A manufacturing method of composite-phase steel having excellent material and durability uniformity and a thickness of 5 mm or more, the manufacturing method comprising:
- reheating a steel slab including, by wt %, C:
- 0.05 to 0.15%, Si:
- 0.01 to 1.0%, Mn:
- 1.0 to 2.3%, Al:
- 0.01 to 0.1%, Cr:
- 0.005 to 1.0%, P:
- 0.001 to 0.05%, S:
- 0.001 to 0.01%, N:
- 0.001 to 0.01%, Nb:
- 0.005 to 0.07%, Ti 0.005 to 0.11%, Fe and unavoidable impurities at a temperature of 1200 to 1350° C.;
- manufacturing a hot-rolled steel sheet by finish hot rolling the reheated steel slab at a finish hot rolling (FDT) satisfying the following [Relational Expression 1] of steel;
- primarily cooling the hot-rolled steel sheet to a mid-temperature (MT) range of 550 to 650° C. to satisfy the following [Relational Expression 2];
- and
- when the primarily cooled steel sheet is divided, in a lengthwise direction, into three parts:
- HEAD, MID, and TAIL parts, secondarily cooling a region of the HEAD part and the TAIL part corresponding to an outer wound portion of a coil during winding to a temperature range from 450 to 550° C. to satisfy the following [Relational Expression 3], and secondarily cooling a region of the MID part corresponding to an inner wound portion of the coil to the temperature range from 400 to 500° C. to satisfy the following [Relational Expression 4], and then coiling the secondly cooled steel sheet;
- Tn
- -
- 60
- ≤
- FDT
- ≤
- Tn
- [
- Relational
-
- Expression
-
- 1
- ]
- Tn
- =
- 740
- +
- 92
- [
- C
- ]
- -
- 80
- [
- Si
- ]
- +
- 70
- [
- Mn
- ]
- +
- 45
- [
- Cr
- ]
- +
- 650
- [
- Nb
- ]
- +
- 410
- [
- Ti
- ]
- -
- 1
- .
- 4
-
- (
- t
- -
- 5
- )
- the FDT of the above Relational Expression 1 is a finish hot-rolling temperature (° C.),
- [C], [Si], [Mn], [Cr], [Nb], and [Ti] in the above Relational Expression 1 are wt % of the corresponding alloy element,
- t of the above Relational Expression 1 is a thickness of a final hot-rolled sheet (mm)
- CR
-
- 1
- min
- <
- CR
-
- 1
- <
- CR
-
- 1
- max
- [
- Relational
-
- Expression
-
- 2
- ]
- CR
-
- 1
- min
- =
- 210
- -
- 850
- [
- C
- ]
- +
- 1.5
- [
- Si
- ]
- -
- 67.2
- [
- Mn
- ]
- -
- 59.6
- [
- Cr
- ]
- +
- 187
- [
- Ti
- ]
- +
- 852
- [
- Nb
- ]
- CR
-
- 1
- max
- =
- 240
- -
- 850
- [
- C
- ]
- +
- 1.5
- [
- Si
- ]
- -
- 67.2
- [
- Mn
- ]
- -
- 59.6
- [
- Cr
- ]
- +
- 187
- [
- Ti
- ]
- +
- 852
- [
- Nb
- ]
- CR1 of the above Relational Expression 2 is a primary cooling rate (° C./sec) in an FDT to MT (550 to 650° C.) section,
- [C], [Si], [Mn], [Cr], [Ti], and [Nb] in the above Relational Expression 2 are wt % of the corresponding alloy element
- CR
-
- 2
- OUT
- -
- min
- <
- CR
-
- 2
- OUT
- <
- CR
-
- 2
- OUT
- -
- max
- [
- Relational
-
- Expression
-
- 3
- ]
- CR
-
- 2
- OUT
- -
- min
- =
- 14.5
- [
- C
- ]
- +
- 18.75
- [
- Si
- ]
- +
- 8.75
- [
- Mn
- ]
- +
- 8.5
- [
- Cr
- ]
- +
- 35.25
- [
- Ti
- ]
- +
- 42.5
- [
- Nb
- ]
- -
- 14
- CR
-
- 2
- OUT
- -
- max
- =
- 38.7
- [
- C
- ]
- +
- 50
- [
- Si
- ]
- +
- 23.3
- [
- Mn
- ]
- +
- 22.7
- [
- Cr
- ]
- +
- 94
- [
- Ti
- ]
- +
- 113.3
- [
- Nb
- ]
- -
- 37.4
- CR2OUT of the above Relational Expression 3 is the secondary cooling rate (° C./sec) in MT to coiling temperature section of the HEAD part and the TAIL part,
- [C], [Si], [Mn], [Cr], [Ti], and [Nb] in the above Relational Expression 3 are wt % of the corresponding alloy element
- CR
-
- 2
- IN
- -
- min
- <
- CR
-
- 2
- IN
- <
- CR
-
- 2
- IN
- -
- max
- [
- Relational
-
- Expression
-
- 4
- ]
- CR
-
- 2
- IN
- -
- min
- =
- 29
- [
- C
- ]
- +
- 37.5
- [
- Si
- ]
- +
- 17.5
- [
- Mn
- ]
- +
- 17
- [
- Cr
- ]
- +
- 20.5
- [
- Ti
- ]
- +
- 25
- [
- Nb
- ]
- -
- 28
- CR
-
- 2
- IN
- -
- max
- =
- 211.5
- [
- C
- ]
- +
- 5.5
- [
- Si
- ]
- +
- 15
- [
- Mn
- ]
- +
- 6
- [
- Cr
- ]
- +
- 30.5
- [
- Ti
- ]
- +
- 41
- [
- Nb
- ]
- +
- 30.5
- CR2IN of the above Relational Expression 4 is the secondary cooling rate (° C./sec) in MT to coiling temperature section of the MID part,
- [C], [Si], [Mn], [Cr], [Ti], and [Nb] in the above Relational Expression 4 are wt % structure of the corresponding alloy element.