Technical Field
[0001] The present disclosure relates to a high-strength steel sheet used for a vehicle
structure member, and more specifically, to a high-strength steel sheet having excellent
crashworthiness and formability, and a method for manufacturing the same.
Background Art
[0002] Recently, as environmental and safety regulations have become increasingly harsh
in the automobile industry, carbon dioxide emission regulations and fuel efficiency
regulations have also been increasingly strengthened. The Insurance Institute for
Highway Safety in the United States has been increasingly tightening collision stability
regulations to protect passengers, and since 2013, severe collision performance such
as 25% small overlap has been required.
[0003] The only solution to address these environmental and safety issues is automotive
weight reduction. High strength of steel is required to achieve weight reduction,
and high formability is required to apply high-strength steel. In addition, in order
to simultaneously increase the collision performance of the vehicle body, a yield
ratio (YS/TS) is required to be high.
[0004] In general, high-strength vehicle materials may be classified into precipitation
reinforced steel, bake hardened steel, solid solution strengthened steel, and transformation
reinforced steel.
[0005] The transformation reinforced steel includes Dual Phase Steel (DP steel), Complex
Phase Steel (CP steel), or Transformation Induced Plasticity Steel (TRIP steel). The
transformation reinforced steel is also referred to as Advanced High Strength Steel
(ASS).
[0006] Thereamong, DP steel is a steel that secures high strength by finely and homogeneously
dispersing a hard martensite in a soft ferrite, and CP steel is a steel that includes
two or three phases of a ferrite, a martensite, and a bainite, and adds precipitation
hardening elements such as Ti and Nb to improve strength. TRIP steel is a steel that
includes fine and homogeneously dispersed retained austenite, and may ensure high
strength and high ductility by causing a retained austenite phase to be transformed
into a martensite during room temperature processing.
[0007] On the other hand, recent steel sheets for vehicles require steel sheets with higher
strength to improve fuel efficiency and durability, and in terms of collision safety
and passenger protection, ultra-high-strength steel sheets with a tensile strength
of 980 MPa or higher are increasingly being applied as body structures or reinforcement
materials.
[0008] Specifically, high-strength steel having excellent yield strength is adopted in structural
members such as members, seat rails, and pillars, in order to improve crashworthiness
of a vehicle body. As yield strength (YS), that is, a yield ratio (YR=YS/TS), compared
to tensile strength (TS), becomes higher and higher, a structural member is more advantageous
for crashworthiness characteristics.
[0009] However, in general, ductility decreases as the strength of the steel sheet increases,
which may cause a problem of deteriorating molding processability, and thus, the development
of a material capable of supplementing the problem is required. In other words, it
may be essential to develop a material with high yield strength and excellent ductility
to simultaneously secure collision stability and component formability.
[0010] Furthermore, most of the processed components have a shear surface therein or at
an edge thereof, and accordingly, when the Hall Expansion Station (HER) is excellent,
the components may be molded without defects such as cracks in the shear surface,
and even in the event of collisions, collision performance may be improved through
impact absorption.
[0011] Accordingly, when it is possible to secure excellent ductility while increasing a
low yield ratio and an inferior hole expansion ratio, which are shortcomings of the
most widely used DP steel among the transformation reinforced high-strength steel,
in order to improve the impact characteristics and simultaneously of high-strength
steel, an application of high-strength steel could be further expanded.
[0012] On the other hand, in order to increase the yield ratio of the steel, it is necessary
to increase yield strength compared to tensile strength, and a representative way
to achieve the increased yield strength is to use water cooling during continuous
annealing. As an example, a steel sheet in which a microstructure has a tempered martensite
phase may be manufactured through a tempering process after forming a martensite by
performing cracking in an annealing process and then depositing in water.
[0013] However, in the method, since a shape quality is deteriorated due to temperature
variations in a width direction and a length direction during water cooling, there
may be very serious disadvantages such as deterioration of workability such as cracks
during molding and material deviation by location.
[0014] Patent Document 1, which is a prior art related to the aforementioned technology,
discloses martensite steel with a volume ratio of 80 to 97% of martensite, obtained
by continuously annealing a steel material containing 0.18% or more of carbon (C)
and then cooling the steel material to room temperature, and then treating over-aging
on the steel material at a temperature of 120 to 300°C for 1 to 15 minutes. As described
above, when ultra-high strength steel is manufactured by a water cooling and tempering
manner, the yield ratio is very high, but the shape quality of a coil may be deteriorated
due to temperature variations in a width direction and a length direction, resulting
in problems such as an occurrence of cracks and workability reduction occur during
molding processing.
[0015] Patent Document 2 relates to a steel sheet formed of a complex tissue mainly composed
of martensite, and discloses a method of manufacturing a high-tensile steel sheet
in which fine precipitated copper particles having a particle diameter of 1to 100
nm are dispersed inside the tissue to improve processability. However, by adding Cu
in excess of 2 to 5% to precipitate fine copper particles, there may be a concern
that hot shortness due to Cu may occur, which may excessively increase manufacturing
costs.
[0016] Patent Document 3 relates to a precipitation-reinforced steel sheet containing 2
to 10% of pearlite with ferrite as a base structure, which adds carbon/nitride forming
elements such as Nb, Ti, V, and the like, thereby improving strength by precipitation
reinforcement and grain refinement. The steel sheet has a good hole expansion ratio,
but has a limitation to increasing tensile strength, and also has high yield strength
and low ductility, resulting in an occurrence of cracks during press molding.
[0017] Patent Document 4 discloses a method of manufacturing a cold-rolled steel sheet with
excellent plate shape after continuous annealing and securing high strength and high
ductility at the same time by utilizing a tempered martensite, but since a carbon
content is as high as 0.2% or more, the weldability may be degraded, and dent defects
in a furnace may occur due to a large amount of Si.
[Prior Art Document]
Summary of Invention
Technical Problem
[0019] An aspect of the present disclosure is to provide a steel sheet used for a vehicle
structure member, that is, a steel sheet having excellent strength as well as ductility
and having improve crashworthiness and formability, and a method for manufacturing
the same.
[0020] The aspect of the present disclosure is not limited to the above. The aspect of the
present disclosure may be understood from overall contents of the present specification,
and those of ordinary skill in the technical field to which the present disclosure
pertains will have no difficulty in understanding an additional aspect of the present
disclosure.
Solution to Problem
[0021] According to an aspect of the present disclosure, a high-strength steel sheet having
excellent crashworthiness and formability may include: by wt%, carbon (C): 0.06 to
0.2%, silicon (Si): 0.4 to 1.4%, manganese (Mn): 1.8 to 3.0%, aluminum acid (Sol.Al):
1.0% or less, molybdenum (Mo): 0.4% or less, chromium (Cr): 1.0% or less, antimony
(Sb): 0.06% or less, boron (B): 0.01% or less, phosphorus (P): 0.1% or less, sulfur
(S): 0.01% or less, and a balance of Fe and unavoidable impurity elements, wherein
the C, Si and Al satisfy the following Relational Expression 1,
[0022] a microstructure includes 40 to 80% of a sum of tempered martensite and bainite phases
as an area fraction, 3 to 15% of a retained austenite phase, and a balance of ferrite
and fresh martensite, and in the retained austenite phase, a share (A
TM+B/A
T) of retained austenite (A
TM+B) adjacent to tempered martensite and bainite among a total retained austenite fraction
(A
T) is 90% or more,

(In the relational expression 1, each element denotes a weight content).
[0023] According to another aspect of the present disclosure, a method for manufacturing
a high-strength steel sheet having excellent crashworthiness and formability may include:
heating a steel slab in a temperature range of 1050 to 1250°C, the steel slab including,
by wt%, carbon (C): 0.06 to 0.2%, silicon (Si): 0.4 to 1.4%, manganese (Mn): 1.8 to
3.0%, aluminum acid (Sol.Al): 1.0% or less, molybdenum (Mo): 0.4% or less, chromium
(Cr): 1.0% or less, antimony (Sb): 0.06% or less, boron (B): 0.01% or less, phosphorus
(P): 0.1% or less, sulfur (S): 0.01% or less, and a balance of Fe, and unavoidable
impurity elements, the C, Si and Al satisfying the following Relational Expression
1; manufacturing a hot-rolled steel sheet by finish hot rolling the reheated steel
slab at a temperature range of a finish hot rolling outlet-side temperature Ar3 to
Ar3+50°C; coiling the hot-rolled steel sheet in a temperature range of 400 to 700°C;
after the coiling, cooling the hot-rolled steel sheet to room temperature at cooling
rate of 0.1°C/s; after the cooling, manufacturing a cold-rolled steel sheet by cold
rolling the hot-rolled steel sheet with a total reduction ratio of 30 to 80%; continuously
annealing the cold-rolled steel sheet; primarily cooling the continuously annealed
cold-rolled steel sheet at cooling rate of 10°C/s or less by 450 to 700°C; after the
primary cooling, performing secondary cooling at cooling rate of 3°C/s or higher by
250 to 500°C; and reheating the secondary cooled cold-rolled steel sheet by a temperature
of 490°C or less and maintaining for 30 seconds or more,
wherein the cold rolling is performed at a cumulative reduction ratio of 20% or more
for the first 1 to 3 stands.
Advantageous Effects of Invention
[0024] According to an aspect of the present disclosure, a steel sheet having high strength
and excellent ductility may be provided. Specifically, since the steel sheet of the
present disclosure has a higher yield ratio than that of conventional DP steel, the
steel sheet has an excellent hole expansion ratio, thereby having excellent impact
resistance and formability.
[0025] The steel sheet of the present disclosure may be suitably applied as a material for
a vehicle structure member requiring processing into a complex shape.
Brief Description of Drawings
[0026]
FIG. 1 is a graph showing a change in mechanical properties (Relational Expression
2) according to Relational Expression 1 according to an example embodiment of the
present disclosure.
FIG. 2 is a microstructure measurement image of a steel of the present disclosure
according to an example embodiment of the present disclosure.
Best Mode for Invention
[0027] The inventors of the present disclosure studied deeply to provide a high-strength
steel sheet having improved crashworthiness and formability by increasing a yield
ratio (YR) and a hole expansion ratio, as compared to conventional DP steel, while
satisfying high ductility, which is a characteristic of the conventional DP steel.
[0028] As a result, the inventors confirmed that by optimizing an alloy component system
and manufacturing conditions of the steel, a steel sheet may have an advantageous
structure for securing target physical properties, from which it is possible to provide
a steel sheet suitable for a vehicle structure member that require processing into
a complex shape, and have completed the present disclosure.
[0029] Hereinafter, the present disclosure will be described in detail.
[0030] A high-strength steel sheet having excellent crashworthiness and formability according
to an aspect of the present disclosure may include: by wt%, carbon (C): 0.06 to 0.2%,
silicon (Si): 0.4 to 1.4%, manganese (Mn): 1.8 to 3.0%, aluminum acid (Sol.Al): 1.0%
or less, molybdenum (Mo): 0.4% or less, chromium (Cr): 1.0% or less, antimony (Sb):
0.06% or less, boron (B): 0.01% or less, phosphorus (P): 0.1% or less, sulfur (S):
0.01% or less.
[0031] Hereinafter, a reason for limiting an alloy composition of a steel sheet provided
by the present disclosure as above will be described in detail.
[0032] Meanwhile, unless specifically stated in the present disclosure, a content of each
element is based on weight, and a ratio of a structure is based on area.
Carbon (C): 0.06 to 0.2%
[0033] Carbon (C) is a greatly important element added to strengthen a transformation structure.
The C promotes the high-strength of steel and promotes a formation of martensite in
complex structure steel. When the content of C increases, the amount of martensite
increases.
[0034] When the content of C exceeds 0.2%, the strength due to the formation of martensite
is increased, but a strength difference from ferrite having a low carbon concentration
is increased. Such a difference in strength may result in ductility and a process
curing ratio because destruction at an interphase interface is easily caused during
plastic deformation. Furthermore, welding defects occur during component processing
due to poor weldability, and liquid metal embrittlement (LME) cracks occur during
welding, leading to undermining component performance. On the other hand, when the
content of C is less than 0.06%, it is difficult to secure a target level of strength,
and it becomes difficult to secure a certain percentage of retained austenite phase
required for ductility.
[0035] Accordingly, in the present disclosure, C may be included in an amount of 0.06 to
0.20%, and more preferably 0.08% or more and 0.18% or less.
Silicon (Si): 0.4 to 1.4%
[0036] Silicon (Si) is a ferrite stabilizing element that promotes a transformation of ferrite
and promotes the concentration of carbon (C) into untransformed austenite, thus contributing
to the formation of martensite. In addition, the Si is effective in reducing a hardness
difference between phases by increasing the strength of ferrite due to an excellent
solid solution strengthening ability thereof. Furthermore, the Si effectively inhibits
the precipitation of carbides in bainite when maintained in a bainite area, thereby
encouraging C concentration into untransformed austenite, and the Si delays the transformation
of martensite during cold rapid cooling, thereby forming retained austenite required
for ductility, so that the Si is a useful element for improving the ductility of a
steel sheet. That is, the Si is a useful element capable of securing strength without
lowering the ductility of the steel sheet.
[0037] When the content of Si exceeds 1.4%, it causes surface scale defects to adversely
affect plating surface quality, reduces phosphatability, and causes welding defects
during component processing due to poor weldability. Specifically, LME cracks occur
during welding, which reduces component performance. On the other hand, when the content
of Si is less than 0.4%, it may be difficult to secure a certain percentage of retained
austenite phase required for ductility, and the strength of ferrite may decrease due
to poor solid solution hardenability, so that there is a limit to reducing a difference
in hardness between phases.
[0038] Accordingly, in the present disclosure, the Si may be included in an amount of 0.4
to 1.4%, and more preferably may be 0.5% or more and 1.2% or less.
Manganese (Mn): 1.8 to 3.0%
[0039] Manganese (Mn) is an effective element for micronizing particles without decreasing
ductility, and strengthening steel as well as preventing hot brittleness caused by
FeS generation by completely precipitating sulfur (S) in steel as MnS. In addition,
the Mn reduces critical cooling rate at which a martensite phase is obtained in composite
phase steel, thereby facilitating the formation of martensite.
[0040] When the content of Mn is less than 1.8%, it may be difficult to ensure target strength
in the present disclosure. On the other hand, when the content of Mn exceeds 3.0%,
problems such as weldability and hot rolling may be likely to occur, and since martensite
is excessively formed, the material is unstable and a manganese oxide band (Mn-Band)
is formed in a structure, which may increase the risk of causing defects such as processing
cracks and plate breakage. In addition, there may be a problem that Mn oxide may be
eluted to a surface during an annealing process to greatly reduce the surface quality.
[0041] Accordingly, in the present disclosure, the Mn may be included in an amount of 1.8
to 3.0%, and more preferably 2.0% or more and 2.9% or less.
Acid-Soluble Aluminum (Sol.Al): 1.0% or less
[0042] Acid-soluble aluminum (Sol.Al) is an element added for refining a particle size of
the steel and deoxidation, and is a ferrite stabilizing element similar to Si. The
Al is an element useful for improving hardenability of martensite by distributing
carbon in ferrite to austenite. Furthermore, the Al may effectively suppress the precipitation
of carbides in bainite when maintained in a bainite area during annealing to promote
C concentration with untransformed austenite and delay martensite transformation during
cold rapid cooling, and may improve the ductility of a steel sheet by generating a
retained austenite phase.
[0043] When continuous casting is performed in steelmaking by allowing the content of Al
to exceed 1.0%, excessive formation of inclusions may increase the likelihood of surface
defects on a steel sheet surface, and may also cause an increase in manufacturing
costs. In addition, due to poor weldability, there may be a concern that welding defects
may occur during component processing.
[0044] Thus, the Al may be included in an amount of 1.0% or less, excluding 0%. More preferably,
the Al may be included in an amount of 0.01% or more.
Molybdenum (Mo): 0.4% or less
[0045] Molybdenum (Mo) is an element delaying the transformation of austenite into pearlite
and improving the miniaturization and strength of ferrite. The Mo has an advantage
of improving the hardenability of the steel and controlling a yield ratio by finely
forming martensite on a grain boundary. However, the Mo is an expensive element, and
as a content thereof increase, the manufacturing costs thereof increases, which is
economically disadvantageous.
[0046] In order to sufficiently obtain the above-described effects, the Mo may be added
in a maximum amount of 0.4%. When the content of Mo exceeds 0.4%, alloy costs are
rapidly increased, leading to a decrease in economic feasibility, and also, an effect
refining crystal grains and an effect of solid solution strengthening, leading to
a decrease in the ductility of the steel.
[0047] Accordingly, in the present disclosure, the content of the Mo may 0.4% or less. According
to the present disclosure, even if the Mo is not added, there is no difficulty in
securing intended microstructure and physical properties, and thus, the content of
the Mo may be 0%. However, when the Mo is added, the Mo may be more advantageously
included in the amount of 0.01% or more.
Chromium (Cr): 1.0% or less
[0048] Chromium (Cr) is an element added to improve the hardenability of steel and secure
high strength, and plays an important role in the formation of martensite. Furthermore,
the Cr is advantageous for manufacturing highly flexible complex phase steel by minimizing
the decrease in an elongation ratio as compared to an increase in strength.
[0049] When the content of Cr exceeds 1.0%, there may be a problem in that not only the
above-described effects are saturated, but also hot rolling strength is excessively
increased to deteriorate cold rolling. Furthermore, since Cr-based carbides are excessively
formed and coarsened, there may be a problem in that a size of martensite becomes
coarse after annealing, resulting in a decrease in an elongation ratio.
[0050] Accordingly, in the present disclosure, the content of the Cr may be 1.0% or less.
In the present disclosure, even if the Cr is not added, there is no difficulty in
ensuring intended microstructure and physical properties, and thus, the content of
Cr may be 0%. However, when the Cr is added, the Cr may be more advantageously included
in the amount of 0.1% or more.
Antimony (Sb): 0.06% or less
[0051] Antimony (Sb) is distributed in a grain boundary to delay a diffusion of oxidizing
elements such as Mn, Si, and Al through the grain boundary, thus suppressing a surface
concentration of an oxide. Furthermore, the Sb has an excellent effect on suppressing
the coarsening of surface agglomerates due to temperature increase and hot-rolled
process change. When the content of Sb exceeds 0.06%, the above-described effects
may be saturated, manufacturing costs may be increased, and processability may be
degraded.
[0052] Accordingly, the content of the Sb may be 0.06% or less. According to the present
disclosure, even if the Sb is not added, there is no difficulty in ensuring intended
microstructure, physical properties, and the like, and thus, the content of Sb may
be 0%. However, when the Sb is added, the Sb may be more advantageously included in
an amount of 0.01% or more.
Boron (B): 0.01% or less
[0053] Boron (B) is an element delaying the transformation of austenite into pearlite in
a cooling process during annealing, and is a hardenability element inhibiting ferrite
formation and promoting martensite formation. When the content of B exceeds 0.01%,
the B may be excessively enriched on a surface of steel, which may degrade plating
adhesiveness.
[0054] Accordingly, the content of B may be 0.01% or less. According to the present disclosure,
even if the B is not added, there is no difficulty in ensuring intended microstructure
and physical properties, and thus, the content of B may be 0%. However, when the B
is added, the B may be more advantageously included in an amount of 0.0005% or more.
Phosphorus (P): 0.1% or less
[0055] Phosphorus (P) is a substituted element having a large solid solution strengthening
effect and is the most advantageous element for improving in-plane anisotropy and
securing strength without significantly impairing formability. However, when the content
of P is excessively added, the possibility of brittle destruction increases significantly,
which may hinder the possibility of plate fracture of a slab during hot rolling and
plating surface properties.
[0056] Accordingly, the P may be included in an amount of 0.1% or less, and the amount of
0% may be excluded in consideration of a level inevitably added during a steel manufacturing
process.
Yellow (S): 0.01% or less
[0057] Sulfur (S) is an impurity inevitably added to steel and is an element that inhibits
ductility and weldability, and thus, it may be advantageous to manage the content
of S to be as low as possible. Specifically, since there is a high possibility of
generating hot brittleness, it may be preferable to control the content thereof to
0.01% or less. However, 0% may be excluded in consideration of the level inevitably
added during a steel manufacturing process.
[0058] In addition to the above-described alloy composition, the steel sheet of the present
disclosure may further include at least one of Ti and Nb for the purpose of further
improving the mechanical properties of the steel sheet.
Titanium (Ti): 0.05% or less, and Niobium (Nb): 0.05% or less
[0059] Titanium (Ti) and niobium (Nb) are effective elements for increasing the strength
of steel and refining crystal grains by forming nano-precipitation hardening. When
these elements are added, they may be coupled to carbon to form very fine nano-precipitation
hardening, and the nano-precipitation hardening may serve to strengthen a matrix structure
and reduce a hardness difference between phases.
[0060] In a case in which the Ti and the Nb are added, when the content thereof exceeds
0.05%, respectively, manufacturing costs may increase, and the precipitation hardening
may be excessively formed, resulting in significantly degraded ductility.
[0061] Accordingly, when one or more of Ti and Nb are added, each of them may be included
in an amount of 0.05% or less.
[0062] The remaining component of the present disclosure is iron (Fe). However, since impurities
that are not intended from raw materials or the surrounding environments may inevitably
be mixed in the normal manufacturing process, the impurities may not be excluded.
Since these impurities are known to those skilled in the steel manufacturing field,
not all of these impurities are specifically mentioned in this specification.
[0063] In a steel sheet of the present disclosure satisfying the alloy composition described
above, preferably, a relationship of the content of C, Si and Al may satisfy Relational
Expression 1 below.

(In the relational expression 1, each element denotes a weight content.)
[0064] Si and Al in steel are ferrite stabilizing elements promoting ferrite transformation,
and contributing to the formation of retained austenite and martensite by encouraging
C concentration to untransformed austenite. C is also an element contributing to the
formation and fraction adjustment of martensite by promoting the C concentration to
untransformed austenite.
[0065] Specifically, when a value of R relational Expression 1 is controlled to be 1.7 or
more, the fraction of retained austenite that can contribute to ductility may be secured,
from which it is possible to improve the ductility and formability of the steel sheet.
On the other hand, when Relational Expression 1 above is not satisfied, the retained
austenite fraction is insufficient, and a distribution of the generated retained austenite
is not uniform, which may make it difficult to secure ductility and formability.
[0066] As will be described in detail below, the present disclosure may distribute retained
austenite produced by optimizing the steel sheet manufacturing process together with
the above-described alloy component system finely around a hard phase, thus mitigating
local stress concentration, from which it may be possible to improve ductility thereof
and to secure excellent formability.
[0067] The steel sheet of the present disclosure may include 40 to 80% of tempered martensite
and bainite phases as a total area fraction, 3 to 15% of a retained austenite phase,
and a balance of ferrite and fresh martensite , as a microstructure.
[0068] In the present disclosure, the tempered martensite and bainite structures assist
in forming retained austenite in addition to an effect contributing to strength. Specificall
y, when Si and Al are added to steel, by delaying the precipitation of carbides during
bainite transformation, carbon (C) is accumulated into untransformed austenite around
bainite, thereby lowering a martensite transformation temperature below room temperature.
In this case, retained austenite may be secured at room temperature. Furthermore,
when tempering the martensite, carbon (C) introduced in the martensite moves to surrounding
untransformed austenite and is then accumulated, thereby lowering the martensite transformation
temperature below room temperature, as well as securing retained austenite at room
temperature.
[0069] From this, the steel sheet of the present disclosure may include 3 to 15% of a retained
austenite phase. By securing 3% or more of the retained austenite phase, it is advantageous
to secure ductility of the steel sheet by causing transformation induced plasticity
during molding. However, if a fraction thereof is excessive, the steel sheet tends
to be vulnerable to liquid metal brittleness (LME) during point welding to assemble
plated steel sheets into vehicle components. Accordingly, preferably, the retained
austenite phase may be included in an amount of 15% or less.
[0070] On the other hand, the retained austenite phase is characterized in that a share
(A
TM+B/A
T) of retained austenite (A
TM+B) adjacent to tempered martensite and bainite among a total retained austenite fraction
(A
T) is more than 90%.
[0071] Here, being adjacent to the tempered martensite and the bainite may refer to the
periphery of their phases, more specifically an interface area of these phases. As
an example, as illustrated in FIG. 2, this denotes that retained austenite phases
are mainly distributed around a grain boundary on the tempered martensite and the
bainite.
[0072] As described above, theretained austenite phases may be finely and evenly distributed
around the tempered martensite and the bainite, thereby improving ductility through
an effect of relieving local stress concentration, and accordingly, excellent formability
without cracks when forming components may be secured.
[0073] When a total fraction of the tempered martensite and the bainite is less than 40%,
retained austenite cannot be evenly distributed around the tempered martensite and
the bainite, and the amount thereof may also be reduced, which may make it impossible
to improve formability. On the other hand, when the fraction thereof exceeds 80%,
the fraction of ferrite contributing to ductility may be significantly lowered, and
the fraction of the retained austenite may also be lowered, which may make it impossible
to improve ductility and formability.
[0074] More advantageously, the tempered martensite phase of the total fraction may be included
in an amount of 25 to 65%.
[0075] In the present disclosure, ferrite and fresh martensite phases may be included in
addition to the above-described tempered martensite, bainite, and retained austenite
phases. In this case, a ferrite phase may be included in an amount of 40% or less,
and a fresh martensite phase may be included in an amount of 20% or less. Here, the
amount of 0% of the ferrite phase and the fresh martensite phase are excluded.
[0076] When the fraction of the ferrite phase exceeds 40%, not only cannot a target level
of strength be secured, but it may be difficult to improve a yield ratio. Furthermore,
when the fraction of the fresh martensite exceeds 20%, the fraction of the retained
austenite phase may decrease to reduce the ductility, and the formability thereof
may not be secured.
[0077] The steel sheet of the present disclosure, which has the above-described alloy component
system and microstructure, not only has high strength having a tensile strength of
980 MPa or more, but also has a yield ratio of 0.6 to 0.9, an elongation ratio of
10% or more, and a hole expansion ratio of 20% or more. When the yield ratio is less
than 0.6, the hole expansion ratio is degraded, but when the yield ratio exceeds 0.9,
the ductility decreases.
[0078] In addition, the steel sheet of the present disclosure may provide a steel sheet
having both high yield ratio and high ductility as a relationship between the yield
ratio, the elongation ratio, and the tensile strength satisfies the following Relational
Expression 2.
[0079] The high yield ratio of the steel sheet may contribute to the improvement of stability
during a vehicle collision due to excellent crashworthiness of the material, and the
high ductility may prevent processing defects such as cracks and wrinkles that occur
during press processing into components, thereby securing excellent formability.
[0080] In the present disclosure, when a value of the following Relational Expression 2
is 9 or more, the crashworthiness and formability may be ensured at the same time,
but when the value thereof is less than 9, the crashworthiness and the formability
may not be ensured at the same time.

(In the relational expression 2,units of each physical property are excluded.)
[0081] Since the steel sheet of the present disclosure having the mechanical properties
as described above may prevent processing defects such as cracks and wrinkles when
processing into components, the steel sheet may be used in various ways for a vehicle
structure member. In addition, the steel sheep may contribute to improving the safety
of structural components and vehicles by delaying an occurrence of crashworthiness
and cracks during a collision.
[0082] On the other hand, the steel sheet of the present disclosure may be a cold-rolled
steel sheet, and may be a hot-dip galvanized steel sheet including a zinc-based plating
layer on at least one surface of the cold-rolled steel sheet, and an alloyed hot-dip
galvanized steel sheet alloyed with the hot-dip galvanized steel sheet.
[0083] Although not particularly limited, the zinc-based plating layer may be a zinc plating
layer mainly containing zinc and a zinc alloy plating layer containing aluminum and/or
magnesium other than zinc.
[0084] Hereinafter, a method for manufacturing a high-strength steel sheet having excellent
crashworthiness and formability provided by the present disclosure, another aspect
of the present invention, will be described in detail.
[0085] In short, the present disclosure may manufacture a desired steel sheet through a
process of [steel slab reheating - hot rolling - coiling - cooling - cold rolling
- continuous annealing - cooling - reheating and maintaining], and then further processes
such as [hot dip galvanizing - alloying heat treatment] may be performed.
[0086] The conditions for each operation will be described in detail below.
[Heating Steel Slab]
[0087] First, after preparing a steel slab that satisfy all of the above-described alloy
component systems, the steel slab may be heated. This process is performed to smoothly
perform a subsequent hot rolling process and to sufficiently obtain properties of
a desired steel sheet.
[0088] The heating process may be performed in a temperature range of 1050 to 1250°C. When
the heating temperature is less than 1050°C, friction between the steel sheet and
a rolling mill increases, which may rapidly increase a load applied to a roller during
hot rolling. On the other hand, when the temperature exceeds 1250°C, not only does
energy costs required for temperature rise increase, but also the amount of surface
scale increases, leading to material loss.
[0089] Accordingly, the heating process may be performed in a temperature range of 1050
to 1250°C.
[Hot Rolling]
[0090] A hot-rolled steel sheet may be manufactured by finishing hot rolling the steel slab
heated according to the aforementioned process at a Ar3 transformation point or higher,
and in this case, a temperature on an outlet side may satisfy Ar3 to Ar3+50°C.
[0091] When the temperature at the outlet side is less than Ar3 during the finishing hot
rolling, ferrite and austenite two-phase rolling may be performed, resulting in material
non-uniformity. On the other hand, when the temperature thereof exceeds Ar3+50°C,
there may be a concern that material non-uniformity may occur due to the formation
of abnormally coarsened grains by high-temperature rolling, and as a result, there
may be a problem in that coil distortion occurs during subsequent cooling.
[0092] More specifically, the finishing hot rolling may be performed in a temperature range
of 800 to 1000°C.
[Coiling]
[0093] The hot-rolled steel sheet produced according to the aforementioned process may be
coiled, and in this case, the coiling may be performed in a temperature range of 400
to 700°C.
[0094] When the coiling temperature is less than 400°C, the strength of the hot-rolled steel
sheet may be excessively increased, which may result in a rolling load during subsequent
cold rolling. Furthermore, it takes excessive costs and time to cool the hot-rolled
steel sheet to the coiling temperature, causing an increase in process costs. On the
other hand, when the temperature exceeds 700°C, excessive scale may occur on a surface
of the hot-rolled steel sheet, which is likely to cause surface defects, and this
may cause the deterioration of plating.
[0095] Accordingly, the coiling process may be performed in a temperature range of 400 to
700°C.
[Cooling]
[0096] The coiled hot-rolled steel sheet may be cool to room temperature at average cooling
rate of 0.1°C/s or less (excluding 0°C/s). The cooling may be performed at the average
cooling rate of more advantageously 0.05°C/s or less, and more advantageously 0.015°C/s
or less. Here, the cooling denotes average cooling rate.
[0097] In this way, by cooling the coiled hot-rolled steel sheet at a constant velocity,
it may be possible to obtain a hot-rolled steel sheet in which carbides as a nucleation
site of austenite are finely dispersed. In other words, fine carbides are evenly dispersed
in the steel during a hot rolling process, and during subsequent annealing, the carbides
dissolve to allow an austenite phase in the steel to be finely dispersed and formed,
and as a result, after the annealing is completed, a uniformly dispersed fine martensite
phase may be obtained.
[Cold rolling]
[0098] The hot-rolled steel sheet coiled according to the aforementioned process may be
manufactured as a cold-rolled steel sheet by cold rolling, and in this case, the cold
rolling may be performed at a cold reduction ratio (total reduction ratio) of 30 to
80%.
[0099] Specifically, the present disclosure may increase energy stored in the steel by controlling
a cumulative reduction ratio of an initial stand, preferably stands 1 to 3, by 20%
or more, during the cold rolling, thereby having an effect of acting as a driving
force for promoting recrystallization of ferrite in a subsequent annealing process.
For this reason, the present disclosure may impart an effect of lowering the fraction
of microcrystalline ferrite in the steel.
[0100] When the microcrystalline ferrite is present in the steel, deformation and stress
are concentrated locally, resulting in poor steel ductility, while recrystallized
ferrite contributes to ductility improvement by mitigating deformation and stress
concentration.
[0101] When the cumulative reduction ratio of the initial stands 1 to 3 is less than 20%
during the cold rolling, or the cold reduction ratio (total reduction ratio) to a
final stand is less than 30%, it may be difficult to secure a desired thickness and
to correct a shape of the steel sheet. In addition, there may be a problem in that
the fraction of microcrystalline ferrite increases to reduce the ductility. On the
other hand, when the cold reduction ratio to the final stand exceeds 80% during the
cold rolling, there may be a problem in that the strength thereof increases, resulting
in a roll load during cold rolling, and the possibility of cracks occurring at an
edge portion of the steel sheet may increase.
[0102] In the present disclosure, the cold rolling may be performed using a rolling mill
comprised of five or six stands, but the present disclosure is not limited thereto.
[Continuous Annealing]
[0103] The cold-rolled steel sheet produced according to the aforementioned process may
be continuously annealed. The continuous annealing treatment may be performed, for
example, in a continuous alloying molten plating furnace.
[0104] The continuous annealing operation is a process of forming ferrite and austenite
phases simultaneously with recrystallization and decomposing carbons.
[0105] The continuous annealing treatment may be preferably performed in a temperature range
of Ac1+30°C to Ac3+30°C, and more preferably, in a temperature range of 800 to 870°C.
[0106] When a temperature during the continuous annealing is below Ac1+30°C, insufficient
recrystallization may not be achieved, and also, it may be difficult to form sufficient
austenite, and thus, the fraction of a desired level of martensite phase and bainite
phase may not be secured after the annealing. On the other hand, when the temperature
exceeds Ac3+30°C, because a size of austenite crystal grains is coarsened, fine retained
austenite phase cannot be evenly formed around a hard phase. Furthermore, productivity
may be reduced, and due to high-temperature annealing, the formation of surface enriched
materials is intensified by elements degrading the wettability of hot-dip galvanizing
of Si, Mn, B and the like, and thus plating surface quality may not be ensured.
[Staged Cooling]
[0107] As described above, the continuously annealed cold-rolled steel sheet may be cooled
step by step.
[0108] Specifically, the cooling may be performed at average cooling rate of 10°C/s or less
(excluding 0°C/s) by 450 to 700°C (the cooling at this time is referred to as primary
cooling) and then performed at average cooling rate of 3°C/s or more by 250 to 500°C
(the cooling at this time is referred to as secondary cooling).
Primary Cooling
[0109] According to the present disclosure, in formation of tempered martensite and bainite
phases with a total area fraction of 40-80% as a final structure, an end temperature
in a subsequent secondary cooling process may be controlled, thereby controlling a
fraction of martensite and bainite generated in this case.
[0110] Specifically, when the subsequent secondary cooling is terminated below a martensite
transformation starting temperature (Ms), a relatively large amount of the martensite
phase may be formed, and for this purpose, it is advantageous to control the end temperature
of the primary cooling to be as low as possible. Furthermore, if the subsequent secondary
cooling is terminated in a bainite temperature range, a bainite phase may be relatively
advantageously formed, and for this purpose, it is advantageous to control the end
temperature of the primary cooling to be higher.
[0111] Preferably, when the subsequent secondary cooling is terminated below Ms, the primary
cooling may be performed up to a temperature range of 450 to 600°C, and when the subsequent
secondary cooling is terminated in the bainite temperature range, the primary cooling
may be performed by a temperature range of 550 to 700°C.
[0112] When the end temperature during the primary cooling is less than 450°C, a larger
load may be applied to facilities configured to cool an atmospheric gas in an annealing
furnace, and the cooling rate is accelerated, and thus, a ferrite phase generated
during cooling may not be sufficiently ensured. On the other hand, when the end temperature
exceeds 700°C, an excessively high cooling rate may be required during subsequent
cooling (secondary cooling).
[0113] Furthermore, when the average cooling rate exceeds 10°C/s during the primary cooling,
carbon diffusion may not be sufficiently generated. Meanwhile, in consideration of
productivity, the primary cooling may be performed at the average cooling rate of
1°C/s or more.
Secondary Cooling
[0114] After completing the first cooling under the above-described conditions, the second
cooling may be performed, and in this case, the formation of a desired microstructure
may be induced by controlling a cooling end temperature and cooling rate.
[0115] When cooling is performed below Ms during the secondary cooling, quenching martensite
may be formed, and as the temperature decreases, the fraction of the quenching martensite
increases, which may lead to an improvement in the strength of the steel sheet. Furthermore,
in a subsequent heat treatment (i.e., a reheating process of the present disclosure),
the martensite may be tempered into tempered martensite, and supersaturated carbon
in the martensite may be distributed to surrounding untransformed austenite, thereby
increasing the stability of retained austenite and improving ductility.
[0116] When the cooling is performed at a temperature exceeding Ms during the secondary
cooling, a bainite fraction may be increased. In this case, during a bainite transformation
process, the precipitation of carbides may be delayed due to the effects of Si and
Al, and as carbons is distributed from the bainite to the surrounding untransformed
austenite, the stability of the retained austenite may be increased and ductility
may be improved.
[0117] When the end temperature of the secondary cooling is less than 250°C, there may be
a problem in that the fraction of the quenching martensite may increase excessively
to decrease the fraction of a retained austenite phase, and the shape of the steel
sheet may become inferior. On the other hand, when the temperature exceeds 500°C,
bainite may be insufficiently formed to decrease the fraction of the retained austenite
phase, and in a subsequent process, there may be a problem in that the fraction on
fresh martensite may increase significantly to excessively increase the strength thereof.
More advantageously, the secondary cooling may be terminated at 400°C or less.
[0118] Furthermore, when the average cooling rate is less than 3°C/s during the secondary
cooling, a pearlite phase may be formed, so that there may be a concern that a bainite
phase may not be formed at a target level. On the other hand, an upper limit of the
average cooling rate is not particularly limited, and may be selected appropriately
by a person skilled in the art in consideration of the specifications of the cooling
facility. For example, the cooling may be performed at 100°C/s or less.
[0119] Furthermore, the secondary cooling may use a hydrogen cooling facility using hydrogen
gas (H
2 gas). In this manner, the cooling may be performed using a hydrogen cooling facility
to obtain the effect of suppressing surface oxidation that may occur during the secondary
cooling. In this case, the hydrogen cooling facility may be controlled by 60 to 70%
hydrogen (H
2) and residual nitrogen (N
2).
[0120] On the other hand, in performing cooling in stages as described above, it may be
possible to perform a faster cooling rate during the secondary cooling than the cooling
speed during the primary cooling.
Maintenance
[0121] After completing the secondary cooling according to the aforementioned process, a
process of maintaining in the cooling temperature range for 30 seconds or more may
be further performed.
[0122] Through the maintenance process, it may be possible to obtain an effect of tempering
quenching martensite or further increasing the amount of bainite transformation. When
the maintenance time is less than 30 seconds, it may be difficult to expect the above-described
effect.
[Reheating and Maintaining]
[0123] According to the aforementioned process, a microstructure intended in the present
disclosure may be formed through a process of reheating and maintaining a cold-rolled
steel sheet that has been cooled step by step. Specifically, it may be desirable to
undergo a process of reheating the secondary cooled cold-rolled steel sheet at a temperature
of 490°C or less and maintaining for more than 30 seconds.
[0124] By performing reheating and maintaining at the above-described temperature, the quenching
martensite produced during the previous cooling process may be transformed into tempered
martensite, and may also be accompanied by bainite transformation.
[0125] During the tempering process, carbons supersaturated in martensite is redistributed
into surrounding untransformed austenite. Furthermore, when the secondary cooling
is terminated in excess of Ms, a bainite fraction may increase significantly during
the reheating and maintenance process, and in this process, carbons discharged from
the bainite is redistributed into untransformed austenite, and thus, the stability
of the retained austenite may be improved to obtain an effect of increasing ductility.
[0126] In addition, during the reheating and maintenance process, potential may be fixed
to the tempered martensite and bainite, which may increase the yield strength, and
as a result, it may be possible to obtain a steel sheet having a yield ratio of 0.6
to 0.9.
[0127] However, when the temperature is excessively high during the reheating, carbides
in the tempered martensite and bainite may be coarsened to decrease the strength thereof,
and a carbon redistribution effect to untransformed austenite due to the formation
of coarsened carbides may be reduced, resulting in a decrease in a retained austenite
fraction, and thus, it is difficult to expect an improvement in ductility.
[0128] Accordingly, the reheating temperature may be limited to 490°C or less, and more
advantageously, the reheating temperature may be 350°C or higher.
[0129] As described above, the cold-rolled steel sheet reheated below 490°C may be maintained
for more than 30 seconds at that temperature so that the above-described effects are
sufficiently realized.
[0130] When the time exceeds 5 minutes during the maintenance, there may be a problem that
a tempering effect of martensite is excessive to decrease the strength.
[0131] According to the present disclosure, by optimizing the alloy component system and
manufacturing conditions described above, the tempered martensite and bainite may
be formed as a matrix structure in a microstructure, and a certain fraction of retained
austenite may be finely and uniformly around the tempered martensite and bainite,
thereby increasing a yield ratio and ductility compared to the conventional DP steel,
and improving the formability for processing components of a steel sheet and the crashworthiness
during a vehicle collision. The steel sheet of the present disclosure, which is precisely
controlled, may secure ductility while maintaining a higher yield ratio than the conventional
DP steel. As a result, it may be possible to provide a high-strength steel sheet having
excellent ductility, hole expansion ratio, formability, and crashworthiness.
[0132] Meanwhile, the present disclosure may provide a plated steel sheet by plating the
cold-rolled steel sheet produced according to the aforementioned process.
[Hot-Dip Galvanizing]
[0133] According to the aforementioned process, a hot-dip galvanized steel sheet may be
manufactured by immersing a steel sheet in a hot-dip galvanized steel sheet bath after
reheating and maintaining processes.
[0134] In this case, the hot-dip galvanizing may be performed under normal conditions, but
for example, the hot-dip galvanizing may be performed in a temperature range of 430
to 490°C. In addition, a composition of the hot-dip galvanized bath during the hot-dip
galvanizing is not particularly limited, and may be a pure zinc plating bath or a
zinc-based alloy plating bath containing Si, Al, Mg, and the like.
[Alloying Heat Treatment]
[0135] Furthermore, if necessary, an alloyed hot-dip galvanized steel sheet may be obtained
by performing an alloying heat treatment on the hot-dip galvanized steel sheet. In
the present disclosure, the alloying heat treatment process condition is not particularly
limited, and may be provided as a normal condition. As an example, an alloying heat
treatment process may be performed in a temperature range of 480 to 600°C.
[0136] Furthermore, final cooling and coarse rolling process may be performed after the
hot-dip galvanizing or alloying heat treatment.
[Final Cooling]
[0137] The hot-dip galvanized or alloyed heat-treated steel sheet may be finally cooled
to further introduce fresh martensite. In this case, the final cooling may be performed
at cooling rate of 3°C/s or more at room temperature.
[0138] When the cooling rate is less than 3°C/s during the cooling, a fresh martensite phase
may not be ensured at an intended level during the cooling process. On the other hand,
an upper limit of the cooling rate is not particularly limited, but the cooling may
be performed at the cooling rate of 50°C/s or less to form a certain fraction of press
martensite.
[Temper Rolling]
[0139] Furthermore, if necessary, by performing the temper rolling on a finally cooled hot-dip
galvanized steel sheet or alloyed hot-dip galvanized steel sheet, a large amount of
potential in the steel may be formed to further improve bake hardenability. In this
case, a reduction ratio thereof may be less than 2% (excluding 0%). When the reduction
ratio is 2% or more, it may be advantageous in terms of potential formation, but side
effects such as plate breakage may occur due to a limitation in equipment capability.
[0140] Hereinafter, the present disclosure will be described in more detail through embodiments.
However, it should be noted that the following embodiments are only for illustrating
and explaining the present disclosure in more detail, and are not intended to limit
the scope of the present disclosure. This is because the scope of the present disclosure
is determined by the matters described in the scope of the patent claim and the matters
reasonably inferred therefrom.
Mode for Invention
[0141] After heating a steel slab having an alloy composition illustrated in Table 1 below
at a temperature of 1050 to 1250°C, each heated slab was subjected to finished hot
rolling at Ar3 to Ar3+50°C to manufacture a hot-rolled steel sheet. Thereafter, each
hot-rolled steel sheet was coiled at 400 to 700°C and then cooled to room temperature
at cooling rate of 0.1°C/s or less. Thereafter, the cooled hot-rolled steel sheet
was subjected to cold rolling at a cold reduction ratio of 45 to 75%, thereby manufacturing
a cold-rolled steel sheet.
[0142] The cold rolling was performed in a rolling mill comprised of six stands, and a cumulative
reduction ratio of stands 1 to 3 was performed under the conditions illustrated in
Table 2 below.
[0143] Then, each cold-rolled steel sheet was continuously annealed under the conditions
illustrated in Table 2 below, followed by step-by-step cooling (primary-secondary
cooling and maintenance). After the secondary cooling and maintenance process is completed,
the steel sheet was reheated at a temperature of 490°C or less, and then, a process
of maintaining at that temperature was performed. The maintaining process was performed
for 30 seconds after the secondary cooling.
[0144] Then, the steel sheet was galvanized in a hot-dip galvanizing bath at 430 to 490°C
and cooled to room temperature at cooling rate of 5°C/s, and was then subjected to
temper rolling to less than 2%, thereby manufacturing a hot-dip galvanized steel sheet.
In this case, some steels were subjected to the galvanizing treatment, followed by
alloying heat treatment.
[Table 1]
Division |
Alloy Composition (weight %) |
Expression 1 |
C |
Si |
Mn |
P |
S |
Sol.A |
Nb |
Ti |
B |
Cr |
Mo |
Sb |
Inventive Steel1 |
0.1 4 |
0.6 0 |
2.4 1 |
0.01 1 |
0.00 2 |
0.035 |
0.02 1 |
0.04 0 |
0 |
0.4 1 |
0.2 0 |
0 |
1.81 |
Inventive Steel2 |
0.1 6 |
0.7 0 |
2.3 9 |
0.01 0 |
0.00 3 |
0.035 |
0.02 0 |
0.01 1 |
0 |
0.2 2 |
0.1 0 |
0.03 0 |
2.08 |
Inventive Steel3 |
0.1 6 |
1.0 0 |
2.2 1 |
0.00 8 |
0.00 2 |
0.030 |
0 |
0 |
0.001 6 |
0.5 1 |
0 |
0 |
2.40 |
Inventive Steel4 |
0.1 5 |
0.9 0 |
2.2 2 |
0.00 8 |
0.00 3 |
0.030 |
0 |
0 |
0.001 0 |
0.7 1 |
0 |
0.03 4 |
2.21 |
Inventive Steel5 |
0.1 7 |
1.0 0 |
2.2 0 |
0.00 8 |
0.00 2 |
0.030 |
0 |
0 |
0.001 4 |
0.4 2 |
0 |
0.03 8 |
2.48 |
Inventive Steel6 |
0.1 8 |
1.0 0 |
1.9 9 |
0.00 8 |
0.00 4 |
0.030 |
0 |
0 |
0.001 5 |
0.6 9 |
0 |
0.03 6 |
2.56 |
Comparati ve Steel1 |
0.0 6 |
0.4 1 |
2.2 9 |
0.01 2 |
0.00 2 |
0.032 |
0.03 1 |
0.02 1 |
0.002 7 |
0.8 4 |
0.1 2 |
0.01 8 |
0.96 |
Comparati ve Steel2 |
0.0 7 |
0.4 0 |
2.3 2 |
0.02 1 |
0.00 4 |
0.035 |
0.05 1 |
0.02 0 |
0.002 4 |
0.8 5 |
0.1 3 |
0 |
1.03 |
Comparati ve Steel3 |
0.0 7 |
0.6 0 |
2.3 1 |
0.02 2 |
0.00 2 |
0.035 |
0.02 1 |
0.02 1 |
0.002 0 |
0.8 5 |
0.1 2 |
0 |
1.25 |
Comparati ve Steel4 |
0.1 1 |
0.6 0 |
2.6 1 |
0.01 1 |
0.00 1 |
0.025 |
0.02 3 |
0.01 5 |
0 |
0.5 0 |
0.2 1 |
0.03 1 |
1.56 |
Comparati ve Steel5 |
0.1 1 |
0.3 0 |
2.6 3 |
0.01 5 |
0.00 1 |
0.125 |
0.02 1 |
0.01 5 |
0 |
0.5 1 |
0.2 1 |
0.03 0 |
1.31 |
[Table 2]
Divisi on |
coilin g Temper ature (°C) |
Cold Rolling |
Anneal ing |
Primary Cooling |
Secondary Cooling |
Reheat ing |
Mainte nance |
1 to 3 Stand Reduc tion Ratio (%) |
Total Reduc tion Ratio (%) |
Temper ature (°C) |
End Temper ature (°C) |
Cooli ng Veloc ity (°C /s) |
End Temper ature (°C) |
Cooli ng Veloc ity (°C /s) |
Temper ature (°C) |
Time (sec) |
Invent ive Steel 1 |
540 |
30 |
60 |
860 |
550 |
5.4 |
280 |
12.8 |
450 |
55 |
Invent ive Steel 2 |
620 |
35 |
55 |
840 |
680 |
2.9 |
480 |
9.5 |
460 |
60 |
Invent ive Steel 3 |
650 |
25 |
70 |
850 |
600 |
4.5 |
450 |
7.1 |
480 |
45 |
Invent ive Steel 4 |
570 |
40 |
50 |
860 |
480 |
6.8 |
300 |
8.5 |
480 |
40 |
Invent ive Steel 5 |
520 |
30 |
65 |
870 |
500 |
6.6 |
300 |
8.5 |
420 |
65 |
Invent ive Steel 6 |
600 |
25 |
60 |
810 |
550 |
4.6 |
300 |
11.9 |
460 |
45 |
Compar ative Steel 1 |
750 |
25 |
45 |
770 |
650 |
3.9 |
550 |
4.7 |
550 |
45 |
Compar ative Steel 2 |
580 |
15 |
60 |
830 |
680 |
2.7 |
500 |
9.5 |
530 |
60 |
Compar ative Steel 3 |
620 |
30 |
70 |
850 |
750 |
1.8 |
300 |
21.4 |
300 |
20 |
Compar ative Steel 4 |
600 |
40 |
55 |
850 |
680 |
3.2 |
200 |
22.8 |
460 |
25 |
Compar ative Steel 5 |
300 |
35 |
75 |
810 |
680 |
3.1 |
450 |
10.9 |
560 |
50 |
[0145] The microstructure of each steel sheet manufactured according to the conditions described
above were observed and illustrated in Table 3 below. In this case, in the microstructure
of each steel plate, fractions of tempered martensite (TM), bainite (B), ferrite (F),
fresh martensite (FM) and retained austenite (A) were measured using FE-SEM, an image
analyzer, EBSD, and XRD, after Nital corrosion at 1/4t (t: steel plate thickness (unit
mm)) point of a steel sheet. In this case, a share of retained austenite was also
measured using the EBSD.
[0146] Furthermore, tensile properties were evaluated in an L direction using the DIN standard
for test specimens collected for a tensile test of each steel plate.
[0147] Furthermore, the hole expansion ratio (HER) was measured by pushing up a circular
hole punched in a 10mm diameter according to the ISO 16630 procedure with a cone punch
until cracks occurred in the specimen, and measuring a ratio of an initial hole diameter
to a hole diameter after change, and was calculated using the following expression.

(Here, D means a hole diameter (mm) when the crack penetrates through the steel sheet
in a thickness direction, and D
0 means an initial hole diameter (mm) .
[Table 3]
Division |
Microstructure (Area%) |
Mechanical Properties |
|
TM+B |
F |
FM |
A |
Share (ATM+B/AT) |
YS (MPa) |
TS (MPa) |
E1 (%) |
YR |
HER (%) |
Expression 2 |
Inventive Steel 1 |
55 |
35 |
5 |
5 |
90 |
799 |
1065 |
14.7 |
0.75 |
30 |
10.4 |
Inventive Steel 2 |
48 |
32 |
13 |
7 |
91 |
755 |
1042 |
15.8 |
0.72 |
25 |
10.9 |
Inventive Steel 3 |
57 |
29 |
7 |
7 |
94 |
780 |
1041 |
15.3 |
0.75 |
31 |
11.0 |
Inventive Steel 4 |
60 |
25 |
7 |
8 |
95 |
845 |
1073 |
16.6 |
0.79 |
35 |
12.2 |
Inventive Steel 5 |
64 |
27 |
2 |
7 |
91 |
848 |
1077 |
15.4 |
0.79 |
40 |
11.3 |
Inventive Steel 6 |
58 |
26 |
7 |
9 |
98 |
823 |
1072 |
17.1 |
0.77 |
32 |
12.3 |
Comparative Steel 1 |
31 |
56 |
9 |
4 |
76 |
500 |
891 |
14.0 |
0.56 |
11 |
8.8 |
Comparative Steel 2 |
35 |
30 |
32 |
3 |
72 |
752 |
1081 |
10.3 |
0.70 |
21 |
6.7 |
Comparative Steel 3 |
85 |
5 |
8 |
2 |
65 |
986 |
1076 |
9.0 |
0.92 |
30 |
7.7 |
Comparative Steel 4 |
82 |
12 |
3 |
3 |
77 |
947 |
1084 |
10.3 |
0.87 |
32 |
8.3 |
Comparative Steel 5 |
38 |
20 |
40 |
2 |
70 |
802 |
1211 |
10.6 |
0.66 |
20 |
5.8 |
YS: Yield Strength, TS: Tensile Strength, El: Elongation Ratio, YR: Yield Ratio (YS/TS) |
[0148] As illustrated in Tables 1 to 3, in Inventive Examples 1 to 6 satisfying both the
alloy component system and the manufacturing conditions proposed in the present disclosure,
a tempered martensite phase and a bainite phase were formed in a total of 40 to 80
area% as intended, and retained austenite phases were mainly formed around the tempered
martensite phase and the bainite phase. Accordingly, a yield ratio thereof may satisfy
0.6 to 0.9 as well as a high strength of 980 MPa, and an elongation ratio of 10% or
more and a hole expansion ratio of 20% or more may be secured.
[0149] In other words, in the steel sheet manufactured by the present disclosure, the strength
and ductility may be significantly improved at the same time, and specifically, by
satisfying the value of Relational Expression 2, it may be possible to secure the
crashworthiness and formability targeted in the present disclosure.
[0150] On the other hand, in Comparative steels 1 to 5 that deviate from Relational Expression
1 proposed in the present disclosure and do not satisfy the manufacturing conditions,
at least one physical property was degraded because an intended microstructure was
not formed.
[0151] Comparative Steel 1 was unable to secure the target level of strength due to an excessive
ferrite phase, and had a poor hole expansion ratio and deviated from Relational Expression
2, which made it impossible to secure crashworthiness and formability.
[0152] Comparative Steels 2 and 5 were excessively formed on a fresh martensite phase to
secure high strength, whereas they deviated from Relational Expression 2, which made
it impossible to secure crashworthiness and formability.
[0153] Comparative Steel 3 had a small ferrite phase, and the ductility thereof significantly
decreased as the retained austenite phase was not formed around a hard phase.
[0154] In Comparative Steel 4, the retained austenite phase was not formed around the hard
phase to lead to a relatively low elongation ratio, it was impossible to secure crashworthiness
and formability as the Comparative Steel 4 deviated from Relational Expression 2.
[0155] FIG. 1 illustrates a graph of a change in mechanical properties (Relational Expression
2) according to a value of Relational Expression 1.
[0156] As illustrated in FIG. 1, it may be confirmed that when the value of Relational Expression
1 proposed in the present disclosure satisfies 1.7 or more, a value of Relational
Expression 2 may be ensured to be 9 or more.
[0157] FIG. 2 illustrates an image of a microstructure of Inventive Steel 4 measured by
the EBSD.
[0158] As illustrated in FIG. 2, it may be confirmed that the retained austenite phase is
mainly formed around the tempered martensite phase and the bainite phase, and it may
be seen that the ferrite phase and the fresh martensite phase are properly formed.