulting square column cannot achieve a low yield ratio of 80% or less needed for building structural members.


It could therefore be helpful to provide a hot rolled steel sheet suitable as a raw material for a square column for building structural members, the hot rolled steel sheet having strength of 215 MPa or more in terms of yield strength and 400 to 510 MPa in terms of tensile strength, a low yield ratio of 75% or less, and high toughness of 180 J or more in terms of absorbed energy in a Charpy impact test performed at a test temperature of 0° C. and preferably −30° C.


SUMMARY

We thus provide:

    • (1) A hot rolled steel sheet for a square column for building structural members, the hot rolled steel sheet having a composition of, in terms of % by mass,

















C: 0.07 to 0.18%,
Mn: 0.3 to 1.5%,



P: 0.03% or less,
S: 0.015% or less,



Al: 0.01 to 0.06%,
N: 0.006% or less,











    • and the balance being Fe and unavoidable impurities, and having a microstructure that includes a primary phase constituted by ferrite and a second phase constituted by pearlite or pearlite and bainite, wherein a second phase frequency defined by equation (1) below is 0.20 to 0.42 and a mean crystal grain diameter of the primary phase and the second phase together is 7 to 15 μm.

    • Note








Second phase frequency=(Number of second phase grains intersecting line segments of particular length)/(Number of primary phase grains and second phase grains intersecting line segments of particular length)  (1)

    • (2) The hot rolled steel sheet for a square column for building structural members described in (1), wherein, in addition to the composition, Si: less than 0.4% by mass is contained.
    • (3) The hot rolled steel sheet for a square column for building structural members according to (1) or (2), wherein, in addition to the composition, at least one selected from Nb: 0.015% or less, Ti: 0.030% or less, and V: 0.070% or less is contained in terms of % by mass.
    • (4) The hot rolled steel sheet for a square column for building structural members according to any one of (1) to (3), wherein, in addition to the composition, B: 0.008% by mass or less is contained.
    • (5) A method of manufacturing a hot rolled steel sheet for a square column for building structural members, the method including a hot rolling step, a cooling step, and a coiling step performed on a steel to form a hot rolled steel sheet, wherein the steel has a composition containing, in terms of % by mass,

















C: 0.07 to 0.18%,
Mn: 0.3 to 1.5%,



P: 0.03% or less,
S: 0.015% or less,



Al: 0.01 to 0.06%,
N: 0.006% or less,











    • and the balance being Fe and unavoidable impurities,
      • the hot rolling step includes heating the steel to a heating temperature of 1100 to 1300° C., rough-rolling the heated steel at a rough rolling end temperature of 1150 to 950° C. to form a sheet bar, and finish-rolling the sheet bar at a finish rolling start temperature of 1100 to 850° C. and a finish rolling end temperature of 900 to 750° C. to form a hot rolled sheet,
      • the cooling step is started immediately after completion of the finish rolling and cooling is performed to a coiling temperature such that an average cooling rate in a temperature range of 750 to 650° C. in terms of surface temperature is 20° C./s or less, a time taken for a temperature at a sheet thickness center to reach 650° C. is within 35 s, and an average cooling rate in a temperature range of 750 to 650° C. at the sheet thickness center is 4 to 15° C./s, and
      • the coiling step includes coiling the cooled steel sheet at a coiling temperature of 500 to 650° C. and allowing the coiled sheet to cool.

    • (6) A method of manufacturing a hot rolled steel sheet for a square column for building structural members, the method including a hot rolling step, a cooling step, and a coiling step performed on a steel to form a hot rolled steel sheet,
      • wherein the steel has a composition containing, in terms of % by mass,




















C: 0.07 to 0.18%
Mn: 0.3 to 1.5%,



P: 0.03% or less,
S: 0.015% or less,



Al: 0.01 to 0.06%,
N: 0.0006% or less,











    • and the balance being Fe and unavoidable impurities,
      • the hot rolling step includes heating the steel to a heating temperature of 1100 to 1300° C., rough-rolling the heated steel at a rough rolling end temperature of 1150 to 950° C. to form a sheet bar, and finish-rolling the sheet bar at a finish rolling start temperature of 1100 to 850° C. and a finish rolling end temperature of 900 to 750° C. to form a hot rolled sheet,
      • the cooling step is started immediately after completion of the finish rolling and includes three stages of cooling, which are first cooling, second cooling, and third cooling so that a time taken for a temperature at a sheet thickness center to reach 650° C. is within 35 s from the start of cooling, wherein the first cooling includes performing cooling so that a cooling end temperature is 550° C. or more in terms of surface temperature, the second cooling includes performing air cooling for 3 to 15 s after completion of the first cooling, and the third cooling includes performing cooling to a temperature of 650° C. or less at an average cooling rate of 4 to 15° C./s in a temperature range of 750 to 650° C. in terms of the temperature at the sheet thickness center after completion of the second cooling, and
      • the coiling step includes coiling the cooled steel sheet at a coiling temperature of 500 to 650° C. and allowing the coiled sheet to cool.

    • (7) The method of manufacturing a hot rolled steel sheet for a square column for building structural members according to (5) or (6), wherein a total reduction of the finish rolling is 35 to 70%.

    • (8) The method of manufacturing a hot rolled steel sheet for a square column for building structural members according to (5) or (6), wherein, in addition to the composition of the steel, Si: less than 0.4% by mass is contained.

    • (9) The method of manufacturing a hot rolled steel sheet for a square column for building structural members according to (5) or (6), wherein, in addition to the composition of the steel, at least one selected from Nb: 0.015% or less, Ti: 0.030% or less, and V: 0.070% or less is contained in terms of % by mass.

    • (10) The method of manufacturing a hot rolled steel sheet for a square column for building structural members according to (5) or (6), wherein, in addition to the composition of the steel, B: 0.008% by mass or less is contained.

    • (11) The method of manufacturing a hot rolled steel sheet for a square column for building structural members according to (6), wherein fourth cooling is performed after completion of the third cooling in addition to the three stages of the cooling.

    • (12) A square column for building structural members, manufactured by cold-forming a raw material which is the hot rolled steel sheet according to any one of (1) to (4).





A hot rolled steel sheet for a square column for building structural members can be manufactured easily and at low cost at significant industrial advantage. A square column exhibiting strength of 295 MPa or more in terms of yield strength and 400 MPa or more in terms of tensile strength and a low yield ratio of 80% or less in a column axis direction, and high toughness of 150 J or more in terms of a Charpy impact test absorbed energy at a test temperature of −0° C. can be easily manufactured by cold-forming the hot rolled steel sheet.





BRIEF DESCRIPTION OF THE DRAWINGS


FIG. 1 is a diagram indicating one example of line segments used for measuring a second phase frequency.



FIGS. 2A-2B include graphs indicating the influence of the second phase frequency on a yield ratio YR and a Charpy absorbed energy vE0 at a test temperature of 0° C. of a cold-formed square column.



FIGS. 3A-3B include graphs indicating the influence of a mean crystal grain diameter on a yield ratio YR and a Charpy absorbed energy vE0 at a test temperature of 0° C. of a cold-formed square column.



FIG. 4 is a graph indicating the relationship between a Charpy absorbed energy vE0 at a test temperature of 0° C. of a cold-formed square column and a mean grain diameter of a second phase.



FIG. 5 is a graph indicating the relationship between a Charpy absorbed energy vE0 at a test temperature of 0° C. of a cold-formed square column and a second phase microstructure volume fraction.





DETAILED DESCRIPTION

The hot rolled steel sheet has the above-described properties and can be used as a raw material to manufacture a square column by cold forming, the square column exhibiting strength of 295 to 445 MPa in terms of yield strength and 400 to 550 MPa in terms of tensile strength and a low yield ratio of 80% or less in the pipe axis direction, and high toughness of 150 J or more in terms of an absorption energy in a Charpy impact test performed at a test temperature of 0° C. and preferably −30° C.


The “hot rolled steel sheet” discussed here refers to a hot rolled steel sheet having a sheet thickness of 6 mm or more and 25 mm or less.


We conducted extensive studies on the effects of various factors on the yield ratio and toughness of a square column manufactured by cold-forming a hot rolled steel sheet as a raw material. We found that the microstructure of the hot rolled steel sheet used as a raw material, in particular, the presence of a second phase, greatly affects the yield ratio and toughness of the square column manufactured by cold forming.


It has been said that in a multiphase microstructure constituted by a ferrite phase and a non-ferrite second phase, the presence of the second phase, which is hard and in which brittle cracks easily propagate compared to in ferrite, decreases the toughness. However, we found that the toughness cannot be satisfactorily evaluated based on the volume fraction of the second phase and the mean grain diameter of the second phase which are parameters that are usually used. This is because the second phase sometimes takes an aggregated form or, in other cases, exists along crystal grain boundaries and the second phase volume fraction and mean grain diameter significantly differ depending on the morphology of the second phase. If the effect of the second phase on toughness is evaluated based on the volume fraction and mean crystal grain diameter of the second phase, which are parameters typically used, then the effect of the second phase that exists along grain boundaries will be underestimated.


We further found that the effect of the second phase on the toughness and yield ratio of a square column manufactured by cold forming can be satisfactorily evaluated by using a second phase frequency of a hot rolled steel sheet used as the raw material and the mean grain diameter of the primary phase, which is ferrite, and the second phase together. The “second phase frequency” discussed here refers to a value obtained as follows.


First, the microstructure of a cross section (L cross section) taken in a rolling direction of a hot rolled steel sheet used as a raw material is photographed with an optical microscope or a scanning electron microscope. A particular number of line segments of a particular length are drawn in the rolling direction and in a sheet thickness direction on the obtained photograph of the microstructure, as shown in FIG. 1. The number of crystal grains that intersect the line segments is counted for each of the primary phase and the second phase. When an end of a line segment stays within a crystal grain, the count is 0.5. The ratio of the obtained total number of grains of the second phase intersecting the line segments (number of grains of second phase) to the obtained total number of grains of both phases intersecting line segments (total number of grains), i.e., (number of grains of second phase)/(total number of grains), is determined and the result is defined to be the second phase frequency. The length of each line segment may be appropriately determined in accordance with the size of the microstructure.


Experimental results will now be described. A slab (thickness: 230 mm) having a composition of, in terms of % by mass, 0.09 to 0.15% C-0.01 to 0.18% Si-0.43 to 1.35% Mn-0.017 to 0.018% P-0.0025 to 0.0033% S-0.031 to 0.040% Al-Balance Fe and unavoidable impurities was heated and soaked at 1200 to 1270° C., subjected to hot rolling that included rough rolling and finish rolling to form a hot rolled steel strip (thickness: 16 to 25 mm), and then coiled. Finish rolling was performed at a total reduction of 40 to 52% and a finish rolling end temperature of 750 to 850° C. Upon completion of finish rolling, accelerated cooling was performed. The coiling temperature was 550 to 600° C. and the steel strip was allowed to cool after being coiled.


The resulting hot rolled steel strip serving as a raw material was formed by cold-rolling into a round steel pipe and then the round steel pipe was cold rolled into a square column (250 mm square to 550 mm square). A JIS 5 tensile test specimen was sampled from a flat portion of the resulting square column so that the tensile direction was the pipe longitudinal direction in accordance with the provisions of JIS Z 2210. A tensile test was performed in accordance with provisions of JIS Z 2241 to determine the yield ratio. A V-notch test specimen was sampled from a ¼ t thickness position of a flat portion of the resulting square column so that the pipe longitudinal direction was the test specimen longitudinal direction and a Charpy impact test was performed in accordance with provisions of JIS Z 2242 at a test temperature of 0° C. to determine the absorbed energy (J).


A microstructure observation specimen was sampled from the hot rolled steel strip used as the raw material of the square column. The observation face of the specimen was at the ¼ t thickness position of a cross section (L cross section) taken in the rolling direction. The specimen was polished and etched with nital, and the microstructure thereof was observed with an optical microscope or a scanning microscope. The microstructure image obtained was analyzed with an image analyzer to determine the volume fraction of each phase, the mean crystal grain diameter of each phase by an intercept method, and the mean crystal grain diameter of the primary phase and the second phase together.


As shown in FIG. 1, six line segments each 125 μm in length were drawn in the rolling direction and another six in the sheet thickness direction in the microstructure image obtained and the number of crystal grains of each phase that intersect these line segments was counted. The second phase frequency defined by the following equation was calculated from the obtained number of grains of each phase intersecting the line segments: Second phase frequency=(Number of second phase grains intersecting the line segments)/(Total number of grains of primary phase and second phase intersecting the line segments). The second phase was constituted by pearlite and bainite and the primary phase was constituted by polygonal ferrite.



FIG. 2A is a graph showing the relationship between the second phase frequency of a hot rolled steel strip used as the raw material and the yield ratio YR of a flat portion of a cold-formed square column and FIG. 2B is a graph showing the relationship between the second phase frequency and the absorbed energy vE0 of the flat portion measured in a Charpy impact test at a test temperature of 0° C. FIG. 3A is a graph showing the relationship between the mean crystal grain diameter of the primary phase and the second phase together of the hot rolled steel strip used as the raw material and the yield ratio YR of the flat portion of the cold-formed square column and FIG. 3B is a graph showing the relationship between the mean crystal grain diameter and the absorbed energy vE0 of the flat portion measured in a Charpy impact test at a test temperature of 0° C.



FIGS. 2A and 2B show that the yield ratio YR and the absorbed energy vE0 in a Charpy impact test of a flat portion of a cold-formed square column can be characterized with less variation by using the second phase frequency. This shows that the second phase frequency significantly affects the toughness and yield ratio of the cold-formed square column. FIGS. 3A and 3B show that the yield ratio YR and the absorbed energy vE0 in a Charpy impact test of a flat portion of a cold-formed square column can also be characterized with less variation by using the mean crystal grain diameter of the primary phase (ferrite) and the second phase (pearlite and bainite) together. This shows that the mean crystal grain diameter significantly affects the toughness and yield ratio of the cold-formed square column. When the microstructure of a region from a surface to near a ¼ t position has come to have a microstructure including bainite as the primary phase as a result of quenching, the yield ratio increases notably.



FIGS. 2A, 2B, 3A and 3B also show that a yield ratio YR of 80% or less in a cold-formed square column, can be achieved by adjusting the second phase frequency to 0.20 or more and the mean crystal grain diameter of the primary phase (ferrite) and the second phase (pearlite and bainite) together to 7 μm or more. It is also shown that an absorbed energy vE0 of 150 J or more in a Charpy impact test of a cold-formed square column can be achieved by adjusting the second phase frequency to 0.42 or less and the mean crystal grain diameter of the primary phase (ferrite) and the second phase (pearlite and bainite) together to 15 μm or less.


For reference, the relationship between the Charpy absorbed energy vE0 of a flat portion of a cold-formed square column and a second phase mean grain diameter of a hot rolled steel strip used as a raw material is shown in FIG. 4 and the relationship between vE0 and the second phase microstructure volume fraction is shown in FIG. 5. FIGS. 4 and 5 show the relationship between vE0 and the second phase mean grain diameter and the relationship between vE0 and the second phase microstructure volume fraction have large variations and that the toughness of the flat portion of the cold-formed square column cannot be satisfactorily evaluated based on either the second phase mean grain diameter or the second phase microstructure volume fraction.


Our hot rolled steel sheets have a strength of 215 MPa or more in terms of yield strength and 400 to 510 MPa in terms of tensile strength, a low yield ratio of 75% or less, preferably an elongation of 28% or more, and high toughness of 180 J or more in terms of absorbed energy in a Charpy impact test at a test temperature of 0° C. and preferably at −30° C.


First, the reasons for setting limitations on the composition of the hot rolled steel sheet are described. In the description below, % by mass is merely indicated by % unless otherwise noted.


C: 0.07 to 0.18%

Carbon (C) is an element that increases the strength of a steel sheet by solution strengthening and contributes to formation of pearlite, which is a part of the second phase. To obtain desired tensile properties, toughness, and steel sheet microstructure, the C content needs to be 0.07% or more. At a C content exceeding 0.18%, the desired steel sheet microstructure is no longer obtained and the desired tensile properties and toughness of the hot rolled steel sheet and the square column cannot be obtained. Accordingly, the C content is 0.07 to 0.18%. Preferably, the C content is 0.09 to 0.17%.


Mn: 0.3 to 1.5%

Manganese (Mn) is an element that increases the strength of a steel sheet through solution strengthening and the content thereof needs to be 0.3% or more to obtain the desired steel sheet strength. At a Mn content less than 0.3%, the ferrite transformation start temperature rises and the microstructure tends to coarsen. At a Mn content exceeding 1.5%, the yield strength of the steel sheet increases excessively. Thus, the yield ratio of a square column manufactured by cold-forming such a steel sheet exhibits a high yield ratio and the desired yield ratio can no longer be obtained. Accordingly, the Mn content is limited to 0.3 to 1.5%. The Mn content is preferably 0.35 to 1.4%.


P: 0.03% or Less

Phosphorus (P) is an element that segregates at ferrite grain boundaries and has an effect of decreasing toughness. P is an impurity and the content thereof is preferably as low as possible. However, since excessively decreasing the P content increases the refining cost, the P content is preferably 0.002% or more. A P content up to 0.03% is allowable. Thus, the P content is limited to 0.03% or less and more preferably 0.025% or less.


S: 0.015% or Less

Sulfur (S) exists as sulfides in steel and, in our composition range, mainly exists as MnS. MnS becomes thinly stretched in a hot rolling step and adversely affects ductility and toughness. Accordingly, the S content is preferably as low as possible. However, excessively decreasing the S content increases the refining cost and thus the S content is preferably 0.0002% or more. The S content up to 0.015% is allowable. Thus, the S content is limited to 0.015% or less and preferably 0.010% or less.


Al: 0.01 to 0.06%

Aluminum (Al) is an element that acts as a deoxidizer and has an effect of fixing N as AlN. The Al content needs to be 0.01% or more to achieve these effects. At an Al content less than 0.01%, deoxidizing power is insufficient if Si is not added, the amount of oxide-based inclusions is increased, the cleanliness of the steel sheet is degraded, and the quality of a welded portion of the square column is adversely affected. At an Al content exceeding 0.06%, an amount of Al dissolved as a solid solution is increased, the risk of formation of oxides in the welded portion is increased during welding of a square column, in particular, welding in air, and the toughness of the welded portion of the square column is decreased. Accordingly, the Al content is limited to 0.01 to 0.06%. Preferably, the Al content is 0.02 to 0.05%.


N: 0.006% or Less

Nitrogen (N) decreases ductility of a steel sheet and weldability of a square column and thus the N content is desirably as low as possible. A N content up to 0.006% is allowable. Accordingly, the N content is limited to 0.006% or less and is preferably 0.005% or less.


The elements described heretofore are the basic components. In addition to these basic components, Si: less than 0.4%, and/or at least one selected from Nb: 0.015% or less, Ti: 0.030% or less, and V: 0.070% or less, and/or B: 0.008% or less can be selected as needed as optional elements.


Si: Less than 0.4%


Silicon (Si) is an element that contributes to increasing the strength of a steel sheet by solution strengthening and can be added as needed to obtain the desired steel sheet strength. To achieve this effect, the Si content preferably exceeds 0.01% but at a Si content of 0.4% or more, fayalite also known as red scale easily forms on surfaces of a steel sheet and appearance properties of surfaces are frequently degraded. Accordingly, the Si content is preferably less than 0.4% if Si is to be added. When Si is not intentionally added, the content of Si as an unavoidable impurity is 0.01% or less.


At least one selected from Nb: 0.015% or less, Ti: 0.030% or less, and V: 0.070% or less.


Niobium (Nb), titanium (Ti), and vanadium (V) all form carbides and nitrides and are elements that have an effect of reducing the crystal grain diameter and the yield ratio tends to be high as a result. Accordingly, these elements are desirably not contained but as long as their contents are within the range that does not excessively decrease the crystal grain diameter, in other words, within the range in which the mean grain diameter of the ferrite phase and the second phase (pearlite and bainite) together is 7 μm or more, these elements may be contained. The content ranges are Nb: 0.015% or less, Ti: 0.030% or less, and V: 0.070% or less.


B: 0.008% or Less

Boron (B) is an element which delays ferrite transformation during a cooling process, promotes formation of a low-temperature transformed ferrite, i.e., an acicular ferrite phase, and increases the strength of a steel sheet. Addition of B increases the yield ratio of a steel sheet and thus increases the yield ratio of a square column. Accordingly, boron can be contained as needed as long as the yield ratio of the square column is 80% or less. Such a B content is 0.008% or less.


The balance other than the components described above is Fe and unavoidable impurities. As unavoidable impurities, O: 0.005% or less and N: 0.005% or less are allowable.


Next, the reasons for setting limitations on the microstructure of a hot rolled steel sheet are described.


Our hot rolled steel sheets have the above-described composition and a microstructure that includes ferrite as a primary phase and a second phase. The second phase is constituted by pearlite or pearlite and bainite. The primary phase referred here is a phase having an area fraction of 50% or higher.


The second phase constituted by pearlite or pearlite and bainite has a second phase frequency of 0.20 to 0.42. At a second phase frequency less than 0.20, the yield ratio of a square column obtained by cold forming exceeds 0.80 and fails to satisfy the yield ratio required (0.80 or less) as building structural members. At a second phase frequency exceeding 0.42, the desired toughness required for a square column for building structural members, namely, an absorbed energy vE0 of 150 J or more in a Charpy impact test at a test temperature of 0° C. cannot be obtained. Accordingly, the second phase frequency is 0.20 to 0.42. Preferably, the second phase frequency is 0.40 or less. To obtain high toughness, namely, an absorbed energy vE−30 of 150 J or more in a Charpy impact test at a test temperature of −30° C., the second phase frequency is preferably 0.35 or less. The second phase frequency is defined by the following equation:





Second phase frequency=(Number of second phase grains intersecting line segments of particular length)/(Total number of primary phase grains and second phase grains intersecting line segments of particularly length)


The measurement method is as described above.


The hot rolled steel sheet has a microstructure that has not only the above-described second phase frequency but also a mean crystal grain diameter of 7 to 15 μm for the ferrite phase, which is a primary phase, and a second phase together.


“The mean crystal grain diameter of the ferrite phase, which is a primary phase, and a second phase together” refers to the mean crystal grain diameter determined by measuring all crystal grains in the ferrite phase, which is the primary phase, and the pearlite phase and the bainite phase which form the second phase. The mean crystal grain diameter is measured by using a microstructure observation test specimen sampled from a particular position of a hot rolled steel sheet. A cross section of the test specimen taken in the rolling direction (L cross section) is polished, etched with nital, subjected to microstructural observation with an optical microscope (magnitude: 500) or a scanning electron microscope (magnitude: 500) at a ¼ t sheet thickness position, and photographed for one or more areas of view, and the obtained photograph or image was subjected to image processing so that the mean grain diameter is calculated by an intercept method.


When the mean crystal grain diameter measured by the method described above is less than 7 μm, the grains are too fine for a square column to achieve a yield ratio of 80% or less. If the grains are coarsened to 15 μm or larger, the toughness of the square column is degraded and a desired toughness cannot be obtained. From the viewpoint of reliably achieving higher toughness, the mean grain diameter is preferably 12 μm or less. A hot rolled steel sheet having the above-described composition and the above-described microstructure has a strength of 215 MPa or more in terms of yield strength and 400 to 510 MPa in terms of tensile strength, a low yield ratio of 75% or less, and a high toughness of 180 J or more in terms of an absorbed energy in a Charpy impact test at a test temperature of 0° C. and preferably at a test temperature of −30° C. When such a hot rolled steel sheet is used as a raw material and cold-rolled into a square column, a square column having a strength of 295 MPa or more in terms of yield strength and 400 to 550 MPa in terms of tensile strength and a low yield ratio of 80% or less in the column axis direction, and high toughness of 150 J or more in terms of an absorbed energy in a Charpy impact test at a test temperature of 0° C. and preferably at a test temperature of −30° C. can be obtained.


Next, a preferred method of manufacturing a hot rolled steel sheet is described. A hot rolled steel sheet is manufactured by subjecting a steel having the above-described composition to a hot rolling step, a cooling step, and a coiling step.


The steel to be used is manufactured such that a molten steel having the above-described composition is produced by a common known refining method such as one using a converter, electric furnace, vacuum melting furnace or the like, and then cast into a slab with desired dimensions by a common known casting method such as a continuous casting method. The molten steel may be further subjected to secondary refining such as ladle refining. Instead of the continuous casting method, an ingot-slabbing method may be employed.


In a hot rolling step, a steel having the above-described composition is heated to a heating temperature of 1100 to 1300° C. and subjected to rough rolling at a rough rolling end temperature of 950 to 1150° C. to form a sheet bar. The sheet bar is then finish-rolled at a finish rolling start temperature of 1100 to 850° C. and a finish rolling end temperature of 750 to 900° C. Heating temperature: 1100 to 1300° C.


When the heating temperature for the steel is less than 1100° C., deformation resistance of a material to be rolled becomes excessively large and withstand load and rolling torque of a roughing mill and a finishing mill become insufficient, thereby the rolling becomes difficult to be performed. In contrast, when the heating temperature exceeds 1300° C., austenite crystal grains coarsen and it becomes difficult to refine the crystal grains even if deforming and recrystallizing of austenite grains are repeated by performing rough rolling and finish rolling. Thus, it becomes difficult for the hot rolled steel sheet to obtain the desired mean crystal grain diameter. Accordingly, the heating temperature of the steel is preferably limited to 1100 to 1300° C. More preferably, the heating temperature is 1100 to 1250° C. If the withstand load and rolling torque of the rolling mill allow, a heating temperature in the range of 1100° C. or less and the Ac3 transformation point or more can be selected. The thickness of the steel may be about 200 to 350 mm, which is the thickness generally employed, and is not particularly limited.


The heated steel is subjected to rough rolling to be formed into a sheet bar. Rough rolling end temperature: 950 to 1150° C.


When the heated steel is subjected to rough rolling, austenite grains are deformed and recrystallized become finer. At a rough rolling end temperature less than 950° C., the withstand load and rolling torque of the roughing mill tend to be insufficient. In contrast, in the case where the temperature exceeds 1150° C., austenite grains coarsen and it becomes difficult to obtain the desired mean crystal grain diameter of 15 μm or less even if finish rolling is performed subsequently. Accordingly, the rough rolling end temperature is preferably limited to 950 to 1150° C. This rough rolling end temperature range can be achieved by adjusting the heating temperature of the steel, retention between passes of rough rolling, thickness of the steel and the like. If the withstand load and the rolling torque of the rolling mill allow, the lower limit of the rough rolling end temperature may be at least 100° C. higher than the Ar3 transformation point. The thickness of the sheet bar may be any value as long as the product sheet (hot rolled steel sheet) has a desired thickness after finish rolling, and thus is not particularly limited. An appropriate sheet bar thickness is about 32 to 60 mm.


The sheet bar is then subjected to finish rolling in a tandem rolling mill to be formed into a hot rolled steel sheet.


Finish Rolling Start Temperature (Finishing Entry Temperature): 1100 to 850° C.

In finish rolling, rolling and recrystallization are repeated and refining of the austenite (γ) grains proceeds. When the finish rolling start temperature (finishing entry temperature) is decreased, working strain introduced by rolling tends to remain and grain refining of γ grains is easily achieved. When the finish rolling start temperature (finishing entry temperature) is less than 850° C., the temperature near the steel sheet surfaces in the finishing mill decreases to the Ar3 transformation temperature or less and a risk of ferrite generation increases. The generated ferrite forms ferrite grains stretched in the rolling direction as a result of the subsequent finish rolling and causes degradation of workability. In contrast, when the finish rolling start temperature (finishing entry temperature) exceeds 1100° C., the above-described γ grain refining effect brought about by finish rolling is decreased and it becomes difficult to obtain a hot rolled steel sheet having a desired mean crystal grain diameter of 15 μm or less. Accordingly, the finishing entry temperature (finish rolling start temperature) is preferably limited to 1100 to 850° C. and more preferably 1050 to 850° C.


Finish Rolling End Temperature (Finishing Delivery Temperature): 900 to 750° C.

If the finish rolling end temperature (finishing delivery temperature) exceeds 900° C., the work strain applied during finish rolling becomes insufficient, refining of the γ grains is not achieved, and thus, it becomes difficult for the hot rolled steel sheet to achieve a desired mean crystal grain diameter of 15 μm or less. In contrast, if the finish rolling end temperature (finishing delivery temperature) is less than 750° C., the temperature near the surfaces of the steel sheet in the finishing mill is equal to the Ar3 transformation point or less, ferrite grains stretched in the rolling direction are formed, ferrite grains form mixed grains, and the risk of degradation of workability is increased. Accordingly, the finishing delivery temperature (finish rolling end temperature) is preferably limited to 900 to 750° C. and more preferably 850 to 750° C.


More preferably, in the finish rolling discussed above, the total reduction of the finish rolling is 35 to 70%. If the total reduction is less than 35%, it is difficult to apply work strain sufficient for refining γ grains and it becomes difficult to obtain a hot rolled steel sheet having a desired mean crystal grain diameter. At a total reduction exceeding 70%, the with-stand load and rolling torque of the rolling mill may become insufficient in some cases and γ grains stretched and elongated in the rolling direction are formed, thereby forming elongated ferrite grains, and the risk of degradation of workability is increased. Accordingly, the total reduction of the finish rolling is preferably 35 to 70% and more preferably 40 to 70%.


Upon completion of finish rolling, a cooling step is performed. As the cooling step, two cooling methods are proposed: Cooling method (1) and cooling method (2).


Cooling Method (1)

In the cooling step, cooling of the hot rolled steel sheet is started immediately after completion of the finish rolling and the cooling is performed down to a coiling temperature such that the average cooling rate in the temperature range of 750 to 650° C. in terms of surface temperature is 20° C./s or less, the time taken for the temperature at the sheet thickness center to reach 650° C. is within 30 s, and the average cooling rate in the temperature range of 750 to 650° C. at the sheet thickness center is 4 to 15° C./s. The cooling end temperature is preferably in the range of the coiling temperature to 50° C. higher than the coiling temperature.


“Immediately after completion of the finish rolling” means within 10 s from the completion of the finish rolling. If cooling does not start within 10 s after the completion of the rolling, in other words, if the time the steel is retained at high temperature is long, grain growth proceeds and γ grains coarsen. Accordingly, cooling starts within 10 s and more preferably within 8 s after completion of the finish rolling.


Average Cooling Rate at Steel Sheet Surface: 20° C./s or Less

When the average cooling rate at the steel sheet surfaces exceeds 20° C./s, the regions near the steel sheet surfaces undergo a bainite generation region during cooling, resulting in formation of a bainite phase. Accordingly, the desired microstructure constituted of ferrite and the second phase cannot be formed, the desired second phase frequency cannot be obtained, the yield ratio is increased, and the desired low yield ratio in the column axis direction cannot be achieved when the steel sheet is cold-formed into a square column. Thus, the average cooling rate at steel sheet surfaces is preferably limited to 20° C./s or less and more preferably 4 to 18° C./s. The average cooling rate of the steel sheet surfaces discussed here is the average of 750 to 650° C.


Time Taken for the Temperature at the Sheet Thickness Center to Reach 650° C.: Within 35 s

If a cooling time for the temperature at the sheet thickness center to reach 650° C. is more than 35 s from the start of cooling, high temperature is retained before generation of a pearlite phase and thus crystal grains coarsen. As a result, the second phase frequency exceeds 0.42 and the desired hot rolled steel sheet toughness cannot be obtained. To further improve the toughness, it is preferable to control the time taken for the temperature at the sheet thickness center to reach 650° C. to 30 s or less. When the time is 30 s or less, the cold-formed square column can obtain a toughness of 150 J or more in terms of Charpy absorbed energy vE30 at a test temperature of −30° C.


Average Cooling Rate at Sheet Thickness Center: 4 to 15° C./s

If the average cooling rate at the sheet thickness center is less than 4° C./s, the frequency of ferrite grain generation is reduced, the ferrite crystal grains coarsen, and a hot rolled steel sheet having a desired mean crystal grain diameter of 15 μm or less cannot be obtained. In contrast, if the rate exceeds 15° C./s, formation of pearlite is suppressed and coarse bainite grains are generated. Hence, a hot rolled steel sheet having the desired mean crystal grain diameter cannot be obtained. Thus, it is preferable to limit the average cooling rate at the sheet thickness center to 4 to 15° C./s and more preferably 4.5 to 14° C./s. The average cooling rate at the steel sheet thickness center discussed here refers to the average of 750 to 650° C.


The cooling rate at the sheet thickness center is a value determined by heat-transfer calculation. After cooling, a coiling step is performed. In the coiling step, coiling is performed at a coiling temperature of 500 to 650° C. and the coiled sheet is then allowed to cool.


Coiling Temperature: 500 to 650° C.

At a coiling temperature less than 500° C., generation of pearlite is suppressed, the fraction of aggregated bainite grains with a large lath spacing mixing in is increased, the desired microstructure cannot be obtained, and the cold-formed square column cannot achieve the desired yield ratio and toughness. At a coiling temperature exceeding 650° C., pearlite transformation proceeds after coiling, resulting in such a problem as disturbance of the coil shape and the desired toughness cannot be obtained due to an excessively large mean grain diameter. Accordingly, the coiling temperature is preferably limited to 500 to 650° C. and more preferably 520 to 630° C.


Cooling Method (2)

The cooling step is a step including sequentially performing, immediately after completion of finish rolling, first cooling, second cooling, and third cooling.


Upon start of the cooling of the hot rolled steel sheet, first cooling is performed first. The temperature used in the cooling step is a value (temperature) obtained by heat-transfer calculation.


In the first cooling, cooling is performed so that the cooling end temperature is 550° C. or more in terms of surface temperature.


If the cooling end temperature of the first cooling is less than 550° C., the regions near the steel sheet surfaces, in particular, undergo a bainite generation region and a bainite phase is formed. Thus, the desired microstructure constituted of ferrite and the second phase cannot be formed. Thus, the desired second phase frequency cannot be obtained, the yield ratio is increased, and the desired low yield ratio in the column axis direction cannot be achieved when the sheet is formed into a cold-formed square column. Due to these reasons, the cooling end temperature of the first cooling is limited to 550° C. or more. As long as the cooling end temperature is 550° C. or more, the cooling rate during the cooling is not particularly limited. As a result, formation of bainite in the surface layers can be stably avoided and the desired hot rolled microstructure can be stably formed.


After completion of the first cooling, second cooling is performed.


Second cooling is air cooling for 3 to 15 s after completion of the first cooling. In the second cooling, the sheet is retained in the high-temperature ferrite generation region to suppress generation of bainite. If the air cooling time is less than 3 s, the risk that the sheet would undergo the bainite generation region in the subsequent cooling (third cooling) becomes higher. If the air cooling time is longer than 15 s, the ferrite grains coarsen. Accordingly, the air cooing time in the second cooling is limited to 3 to 15 s. Preferably, the air cooling time is 4 to 13 s.


After completion of the second cooling, third cooling is performed.


In the third cooling, cooling is performed to a temperature of 650° C. or less at an average cooling rate of 4 to 15° C./s at 750 to 650° C. in terms of a sheet thickness center temperature.


If the average cooling rate at the steel sheet thickness center is less than 4° C./s, the frequency of ferrite grain generation is decreased, ferrite crystal grains coarsen, and a hot rolled steel sheet having a desired mean crystal grain diameter of 15 μm or less cannot be obtained. In contrast, at a rate exceeding 15° C./s, generation of pearlite is suppressed and coarse bainite grains are generated. Thus, a hot rolled steel sheet having a desired mean crystal grain diameter cannot be obtained. Accordingly, the average cooling rate at the sheet thickness center is preferably limited to 4 to 15° C./s and more preferably 4.5 to 14° C./s. The average cooling rate at the steel sheet thickness center discussed here refers to the average of 750 to 650° C.


In the cooling step, the above-described first cooling, second cooling, and third cooling are sequentially performed such that the time taken for the temperature at the sheet thickness center to reach 650° C. from the start of cooling is within 35 s. If the cooling time takes longer than 35 s for the temperature at the sheet thickness center to reach 650° C. from the start of cooling, high temperature is retained before generation of a pearlite phase, crystal grains coarsen, the second phase frequency exceeds 0.42, and thus the desired hot rolled steel sheet toughness cannot be obtained. To further improve the toughness, the time taken for the temperature at the sheet thickness center to reach 650° C. is preferably 30 s or less. When the time is 30 s or less, the toughness of the cold-formed square steel sheet can be adjusted to 150 J or more in terms of Charpy absorbed energy vE−30 at a test temperature of −30° C.


After completion of the third cooling, fourth cooling is preferably performed if needed. Fourth cooling is performed to coil the steel sheet accurately at a desired coiling temperature. After completion of the third cooling, it is preferable to measure the temperature of the steel sheet and appropriately adjust the water-cooling time so that the desired coiling temperature can be achieved. If the desired coiling temperature is not obtained by fourth cooling, fifth cooling (water cooling) may be performed.


After completion of cooling, a coiling step is performed.


In the coiling step, coiling is performed at a coiling temperature of 500 to 650° C., followed by cooling in the air.


Coiling Temperature: 500 to 650° C.

At a coiling temperature less than 500° C., generation of pearlite is suppressed, the fraction of aggregated bainite grains with large lath spacing mixing in is high, the desired microstructure cannot be obtained, and a cold-formed square column cannot achieve the desired yield ratio and toughness. If the coiling temperature exceeds 650° C., pearlite transformation proceeds after coiling and thus such a problem as coil shape is disrupted. Thus, the coiling temperature is preferably limited to 500 to 650° C. and more preferably 520 to 630° C.


Our methods will be further described in detail by using Examples below.


Examples

Each of molten steels having compositions indicated in Table 1 was produced with a converter and cast into a slab by a continuous casting method (steel: 215 mm in thickness). The slab (steel) was heated to the heating temperature indicated in Tables 2 and 3, and subjected to a hot rolling step, a cooling step, and a coiling step indicated in Tables 2 and 3. As a result, a hot rolled steel sheet having a thickness of 12 to 25 mm was obtained. The hot rolled steel sheet was used as a raw material and subjected to cold roll forming to form a round steel pipe. The round steel pipe was subjected to cold roll forming to form a square column (250 to 550 mm square).


A test specimen was taken from the hot rolled steel sheet and subjected to microstructure observation, tensile test, and impact test. The test procedures were as follows.


(1) Microstructural Observation

A microstructure observation specimen was taken from the hot rolled steel sheet so that the observation surface was the L cross section. The specimen was polished and etched with nital. The microstructure at a ¼ t sheet thickness position was observed with an optical microscope (magnitude: 500) or a scanning electron microscope (magnitude: 500) and was photographed. The obtained microstructure image was analyzed with an image analyzer to determine the types of the primary phase and the second phase and the mean crystal grain diameter of the primary phase and the second phase together was calculated by an intercept method.


As shown in FIG. 1, six line segments each 125 μm in length were drawn on the obtained microstructure image in the rolling direction and another six in the sheet thickness direction. The number of crystal grains of each phase intersecting these line segments was counted. Then the second phase frequency defined by the following equation was calculated based on the numbers of crystal grains of the respective phases intersecting the line segments:





Second phase frequency=(Number of second phase grains intersecting line segments)/(Total number of primary phase grains and second phase grains intersecting line segments).


(2) Tensile Test

A JIS 5 tensile test specimen was taken from the resulting hot rolled steel sheet so that the tensile direction was the rolling direction. A tensile test was performed in accordance with the provisions of JIS Z 2241 and the yield strength and the tensile strength were measured. The yield ratio (%) defined by (yield strength)/(tensile strength) was calculated.


(3) Impact Test

V-notched specimens were taken from the ¼ t sheet thickness position of the hot rolled steel sheet so that the longitudinal direction of the specimen was the rolling direction and subjected to a Charpy impact test in accordance with the provisions of JIS Z 2242 at a test temperature of 0° C. and −30° C. to determine the absorbed energy (J). The number of specimens for each test was 3.


A specimen was taken from a flat portion of the resulting square column and subjected to a tensile test and an impact test to evaluate the yield ratio and toughness.


(4) Square Column Tensile Test

A JIS 5 tensile test specimen was taken from a flat portion of the square column so that the tensile direction was the column longitudinal direction and subjected to a tensile test in accordance with the provisions of JIS Z 2241 to measure the yield strength and tensile strength. Then the yield ratio (%) defined by (yield strength)/(tensile strength) was calculated.


(5) Square Column Impact Test

V-notched specimens were taken from a ¼ t thickness position of a flat portion of the square column so that the longitudinal direction of the specimen was the longitudinal direction of the column and subjected to a Charpy impact test in accordance with the provisions of JIS Z 2242 at a test temperature of 0° C. and −30° C. to determine the absorbed energy (J). The number of specimens for each test was 3.


The results are indicated in Tables 4 and 5.


In each of our examples, a square column manufactured through cold forming satisfied the desired tensile properties, namely, a yield strength of 295 MPa or more, a tensile strength of 400 MPa or more, and a yield ratio of 80% or less, at a flat portion of the square column. Moreover, the absorbed energy vE0 (J) in a Charpy impact test at a test temperature of 0° C. was 150 J or more and the absorbed energy vE−30 (J) in a Charpy impact test at a test temperature of −30° C. was 150 J or more, showing high toughness. Thus, a hot rolled steel sheet having both the high toughness and the desired tensile properties was obtained. In contrast, all Comparative Examples outside our range fail to satisfy the desired low yield ratio, the desired high toughness, or both the desired low yield ratio and high toughness in the square column.











TABLE 1







Steel
Chemical composition (mass %)


















No.
C
Si
Mn
P
S
Al
N
Nb, Ti, V
B
Note





A
0.16
0.01
0.76
0.017
0.0025
0.030
0.0040


Example


B
0.09
0.02
1.35
0.018
0.0033
0.031
0.0035


Example


C
0.15
0.18
0.43
0.018
0.0030
0.040
0.0041


Example


D
0.12
0.01
1.03
0.015
0.0028
0.029
0.0040


Example



E


0.06

0.15
1.45
0.019
0.0022
0.033
0.0035


Comparative












Example



F


0.21

0.01
0.58
0.021
0.0029
0.035
0.0034


Comparative












Example



G

0.16
0.01

0.21

0.017
0.0031
0.039
0.0042


Comparative












Example



H

0.16
0.02

1.85

0.015
0.0026
0.031
0.0031


Comparative












Example


I
0.11
0.01
0.85
0.015
0.0027
0.031
0.0029
Nb: 0.008

Example


J
0.15
0.01
0.65
0.016
0.0035
0.026
0.0035
Ti: 0.016

Example


K
0.16
0.01
0.50
0.017
0.0045
0.029
0.0033
V: 0.031

Example


L
0.16
0.01
0.76
0.015
0.0031
0.043
0.0040

B: 0.0004
Example



M

0.11
0.02
0.75
0.020
0.0027
0.033
0.0042

Nb: 0.029


Comparative












Example



N

0.16
0.02
0.50
0.019
0.0039
0.029
0.0028

Ti: 0.045


Comparative












Example


R
0.11
0.18
0.35
0.014
0.0036
0.039
0.0037
Nb: 0.010

Example


S
0.13
0.25
0.30
0.017
0.0033
0.045
0.0043
Ti: 0.015

Example


T
0.12
0.19
0.39
0.016
0.0044
0.031
0.0027
V: 0.042

Example


U
0.16
0.23
0.43
0.017
0.0034
0.042
0.0041

B: 0.0006
Example


V
0.16
0.01
0.70
0.016
0.0025
0.032
0.0040
Ti: 0.019
B: 0.0005
Example


















TABLE 2









Hot rolling step












Rough rolling
Finish rolling















Steel

Heating
End
Sheet bar
Start
End
Total



sheet
Steel
temperature
temperature
thickness
temperature
temperature
reduction
Product sheet


No.
No.
(° C.)
(° C.)
(mm)
(° C.)
(° C.)
(%)
thickness (mm)





1
A
1200
1025
42
950
780
62
16


2
A
1180
1010
54
940
780
65
19


3
A
1200
1015
58
960
780
57
25


4
A

1350


1190

42

1120

900
62
16


5
A
1250
1150
42
1100 

950

62
16


6
A
1200
1025
25
950
780
36
16


7
A
1250
1150
42
1050 
890
62
16


8
A
1200
1025
42
950
780
62
16


9
A
1200
1025
42
950
780
62
16


10
A
1200
1025
38
950
780
68
16


11
A
1200
1025
42
950
780
62
16


12
A
1200
1025
42
950
780
62
16


13
B
1250
1075
54
1050 
790
65
19


14
C
1150
 975
58
920
790
57
25


15
D
1120
 975
58
930
800
57
25


16

E

1200
1025
42
950
780
62
16


17

F

1200
1025
42
950
780
62
16


18

G

1200
1025
42
950
780
62
16


19

H

1200
1025
42
950
780
71
12


20
I
1200
1025
58
960
780
57
25


21
J
1200
1025
58
960
780
57
25


22
K
1200
1025
58
960
780
57
25


23
L
1210
1030
58
960
780
57
25


24
M
1220
1030
58
960
780
57
25


25
N
1200
1025
58
960
780
57
25


26
R
1210
1025
54
960
780
65
19


27
S
1220
1030
54
970
790
65
19


28
T
1200
1025
54
990
800
65
19


29
U
1210
1025
54
950
790
65
19


30
V
1190
1015
54
960
810
65
19













Cooling step













Average cooling






rate
Cooling time



(° C./s)*
(s)
Coiling step















Steel
Cooling

Sheet
Start of
Coiling




sheet
start

thickness
cooling
temperature



No.
time (s)
Surface
center
to 650° C.**
(° C.)
Notes







 1
2
16
6.0
25
600
Example



 2
3
12
5.2
29
600
Example



 3
3
20
13.0 
29
600
Example



 4
3
13
4.8
28
600
Comparative Example



 5
3
13
4.8

41

600
Comparative Example



 6
2
13
4.8
28
600
Example



 7

15

13
4.8

43

600
Comparative Example



 8
2

40


17.0

25
600
Comparative Example



 9
3
11

3.3


37

600
Comparative Example



10
2
13

3.4

28
600
Comparative Example



11
2
20
15.0 
20

450

Comparative Example



12
2
14
5.5

1500


660

Comparative Example



13
3
12
4.2
30
550
Example



14
3
19
4.6
29
630
Example



15
3
14
4.0
30
580
Example



16
2
20
7.0
25
550
Comparative Example



17
2
16
6.0
25
600
Comparative Example



18
2
16
6.0
25
600
Comparative Example



19
2
20
8.0
20
500
Comparative Example



20
3
15
4.5
33
600
Example



21
3
15
4.5
33
600
Example



22
3
15
4.5
33
600
Example



23
3
15
4.5
33
600
Example



24
3
15
4.5
33
600
Comparative Example



25
3
15
4.5
33
600
Comparative Example



26
3
14
5.0
30
580
Example



27
3
12
5.3
28
590
Example



28
3
13
5.1
29
600
Example



29
3
14
5.0
32
600
Example



30
3
15
5.5
31
570
Example







*Average in the temperature range of 750 to 650° C.



**Temperature at sheet thickness center
















TABLE 3









Hot rolling step
Cooling step











Finish rolling

First cooing














Rough rolling

Product

Average



















Steel

Heating
End
Sheet bar
Start
End
Total
sheet
Cooling
cooling
Cooling end


sheet
Steel
temperature
temperature
thickness
temperature
temperature
reduction
thickness
start
rate*
temperature**


No.
No.
(° C.)
(° C.)
(mm)
(° C.)
(° C.)
(%)
(mm)
time (s)
(° C./s)
(° C.)





31
A
1200
1025
42
950
780
62
16
2
19
620


32
A
1180
1010
54
940
780
65
19
3
15
650


33
A
1200
1015
58
960
780
57
25
3
19
560


34
A

1350


1190

42
1120
900
62
16
3
20
610


35
A
1250
1150
42
1100

950

62
16
3
15
560


36
A
1200
1025
25
950
780
36
16
2
17
620


37
A
1250
1150
42
1050
890
62
16

15

17
630


38
A
1200
1025
42
950
780
62
16
2
14

490



39
A
1200
1025
42
950
780
62
16
3
19
615


40
A
1200
1025
38
950
780
68
12
2
20
590


41
A
1200
1025
42
950
780
62
16
2
18
620


42
A
1200
1025
42
950
780
62
16
2
18
600


43
B
1250
1075
54
1050
790
65
19
3
12
570


44
C
1150
 975
58
920
790
57
25
3
18
600


45
D
1120
 975
58
930
800
57
25
3
19
620


46

E

1200
1025
42
950
780
62
16
2
14
560


47

F

1200
1025
42
950
780
62
16
2
13
600


48

G

1200
1025
42
950
780
62
16
2
20
620


49

H

1200
1025
42
950
780
71
12
2
12
660


50
I
1200
1025
58
1025
780
57
25
3
19
600


51
J
1200
1025
58
1025
780
57
25
3
20
570


52
K
1200
1025
58
1025
780
57
25
3
15
600


53
L
1210
1030
58
1030
780
57
25
3
17
620


54
M
1200
1030
58
1030
780
57
25
3
17
560


55
N
1200
1025
58
1025
780
57
25
3
15
590


56
R
1210
1025
54
960
780
65
19
3
16
640


57
S
1220
1030
54
970
790
65
19
3
16
610


58
T
1200
1025
54
990
800
65
19
3
17
570


59
U
1150
1000
54
950
790
65
19
3
15
600


60
V
1190
1015
54
960
810
65
19
3
17
620


















Third
Cooling






Second
cooling
time
Fourth cooling
Coiling


















cooling
Average
Start of
Whether


step




Steel
Air
cooling
cooling
fourth
Air
Water
Coiling



sheet
cooling
rate***
to 650° C.****
cooling is
cooling
cooling
temperature



No.
time (s)
(° C./s)
(s)
performed
time (s)
time (s)
(° C.)
Notes







31
10 
6.0
27
Yes
17
3
600
Example



32
9
5.2
28
Yes
15
3
600
Example



33
8
13.0 
23
No


610
Example



34
9
4.8

59

Yes
16
2
600
Comparative











Example



35

1

15.0 

84

No


620
Comparative











Example



36
10 
5.5
29
Yes
17
2
600
Example



37
15 
5.1

62

No


620
Comparative











Example



38
10 
14.0 
35
No


590
Comparative











Example



39
8

3.3

32
Yes
15

4

580
Comparative











Example



40
8

22.0

20
Yes
13
6
590
Comparative











Example



41
10 
15.0 
22
No



450

Comparative











Example



42
8
5.5

1600

No



670

Comparative











Example



43
6
4.2
33
Yes
12
2
550
Example



44
8
4.6
30
No


630
Example



45
11 
4.0
35
Yes
10
4
580
Example



46
7
7.0
30
Yes
17
3
550
Comparative











Example



47
8
6.0
31
No


600
Comparative











Example



48
7
6.0
23
No


600
Comparative











Example



49
10 
8.0
26
Yes
17
3
500
Comparative











Example



50
8
7.7
27
Yes
13
4
550
Example



51
7
8.8
28
Yes
14
3
570
Example



52
6
11.1 
31
No


600
Example



53
7
7.8
26
Yes
12
5
590
Example



54
7
8.8
31
No


620
Comparative











Example



55
8
10.4 
33
Yes
13
4
590
Comparative











Example



56
9
5.3
27
Yes
15
3
590
Example



57
9
5.4
26
No


580
Example



58
6
5.1
29
Yes
12
2
560
Example



59
6
8.0
33
Yes
12
1
600
Example



60
7
7.9
28
Yes
12
5
570
Example







*Average in the temperature range of 750 to 650° C. in terms of surface temperature



**Surface temperature



***Average in the temperature range of 750 to 650° C. in terms of sheet thickness center temperature



****Sheet thickness center temperature

















TABLE 4









Hot rolled steel sheet
Flat portion of square column














Microstructure*
Tensile properties

Tensile properties
























Mean crystal

Yield

Yield

Yield

Yield




Steel


grain
Second
Strength
Tensile
ratio
Toughness
strength
Tensile
ratio
Toughness






















sheet
Steel

diameter
phase
YS
strength
YR
vE0
vE−30
YS
strength
YR
vE0
vE−30



No.
No.
Type**
(μm)***
frequency
(MPa)
TS (MPa)
(%)
(J)
(J)
(MPa)
TS (MPa)
(%)
(J)
(J)
Notes

























1
A
F + P
 9.5
0.25
291
450
65
315
260
365
477
77
227
172
Example


2
A
F + P
 9.8
0.27
302
446
68
300
237
375
467
80
242
178
Example


3
A
F + P +
 8.9
0.32
305
455
67
265
200
378
493
77
228
162
Example




B


4
A
F + P

19.2

0.36
265
444
60
187

152

341
460
74
 62
27
Comparative

















Example


5
A
F + P

15.7


0.49

268
445
60

135

67
344
463
74
124
56
Comparative

















Example


6
A
F + P
14.9
0.35
277
445
62
245
185
352
462
76
223
150
Example


7
A
F + P

18.5


0.52

255
442
58

125

29
331
452
73
108
12
Comparative

















Example


8
A
B

17.5

0.12
397
462

86

347
332
465
512

91

183
166
Comparative

















Example


9
A
F + P

17.5


0.43

271
447
61
186
84
346
469
74
154
52
Comparative

















Example


10
A
F + P
15.0

0.46

282
449
63

153

66
356
475
75
116
29
Comparative

















Example


11
A
B
 6.4
0.08
406
461

88

365
360
459
512

90

260
151
Comparative

















Example


12
A
F + P

20.2


0.48

262
439
60

126

45
338
445
76
 96
15
Comparative

















Example


13
B
F + P
13.8
0.32
294
448
66
273
206
367
471
78
252
185
Example


14
C
F + P
11.2
0.34
306
450
68
252
182
379
479
79
223
152
Example


15
D
F + P
14.9
0.30
316
448
71
284
228
358
472
76
230
174
Example


16

E

F + P
 6.3
0.09
377
457

82

378
375
460
499

92

199
195
Comparative

















Example


17

F

F + P
10.2

0.45

312
455
69

179

85
385
492
78
126
32
Comparative

















Example


18

G

F + P
 9.5
0.25
228
423
54
317
273
305
395
77
220
175
Comparative

















Example


19

H

F + P
 6.2
0.40
395
460

86

216

148

463
509

91

 93
25
Comparative

















Example


20
I
F + P
10.8
0.25
327
456
72
235
197
371
495
75
193
155
Example


21
J
F + P
11.4
0.33
330
458
74
275
205
386
502
77
246
176
Example


22
K
F + P
12.7
0.39
337
456
72
225
205
393
497
79
186
166
Example


23
L
F + P
11.9
0.33
313
453
69
256
239
386
487
79
199
182
Example


24
M
F + P
 6.1
0.16
430
532

81

323
298
506
555

91

289
269
Comparative

















Example


25
N
F + P
 6.5
0.11
445
513

87

343
302
510
552

92

301
279
Comparative

















Example


26
R
F + P
 9.3
0.26
343
473
73
260
218
397
498
80
227
178
Example


27
S
F + P
 9.1
0.24
355
477
74
278
216
400
502
80
229
173
Example


28
T
F + P
11.8
0.37
343
467
73
263
234
412
490
79
226
191
Example


29
U
F + P
10.8
0.33
333
442
75
280
245
365
470
78
244
201
Example


30
V
F + P
 7.4
0.32
349
485
72
297
253
407
511
80
250
202
Example





*¼ t sheet thickness position


**F: ferrite, P: pearlite, B: bainite


***Mean grain diameter of all crystal grains















TABLE 5









Hot rolled steel sheet











Microstructure*
Tensile properties
















Steel


Mean crystal
Second
Yield
Tensile
Yield



sheet
Steel

grain diameter
phase
Strength
strength
ratio
Toughness
















No.
No.
Type**
(μm)***
frequency
YS (MPa)
TS (MPa)
YR (%)
vE0 (J)
vE−30 (J)





31
A
F + P
 9.0
0.24
290
448
65
316
260


32
A
F + P
 9.2
0.23
300
446
67
303
238


33
A
F + P + B
 8.2
0.24
303
450
67
268
202


34
A
F + P

18.4

0.36
261
442
59
190
153


35
A
F + P

15.3


0.54

266
443
60
137
69


36
A
F + P
14.1
0.30
274
442
62
247
188


37
A
F + P

18.0


0.53

254
442
58
125
31


38
A
B

16.7

0.18
394
457
86
348
334


39
A
F + P

17.1


0.49

267
445
60
188
86


40
A
F + P
14.7

0.55

261
445
59
155
68


41
A
B
 5.5
0.04
404
460
88
368
361


42
A
F + P

20.1


0.53

258
435
59
127
46


43
B
F + P
12.9
0.25
293
447
65
274
207


44
C
F + P
10.8
0.30
301
448
67
252
182


45
D
F + P
14.6
0.22
311
446
70
286
228


46

E

F + P
 6.3
0.17
374
455
82
378
377


47

F

F + P
 9.7

0.53

308
453
68
182
88


48

G

F + P
 9.0
0.22
225
422
53
319
275


49

H

F + P
 6.2
0.37
390
455
86
218
150


50
I
F + P
10.5
0.24
325
453
72
236
198


51
J
F + P
11.0
0.32
327
456
72
277
205


52
K
F + P
12.6
0.38
335
452
74
225
206


53
L
F + P
11.7
0.35
313
449
70
258
240


54

M

F + P
 6.0
0.15
428
529
81
323
300


55

N

F + P
 6.2
0.11
442
511
87
345
304


56
R
F + P
 9.0
0.25
335
463
72
251
205


57
S
F + P
 8.9
0.23
347
467
74
268
209


58
T
F + P
12.9
0.38
335
457
73
254
225


59
U
F + P
11.2
0.34
325
432
75
272
236


60
V
F + P
 7.6
0.33
341
475
72
289
245













Flat portion of square column











Tensile properties















Steel
Yield
Tensile
Yield
Toughness
















sheet
strength
strength
ratio
vE0
vE−30




No.
YS (MPa)
TS (MPa)
YR (%)
(J)
(J)
Notes







31
365
478
76
228
173
Example



32
376
469
80
244
179
Example



33
379
495
77
229
162
Example



34
341
460
74
64
28
Comparative Example



35
343
464
74
125
57
Comparative Example



36
350
464
76
225
150
Example



37
330
454
73
108
13
Comparative Example



38
464
514

90

185
169
Comparative Example



39
345
470
73
156
52
Comparative Example



40
437
485

90

116
149
Comparative Example



41
457
513

89

261
152
Comparative Example



42
336
445
76
97
15
Comparative Example



43
378
472
80
254
187
Example



44
379
480
79
224
153
Example



45
374
474
79
232
176
Example



46
462
500

92

200
195
Comparative Example



47
386
493
78
126
33
Comparative Example



48
305
396
77
220
176
Comparative Example



49
463
509

91

96
27
Comparative Example



50
373
496
75
193
155
Example



51
389
503
77
247
178
Example



52
394
499
79
187
167
Example



53
386
490
79
200
182
Example



54
509
558
91
291
269
Comparative Example



55
511
552
92
302
280
Comparative Example



56
395
507
78
221
156
Example



57
398
499
80
237
169
Example



58
379
488
78
220
152
Example



59
365
487
75
232
171
Example



60
430
508
85
245
188
Example







*¼ t sheet thickness position



**F: ferrite, P: pearlite, B: bainite



***Mean grain diameter of all crystal grains





Claims
  • 1. A method of manufacturing a hot rolled steel sheet for a square column for building structural members, comprising a hot rolling step, a cooling step, and a coiling step performed on a steel to form a hot rolled steel sheet, wherein the steel has a composition containing, in terms of % by mass,
  • 2. A method of manufacturing a hot rolled steel sheet for a square column for building structural members, comprising a hot rolling step, a cooling step, and a coiling step performed on a steel to form a hot rolled steel sheet, wherein the steel has a composition containing, in terms of % by mass,
  • 3. The method according to claim 1, wherein a total reduction of the finish rolling is 35 to 70%.
  • 4. The method according to claim 1, wherein the composition of the steel further comprises Si: less than 0.4% by mass.
  • 5. The method according to claim 1, wherein the composition of the steel further comprises at least one selected from Nb: 0.015% or less, Ti: 0.030% or less, and V: 0.070% or less in terms of % by mass.
  • 6. The method according to claim 1, wherein the composition of the steel further comprises B: 0.008% by mass or less.
  • 7. The method according to claim 2, wherein fourth cooling is performed after completion of the third cooling in addition to the three stages of the cooling.
  • 8. The method according to claim 2, wherein a total reduction of the finish rolling is 35 to 70%.
  • 9. The method according to claim 2, wherein the composition of the steel further comprises Si: less than 0.4% by mass.
  • 10. The method according to claim 2, wherein the composition of the steel further comprises at least one selected from Nb: 0.015% or less, Ti: 0.030% or less, and V: 0.070% or less in terms of % by mass.
  • 11. The method according to claim 2, wherein the composition of the steel further comprises B: 0.008% by mass or less.
Divisions (1)
Number Date Country
Parent 14391899 Oct 2014 US
Child 15620957 US