KR20150075580A - Complex steel structure and method of manufacturing the same - Google Patents
Complex steel structure and method of manufacturing the same Download PDFInfo
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- KR20150075580A KR20150075580A KR1020130163670A KR20130163670A KR20150075580A KR 20150075580 A KR20150075580 A KR 20150075580A KR 1020130163670 A KR1020130163670 A KR 1020130163670A KR 20130163670 A KR20130163670 A KR 20130163670A KR 20150075580 A KR20150075580 A KR 20150075580A
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- steel
- steel structure
- structural member
- heating
- cooling
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/08—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for tubular bodies or pipes
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Heat Treatment Of Articles (AREA)
Abstract
The present invention relates to a composite steel structure capable of differently controlling the mechanical properties of an outer surface of a steel structure, and a method for manufacturing the composite steel structure, comprising the steps of: preparing a steel structural member having a hollow; heat treating the steel structural member; Forming a martensite structure by performing a cooling process on the outer side of the heat treated steel structure, and performing a heating process on the inner side of the heat treated steel structure to form a structure more ductile than the martensite structure, Wherein the heating step is performed simultaneously, and a method of manufacturing the same.
Description
TECHNICAL FIELD The present invention relates to a steel structural member, and more particularly, to a composite steel structural member and a manufacturing method thereof.
Generally, the collision members such as door beams, seat frames, bumper bins in the automobile field, high-strength heat treatment products in the field of API oil pipeline, high-strength structural materials and high-pressure pressure tubes in the construction field, steel structures applied to earthquake- It is usual that high pressure acts on the steel structure material buried in the ground because the high pressure crude oil or gas flows mainly in the steel structure material. In order to use steel structural materials in such polar regions and cold regions, such steel materials must have high strength and low temperature toughness, and also require high deformability due to earthquake and other crustal changes have.
However, such a conventional composite steel structure material and a manufacturing method thereof have a problem of high strength and brittleness due to insufficient ductility of the steel structure material.
It is an object of the present invention to provide a composite steel structural member capable of differently controlling the mechanical properties of an outer surface of a steel structural member and a method of manufacturing the same. However, these problems are exemplary and do not limit the scope of the present invention.
According to one aspect of the present invention, there is provided a method of manufacturing a steel structure comprising the steps of preparing a steel structural material having a hollow, heat treating the steel structural material, cooling the outer side of the heat treated steel structural material to form a martensitic structure, Wherein the cooling step and the heating step are simultaneously performed by performing a heating process on the inner side of the steel structure material to form a ductile structure than the martensite structure.
In the method for manufacturing the composite steel structure material, the cooling step and the heating step may be performed simultaneously.
In the method for manufacturing the composite steel structure, the heating process is performed using a heating member, and the heating process can be inserted into the hollow of the heat treated steel structure to heat the inside portion.
In the method for manufacturing the composite steel structure, the heating member may be inserted into the hollow of the heat treated steel structure member during the cooling process.
In the method for manufacturing the composite steel structure, the cooling process may include a water quenching hardening process.
In the method for manufacturing the composite steel structural member, the steel structural member may include a steel pipe.
In the method of manufacturing the composite steel structure material, the structure that is more ductile than the martensitic structure may include bainite or pearlite.
In the method for manufacturing the composite steel structure, the heat treatment may include a high frequency heat treatment.
A method of manufacturing a composite steel structure according to another aspect of the present invention includes the steps of preparing a steel structural member having a hollow structure, heat treating the steel structural member to form an austenitic structure, Forming a martensite structure by performing a first cooling process at a speed lower than the first cooling rate and a second cooling process at a second cooling rate lower than the first cooling rate with respect to the inner side of the heat treated steel structure to form a bainite or perlite structure And the first cooling step and the second cooling step may be performed simultaneously.
According to still another aspect of the present invention, there is provided a composite steel structural member implemented by the above-described method of manufacturing a composite steel structural member.
According to one embodiment of the present invention as described above, a composite steel structural member capable of differently controlling the mechanical properties of the outer surface in the steel structural member and the manufacturing method thereof can be implemented. Of course, the scope of the present invention is not limited by these effects.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a flow chart schematically showing a method of manufacturing a composite steel structural member according to an embodiment of the present invention; FIG.
2 is a view schematically showing a method of manufacturing a composite steel structural member according to an embodiment of the present invention.
3A is a cross-sectional view schematically showing a heating member of a composite steel structural member according to an embodiment of the present invention.
3B is a cross-sectional view schematically showing a heating member of a composite steel structural member according to another embodiment of the present invention.
3C is a cross-sectional view schematically showing a heating member of a composite steel structural member according to another embodiment of the present invention.
FIG. 3D is a cross-sectional view schematically showing a heating member of a composite steel structural member according to another embodiment of the present invention. FIG.
4 is a cross-sectional view schematically showing a composite steel structure formed by a method of manufacturing a composite steel structural member according to embodiments of the present invention.
Hereinafter, embodiments of the present invention will be described in detail with reference to the accompanying drawings. It should be understood, however, that the invention is not limited to the disclosed embodiments, but may be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, Is provided to fully inform the user. Also, for convenience of explanation, the components may be exaggerated or reduced in size.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a flow chart schematically showing a method of manufacturing a composite steel structural member according to an embodiment of the present invention; FIG.
Referring to FIG. 1, a composite steel structural member according to an embodiment of the present invention and a method of manufacturing the same include a step S10 of preparing a steel structural member having a hollow (100 in FIG. 3), a steel structural member (100 in FIG. (S30) of performing a cooling process on the outer side portion (10 of FIG. 3) of the heat treated steel material (100 of FIG. 3) and the inner side portion of the heat treated steel material (S40 in FIG. 3). For example, a steel structure member (100 in Fig. 3) is prepared, heat treatment is applied to the prepared steel structure member (100 in Fig. 3), and then the outer side portion including the outer surface of the heat treated steel structure member (10 in Fig. 3) is subjected to a cooling process to form a martensitic structure (40 in Fig. 4), and the inner portion (20 in Fig. 3) including the inner surface of the heat treated steel structural member A heating process can be performed to form a structure superior in ductility to the martensitic structure (40 in Fig. 4). The inner portion (20 in Fig. 3) of the steel structural member (100 in Fig. 3) is a surface defining a hollow (30 in Fig. 3) formed inside the steel structural member (100 in Fig. 3), for example.
The structure having superior ductility than the martensitic structure (40 in Fig. 4) may include, for example, bainite or pearlite structure (50 in Fig. 4).
The heat treatment may include, for example, a high frequency heat treatment, and the cooling step may include, for example, water quenching and the like.
In addition, the
FIG. 2 is a schematic view showing a method of manufacturing a composite steel structural member according to an embodiment of the present invention, and FIGS. 3A, 3B, 3C and 3D are views showing a method of heating a composite steel structural member according to an embodiment of the present invention Sectional view schematically showing the member.
2 and 3, the heating process is performed using the
A method of manufacturing a composite steel structure according to embodiments of the present invention includes the steps of performing a cooling process S30 on the
The cooling step S30 of the
For example, after the cooling process is performed on the
4 is a cross-sectional view schematically showing a composite steel structure formed by a method of manufacturing a composite steel structural member according to embodiments of the present invention.
2 to 4, a composite steel structural member according to embodiments of the present invention and a steel
For example, when the steel
For example, in the case of vacancy steel (0.8% C steel), at constant temperature transformation curves (S curves) showing the time at which transformation begins and ends, pearlite is formed by constant temperature transformation over the nose temperature At constant temperature below the nose, bainite is formed. When the vacant steel is cooled from 850 ° C to 750 ° C and kept at this temperature, no transformation occurs. However, if the pellet is cooled to 650 ° C and maintained at a constant temperature, pearlite transformation starts after 1 second and transformation is completed within 10 seconds. As the pearlite formation temperature is lowered, the layered pearlite becomes finer and the structure hardens further.
On the other hand, if the vacant steel is subjected to constant temperature transformation at a temperature of about 550 DEG C or lower, bainite starts to be formed. It is assumed that the formation of bainite starts from the formation of ferrite nuclei in the austenite grain boundaries.
Both pearlite and bainite are composed of ferrite and cementite, but pearlite shows a layered structure in which the two phases are alternately repeated, and bainite shows a shape close to the bed. The pearlite formed at a relatively high temperature in the pearlite forming temperature range is coarse, and the pearlite formed at a relatively low temperature is fine. The upper bainite (upper bainite) formed at a temperature in the range of 350 to 550 ° C precipitates the cementite around the ferrite, while the lower part of the bainite formed at the temperature range of 250 to 350 ° C In bainite (lower bay knit), cementite is precipitated in the ferrite.
However, according to embodiments of the present invention, the composite steel structural members and the manufacturing method thereof are not limited thereto. For example, the composite steel structural members and the manufacturing method thereof may include boron steel (0.25% C steel) have.
According to another aspect of the present invention, there is provided a method of manufacturing a composite steel structural member, comprising the steps of: preparing a steel
According to the composite steel structural member and the manufacturing method thereof according to the embodiments of the present invention described above, for example, a
The mechanical strength of the
In addition, the mechanical properties of the inner and outer portions of the metal can be adjusted to produce a product of hybrid structure. The manufactured
While the present invention has been described with reference to exemplary embodiments, it is to be understood that the invention is not limited to the disclosed exemplary embodiments, but, on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the invention. Accordingly, the true scope of the present invention should be determined by the technical idea of the appended claims.
10:
20: medial side
30: hollow
40: Martensite structure
50: Bainite or pearlite structure
100: Steel structural member
110: heating member
Claims (10)
Heat treating the steel structure material;
Performing a cooling process on the outer side of the heat treated steel structure to form a martensite structure; And
Performing a heating process on the inner side of the heat treated steel structure to form a structure more ductile than the martensite structure;
Lt; / RTI >
Wherein the cooling step and the heating step are performed simultaneously.
Wherein the cooling step and the heating step are performed simultaneously.
Wherein the heating process is performed using a heating member and is inserted into the hollow of the heat treated steel structure to heat the inside portion.
Wherein the heating member is inserted into the hollow of the heat treated steel structure member during the cooling process.
Wherein the cooling process comprises water quenching.
Wherein the steel structure material comprises a steel pipe.
Wherein the ductile structure is made of bainite or pearlite.
Wherein the heat treatment comprises a high frequency heat treatment.
Heat treating the steel structure material to form an austenite structure;
Forming a martensite structure by performing a first cooling process on the outer side of the heat treated steel structure material at a first cooling rate; And
And performing a second cooling process with respect to the inner side of the heat treated steel structure material at a second cooling rate lower than the first cooling rate to form a bainite or pearlite structure,
Wherein the first cooling step and the second cooling step are performed simultaneously.
Priority Applications (1)
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KR1020130163670A KR20150075580A (en) | 2013-12-26 | 2013-12-26 | Complex steel structure and method of manufacturing the same |
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KR1020130163670A KR20150075580A (en) | 2013-12-26 | 2013-12-26 | Complex steel structure and method of manufacturing the same |
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2013
- 2013-12-26 KR KR1020130163670A patent/KR20150075580A/en not_active Application Discontinuation
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