AU2021400482A1

AU2021400482A1 - High-hardness armored steel having excellent low-temperature impact toughness, and manufacturing method therefor

Info

Publication number: AU2021400482A1
Application number: AU2021400482A
Authority: AU
Inventors: Nam-Young Cho; Seng-Ho YU
Original assignee: Posco Co Ltd
Current assignee: Posco Holdings Inc
Priority date: 2020-12-18
Filing date: 2021-11-04
Publication date: 2023-07-06
Also published as: KR102498158B1; WO2022131543A1; EP4265793A1; KR20220088234A

Abstract

The present invention can provide armored steel having high hardness and excellent low-temperature impact toughness to provide excellent ferroelasticity, and a method for manufacturing same.

Description

Title of Invention: HIGH-HARDNESS ARMORED STEEL HAVING EXCELLENT LOW-TEMPERATURE IMPACT TOUGHNESS, AND MANUFACTURING METHOD THEREFOR

Technical Field

[0001] The present disclosure relates to a material appropriate for armored vehicles, explosion-proof structures, and the like, and more particularly to armored steel having excellent low temperature impact toughness and having high hardness, and a manufacturing method therefor.

Background Art

[0002] Armored steel is a material of which a surface is made very hard for its main function of blocking bullets, and is used where protection is required, such as for an exterior of armored vehicles used in battlefields. Since bulletproof performance is directly related to human life, research to improve the performance of bulletproof materials has been actively conducted in the past, and recently, a non-ferrous material such as titanium and aluminum has been developed.

[0003] The non-ferrous material has an advantage of weight reduction compared to a steel material, but is relatively expensive and has poor workability. As compared to the non ferrous material, since the steel material is relatively inexpensive and may change physical properties such as harness relatively easily, the steel material is widely used as a material for self-propelled artillery, wheeled armored vehicles, and the like.

[0004] Hardness is one of the important physical properties for securing the performance of armored steel, but simple high hardness does not guarantee bulletproof performance. A high hardness characteristic is a factor that increases resistance to bullets from penetrating through a material, but the material having high hardness may be relatively easily broken, so the high hardness characteristic cannot necessarily guarantee excellent bulletproof performance. Therefore, there is a need to develop a material that can simultaneously secure brittle fracture resistance to external impact as well as high hardness characteristics rather than simply promoting high hardness of

199120021 (GHMatters) P121860.AU the material.

[0005] (Prior art Document)

[0006] (Patent Document 1) Korean Patent Publication No. 10 2018-0043788 (published on April 30, 2018)

Summary of Invention Technical Problem

[0007] An aspect of the present disclosure is to provide armored steel having high hardness characteristics and excellent low temperature impact toughness and a manufacturing method therefor.

[0008] An object of the present disclosure is not limited to the above description. The object of the present disclosure will be understood from the entire content of the present specification, and a person skilled in the art to which the present disclosure pertains will understand an additional object of the present disclosure without difficulty.

Solution to Problem

[0009] According to an aspect of the present disclosure, a high hardness armored steel having excellent low-temperature impact toughness includes, by weight: 0.41 to 0.50% of carbon (C), 1.0 to 2.0% of silicon (Si), 0.5 to 1.6% of manganese (Mn), 0.5 to 1.2% of nickel (Ni), 0.4 to 1.5% of chromium (Cr), 0.05% or less of phosphorus (P), 0.02% or less of sulfur (S), 0.006% or less of nitrogen (N), 0.07% or less of aluminum (Al) (excluding 0%), 0.1 to 0.5% of molybdenum (Mo), 0.01 to 0.05% of niobium (Nb), 0.0002 to 0.005% of boron (B), 0.0005 to 0.004% of calcium (Ca), with a balance of iron (Fe) and inevitable impurities, satisfying the following [Relational Expression 1], wherein a tempered martensite base structure including retained austenite is included as a microstructure.

[0010] [Relational Expression 1]

[0011] (A-200) / 100 1.0

[0012] In the Relational Expression 1, A refers to a value calculated by the following Relational Expression 2.

[0013] [Relational Expression 2]

[0014] A = 539 - 423*[C] - 30.4*[Mn] - 17.7*[Ni] - 12.1*[Cr] 7.5*[Mo]

[0015] In the Relational Expression 2, [C], [Mn], [Ni], [Cr], and [Mo] refer to contents (weight %)of carbon (C), manganese (Mn), nickel (Ni), chromium (Cr), and molybdenum (Mo) included

199120021 (GHMatters) P121860.AU in the steel sheet, and 0 is substituted when the corresponding element is not intentionally added.

[0016] The armored steel may further include, by weight: at least one of 0.005 to 0.025% of titanium (Ti) and 0.2% or less of vanadium (V).

[0017] A fraction of the tempered martensite may be 90% or more by area, and a fraction of retained austenite may be 1% by area to 10% by area.

[0018] The armored steel may have a surface hardness of 560 to 630 HB, and an impact absorption energy of 12 J or more at 400C.

[0019] The armored steel may have a thickness of 25 to 60 mm.

[0020] According to an aspect of the present disclosure, a manufacturing method for a high-hardness armored steel having excellent low-temperature impact toughness includes operations of: preparing a steel slab including, by weight: 0.41 to 0.50% of carbon (C), 1.0 to 2.0% of silicon (Si), 0.5 to 1.6% of manganese (Mn), 0.5 to 1.2% of nickel (Ni), 0.4 to 1.5% of chromium (Cr), 0.05% or less of phosphorus (P), 0.02% or less of sulfur (S), 0.006% or less of nitrogen (N), 0.07% or less of aluminum (Al) (excluding 0%), 0.1 to 0.5% of molybdenum (Mo), 0.01 to 0.05% of niobium (Nb), 0.0002 to 0.005% of boron (B), 0.0005 to 0.004% of calcium (Ca), with a balance of iron (Fe) and inevitable impurities, satisfying the following [Relational Expression 1]; heating the steel slab in a temperature range of 1050 to 1250 0C; rough rolling the heated steel slab in a temperature range of 950 to 1150 0C; subjecting the heated steel slab to finish hot rolling in a temperature range of 850 to 950 0C after the rough rolling to manufacture a hot-rolled steel sheet; and cooling the hot-rolled steel sheet to a temperature of 50 to 250 0C at a cooling rate of 3 °C/s or more and then air cooling the same to room temperature.

[0021] [Relational Expression 1]

[0022] (A-200) / 100 1.0

[0023] In the Relational Expression 1, A refers to a value calculated by the following Relational Expression 2.

[0024] [Relational Expression 2]

[0025] A = 539 - 423*[C] - 30.4*[Mn] - 17.7*[Ni] - 12.1*[Cr] 7.5*[Mo]

[0026] In the Relational Expression 2, [C], [Mn], [Ni], [Cr], and [Mo] refer to contents (weight %) of carbon (C), manganese

199120021 (GHMatters) P121860.AU

(Mn), nickel (Ni), chromium (Cr), and molybdenum (Mo) included in the steel slab, and 0 is substituted when the corresponding element is not intentionally added.

[0027] The steel slab may further include, by weight: at least one of 0.005 to 0.25% of titanium (Ti) and 0.2% or less of vanadium (V).

[0028] The hot-rolled steel sheet may have a thickness of 25 to 60 mm.

[0029] The solution to the above problems does not enumerate all the features of the present disclosure, and various beneficial merits of the present disclosure are not limited to the descriptions above, and may be more easily understood in a process of describing specific exemplary embodiments in the present disclosure.

Advantageous Effects of Invention

[0030] As set forth above, according to the present disclosure, armored steel having excellent low-temperature toughness while having ultra-high hardness may be provided.

[0031] In particular, the present disclosure may provide armored steel having a target level of physical properties without performing a further heat treatment from optimization of an alloy composition and manufacturing conditions, and thus, is economically favorable.

[0032] The effect of the present disclosure is not limited to the above, and may be interpreted as including an effect that can be inferred from the description described below by those skilled in the art.

Best Mode for Invention

[0033] The present disclosure relates to a high-hardness armored steel having excellent low-temperature impact toughness and a manufacturing method therefor. Hereinafter, preferred embodiments of the present disclosure will be described. Embodiments of the present disclosure may be modified in various forms, and the scope of the present disclosure should not be construed as being limited to the embodiments described below. The present embodiments are provided to those skilled in the art to further elaborate the present disclosure.

[0034]

[0035] The present inventors have studied in depth, in order to

199120021 (GHMatters) P121860.AU provide a steel material having excellent physical properties such as high hardness characteristics, low-temperature impact toughness, and the like, which are essentially required physical properties, as a material which may be appropriately applied to wheeled armored vehicles, explosion-proof structures, and the like.

[0036]

[0037] In particular, the bulletproof performance of the steel material was intended to be improved by an economically favorable method, and thus, the present disclosure was provided.

[0038] Hereinafter, armored steel according to an aspect of the present disclosure will be described in more detail.

[0039]

[0040] Hereinafter, a steel composition of the present disclosure will be described in more detail. Hereinafter,

% represents a content of each element based on weight, unless otherwise particularly specified.

[0041]

[0042] Carbon (C): 0.41 to 0.50%

[0043] Carbon (C) is an element which is effective for improving strength and hardness in steel having a low-temperature transformation phase such as a martensite or bainite phase, and is effective for improving hardenability. In order to sufficiently obtain the effect described above, 0.41% or more of carbon (C) may be included. Preferably, a lower limit of a content of carbon (C) may be 0.42%. However, when carbon (C) is excessively added, there may be a concern that weldability and toughness of steel are deteriorated, so in the present disclosure, an upper limit of the content of carbon (C) may be limited to 0.50%. Preferably, the upper limit of the content of carbon (C) may be 0.49%.

[0044]

[0045] Silicon (Si): 1.0 to 2.0%

[0046] Silicon (Si) is an element which is effective for improving strength due to solid solution strengthening together with a deoxidation effect, and is also an element suppressing formation of carbides such as cementite in a steel material containing a certain amount or more of C to promote production of residual austenite. In particular, since residual austenite which is uniformly distributed in steel having a low-temperature transformation phase such as martensite and bainite may

199120021 (GHMatters) P121860.AU effectively contribute to improvement of impact toughness without strength reduction. Therefore, in order to sufficiently obtain the effect described above, in the present disclosure, 1.0% or more of Si may be included. Preferably, a lower limit of a content of silicon (Si) may be 1.1%, and more preferably, the lower limit of the content of silicon (Si) may be 1.2%. However, when silicon (Si) is excessively added, weldability may be rapidly deteriorated, so in the present disclosure, an upper limit of the content of silicon (Si) may be limited to 2.0%. Preferably, the upper limit of the content of silicon (Si) may be 1.9%, and more preferably, the upper limit of the content of silicon (Si) may be 1.8%.

[0047]

[0048] Manganese (Mn): 0.5 to 1.6%

[0049] Manganese (Mn) is an element favorable to suppress production of ferrite and lower an Ar3 temperature, thereby improving quenching properties of steel to increase strength and toughness. In order to obtain a target level of hardness in the present disclosure, 0.5% or more of manganese (Mn) may be included. Preferably, a lower limit of a content of manganese (Mn) may be 0.6%, and more preferably, the lower limit of the content of manganese (Mn) may be 0.7%. However, when manganese (Mn) is excessively added, there may be a concern that weldability is deteriorated and center segregation is encouraged to deteriorate the physical properties in the center part of steel. Therefore, in the present disclosure, an upper limit of the content of manganese (Mn) may be limited to 1.6%. Preferably, the upper limit of the content of manganese (Mn) may be 1.5%, and more preferably, the upper limit of the content of manganese (Mn) may be 1.4%.

[0050]

[0051] Nickel (Ni): 0.5 to 1.2%

[0052] Nickel (Ni) is an element favorable to improve both strength and toughness of steel. In order to obtain the above described effects, in the present disclosure, 0.5% or more of nickel (Ni) may be included. Preferably, a lower limit of a content of nickel (Ni) may be 0.6%, and more preferably, the lower limit of the content of nickel (Ni) may be 0.7%. However, since nickel (Ni) is an expensive element, when nickel (Ni) is excessively added, manufacturing costs may be greatly increased, so in the present disclosure, an upper limit of the

199120021 (GHMatters) P121860.AU content of nickel (Ni) may be limited to 1.2%. Preferably, the upper limit of the content of nickel (Ni) may be 1.17%, and more preferably, the upper limit of the content of nickel (Ni) may be 1.15%.

[0053]

[0054] Chromium (Cr): 0.4 to 1.5%

[0055] Chromium (Cr) is an element of increasing quenching properties of steel to improve strength, and effectively contributing to securing hardness in a surface part and a center part of steel. In addition, since Cr is a relatively inexpensive element, chromium (Cr) is also an element for economically securing hardness and toughness. In order to obtain the above described effects, in the present disclosure, 0.4% or more of chromium (Cr) may be included. Preferably, a lower limit of a content of chromium (Cr) may be 0.45%. However, when chromium (Cr)is excessively added, weldability may be deteriorated, so in the present disclosure, an upper limit of the content of chromium (Cr) may be limited to 1.5%. Preferably, the upper limit of the content of chromium (Cr) may be 1.4%, and more preferably, the upper limit of the content of chromium (Cr) may be 1.3%.

[0056]

[0057] Phosphorous (P): 0.05% or less

[0058] Phosphorus (P) is an element which is inevitably contained in steel, and is also an element which deteriorates toughness of the steel. Thus, it is preferred to lower a content of P as much as possible. In the present disclosure, even in the case of including phosphorus (P) up to 0.05%, the physical properties of the steel are not significantly influenced, and thus, an upper limit of the content of phosphorus (P) may be limited to 0.05%. More favorably, the content thereof may be limited to 0.03% or less. However, 0% may be excluded considering an inevitably contained level.

[0059]

[0060] Sulfur (S): 0.02% or less

[0061] Sulfur (S) is an element which is inevitably contained in steel, and is also an element forming MnS inclusions to deteriorate toughness of steel. Thus, it is preferred to lower a content of S as much as possible. In the present disclosure, even in the case of including sulfur (S) up to 0.02%, the physical properties of the steel are not significantly influenced, and thus, an upper limit of the content of sulfur

199120021 (GHMatters) P121860.AU

(S) may be limited to 0.02%. More favorably, the content thereof may be limited to 0.01% or less. However, 0% may be excluded considering an inevitably contained level.

[0062]

[0063] Nitrogen (N): 0.006% or less

[0064] Nitrogen (N)is an element which is favorable to improve strength of steel by forming precipitates in steel, but when a content of nitrogen (N) is more than a certain level, which may rather cause deterioration in toughness of steel. In the present disclosure, there is no difficulty in securing strength even when N is not contained, so in the present disclosure, an upper limit of a content of nitrogen (N) may be limited to 0.006%. However, 0% may be excluded considering an inevitably contained level.

[0065]

[0066] Aluminum (Al): 0.07% or less (excluding 0%)

[0067] Aluminum (Al) is an element effective for lowering an oxygen content in molten steel as a deoxidizing agent of steel. However, when aluminum (Al) is excessively added, cleanliness of steel may be impaired, so in the present disclosure, an upper limit of a content of aluminum (Al) may be limited to 0.07%.

[0068] On the other hand, when the content of Al is excessively lowered, a load may occur in a steelmaking process and manufacturing costs may be increased, and thus, in the present disclosure, 0% may be excluded from a lower limit of the content of aluminum (Al), and the lower limit thereof may be 0.01%.

[0069]

[0070] Molybdenum (Mo): 0.1 to 0.5%

[0071] Molybdenum (Mo) is an element favorable to increase quenching properties of steel, and in particular, to improve hardness of a thick material having a certain thickness or more. In order to sufficiently obtain the effect described above, 0.1% or more of molybdenum (Mo) may be included. Preferably, a lower limit of a content of molybdenum (Mo) may be 0.11%, and more preferably, the lower limit of the content of molybdenum (Mo) may be 0.12%. However, when molybdenum (Mo) is excessively added, not only manufacturing costs may be increased, but also weldability may be deteriorated, so in the present disclosure, an upper limit of the content of molybdenum (Mo) may be limited to 0.5%. Preferably, an upper limit of the content of molybdenum (Mo) may be 0.48%, and more particularly, the upper limit of the

199120021 (GHMatters) P121860.AU content of molybdenum (Mo) may be 0.45%.

[0072]

[0073] Niobium (Nb): 0.01 to 0.05%

[0074] Niobium (Nb) is an element which is effective for increasing hardenability of austenite by being dissolved in austenite, and increasing strength of steel and suppressing growth of austenite crystal grains by forming carbonitrides such as Nb(C,N). In order to sufficiently obtain the effect described above, in the present disclosure, 0.1% or more of niobium (Ni) may be included. However, when niobium (Ni) is excessively added, coarse precipitates may be formed to become a starting point of brittle fracture, so in the present disclosure, an upper limit of a content of niobium (Nb) may be limited to 0.05%. Preferably, the upper limit of the content of niobium (Nb) content may be 0.04%, and more preferably, the upper limit of the content of niobium (Nb) may be 0.03%.

[0075]

[0076] Boron (B): 0.0002 to 0.005%

[0077] Boron (B) is an element effectively contributing to strength improvement by increasing quenching properties of steel even with a small addition amount thereof. In order to sufficiently obtain the effect,in the present disclosure, 0.0002% or more of boron (B) may be contained. Preferably, a lower limit of a content of boron (B) may be 0.0005%, and more preferably, the lower limit of the content of boron (B) may be 0.001%. However, when boron (B) is excessively added, toughness and weldability of steel may be rather deteriorated, so in the present disclosure, an upper limit of the content of boron (B) may be limited to 0.005%. Preferably, the upper limit of the content of boron (B) may be 0.004%, and more preferably, the upper limit of the content of boron (B) may be 0.003%.

[0078]

[0079] Calcium (Ca): 0.0005 to 0.004%

[0080] Calcium (Ca) an element having a good binding force with sulfur (S) and producing CaS on the periphery (around) MnS, thereby suppressing elongation of MnS to improve toughness in a direction perpendicular to a rolling direction. In addition, Caps produced by adding Ca has an effect of increasing corrosion resistance under a humid external environment. In order to sufficiently obtain the effect described above, 0.0005% or more of Ca may be included. Preferably, a lower limit of a content of

199120021 (GHMatters) P121860.AU calcium (Ca) may be 0.001%. However, when calcium (Ca) is excessively added, defects such as nozzle clogging, or the like, may be caused in a steelmaking operation, so in the present disclosure, an upper limit of the content of calcium (Ca) may be limited to 0.004%. Preferably, the upper limit of the content of calcium (Ca)may be 0.003%.

[0081]

[0082] In addition to the above-described alloy composition, armored steel of the present disclosure may further include the following elements for the purpose of favorably securing target physical properties.

[0083] Specifically, the armored steel of the present disclosure may further include at least one of titanium (Ti) and vanadium (V).

[0084]

[0085] Titanium (Ti): 0.005 to 0.025%

[0086] Titanium (Ti) is an element which maximizes the effect of boron (B), which is an element favorable to improve quenching properties of steel. That is, titanium (Ti) is bonded to nitrogen (N) in steel to be precipitated into TiN to reduce the content of solid-solubilized N, while suppressing formation of BN of B therefrom to increase solid-solubilized B, thereby maximizing improvement of quenching properties. In order to sufficiently obtain the effect described above, 0.005% or more of titanium (Ti) may be contained. However, when titanium (Ti) is excessively added, coarse TiN precipitates may be formed and toughness of steel may be deteriorated, so in the present disclosure, an upper limit of the content of titanium (Ti) may be limited to 0.025%.

[0087]

[0088] Vanadium (V): 0.2% or less (including 0%)

[0089] Vanadium (V) is an element favorable to form a VC carbide when reheating after hot rolling, thereby suppressing growth of austenite crystal grains and improving quenching properties of steel to secure strength and toughness. However, since vanadium (V) is a relatively expensive element, an upper limit of a content of vanadium (V) may be limited to 0.2% in consideration of manufacturing costs.

[0090]

[0091] The armored steel according to an aspect of the present disclosure may include a remainder of Fe and other inevitable

199120021 (GHMatters) P121860.AU impurities in addition to the components described above. However, since in the common manufacturing process, unintended impurities may be inevitably incorporated from raw materials or the surrounding environment, the component may not be excluded. Since these impurities are known to any person skilled in the common manufacturing process, the entire contents thereof are not particularly mentioned in the present specification. In addition, further addition of effective ingredients other than the above-mentioned ingredients is not entirely excluded.

[0092]

[0093] The armored steel according to an aspect of the present disclosure may satisfy the following [Relational Expression 1].

[0094]

[0095] [Relational Expression 1]

[0096] (A - 200) / 100 1.0

[0097] In Relational Expression 1, A refers to a value calculated by the following [Relational Expression 2].

[0098] [Relational Expression 2]

[0099] A = 539 - 423*[C] - 30.4*[Mn] - 17.7*[Ni] - 12.1*[Cr] 7.5*[Mo]

[00100] In Relational Expression 2, [C], [Mn], [Ni], [Cr], and

[Mo] refer to contents (weight %) of carbon (C), manganese (Mn), nickel (Ni), chromium (Cr), and molybdenum (Mo) included in a steel sheet, and 0 is substituted if the corresponding element is not intentionally added.

[00101]

[00102] The inventors of the present disclosure have conducted in-depth research on a method capable of securing high-hardness characteristics and excellent low-temperature impact toughness of a steel sheet at the same time, and have derived that it is effective to control not only a content range of each respective alloy composition, but also a relative content range of the specific alloy composition included in the steel sheet. In the present disclosure, not only the content range of each respective alloy composition included in the steel sheet is controlled to be within a certain range, but also the relative content range of carbon (C), manganese (Mn), chromium (Cr), nickel (Ni), and molybdenum (Mo) is controlled to be within a certain range, as illustrated in [Relational Expression 1] and [Relational Expression 2], so that high hard characteristics and excellent low-temperature impact toughness may be effectively compatible.

199120021 (GHMatters) P121860.AU

[00103]

[00104] Armored steel of the present disclosure having the alloy composition described above may have a tempered martensite base structure including retained austenite as a microstructure, and may further include other inevitable structures. In this case, a fraction of retained austenite may be 1% by area to 10% by area , and a fraction of tempered martensite may be 90% or more by area.

[00105] Retained austenite is a structure remaining without being completely phase transformed into martensite during a rapid cooling heat treatment, and has relatively low hardness but excellent toughness as compared to martensite. For this effect, the armored steel of the present disclosure may include 1% or more by area of retained austenite, more preferably 2% or more by area of retained austenite. On the other hand, when the retained austenite is excessively formed, the low-temperature impact toughness greatly increases, but it is difficult to secure target hardness characteristics. Therefore, in the present disclosure, an upper limit of the fraction of the retained austenite may be set to be 10% by area. The upper limit of the fraction of the retained austenite may be 6% by area, and a lower limit of the fraction of the tempered martensite fraction may be 94% by area.

[00106]

[00107] Meanwhile, the armored steel of the present disclosure may have the above-described microstructural configuration over the entire thickness.

[00108]

[00109] The armored steel of the present disclosure having the above-described alloy composition and the proposed microstructure may have a thickness of 25 to 60 mm and a surface hardness of 560 to 630HB, exhibiting ultra-high hardness, and may have an impact absorption energy of 12 J or more at -40 °C, exhibiting excellent low-temperature toughness.

[00110] Here, the surface hardness refers to an average value of three measurements after milling a surface of the armored steel at 2 mm in a thickness direction using a Brinell hardness tester (load: 3000 kgf, 10 mm tungsten injection port).

[00111]

[00112] Hereinafter, a manufacturing method for armored steel according to an aspect of the present disclosure will be

199120021 (GHMatters) P121860.AU described in more detail.

[00113]

[00114] A steel slab having a predetermined component is prepared. Since the steel slab of the present disclosure has an alloy composition corresponding to the alloy composition of the hot-rolled steel sheet described above (including [Relational Expression 1] and [Relational Expression 2]), a description of the alloy composition of the steel slab is substituted for the description of the alloy composition of the above-described hot rolled steel sheet.

[00115]

[00116] In brief, the armored steel may be manufactured by preparing a steel slab satisfying the alloy composition described above, and then subjecting the steel slab to the processes of [heating - rolling- cooling - self tempering]. Hereinafter, each process condition will be described in detail.

[00117]

[00118] [Steel slab heating process]

[00119] First, a steel slab having the alloy composition suggested in the present disclosure is prepared, which may be then heated in a temperature range of 1050 to 12500C.

[00120] When the temperature is lower than 10500C during heating, deformation resistance of steel is increased, so that a subsequent rolling process may not be effectively performed. On the other hand, when the temperature is higher than 12500C, austenite crystal grains are coarsened, so that non-uniform structure may be formed.

[00121] Therefore, the steel slab may be heated in a temperature range of 1050 to 12500C.

[00122]

[00123] [Rolling process]

[00124] The steel slab heated as described above may be rolled, and then may be subjected to rough rolling and finish hot rolling to manufacture a hot-rolled steel sheet.

[00125] First, the heated steel slab is roughly rolled in a temperature range of 950 to 11500C to be manufactured into a bar, which may be then subjected to finish hot rolling in a temperature range of 850 to 9500C.

[00126] When the temperature is lower than 9500C during the rough rolling, a rolling load is increased to reduce the steel slab relatively weakly, and thus, deformation is not sufficiently

199120021 (GHMatters) P121860.AU transferred to a center of the slab in the thickness direction, and as a result, defects such as voids may not be removed. On the other hand, when the temperature thereof is higher than 11500C, recrystallization granularity is coarsened, which may be harmful to toughness.

[00127] When the temperature is lower than 8500C in the finish hot rolling, two-phase region rolling is performed, so that there is a concern that ferrite may be produced in the microstructure. On the other hand, when the temperature thereof is higher than 9500C, the granularity of the final structure is coarsened to deteriorate low-temperature toughness.

[00128]

[00129] [Cooling and Self tempering process]

[00130] The hot rolled steel sheet manufactured through the rolling process described above is cooled to 50 to 2500C at a 0 rate of 3 C/s and then air-cooled to room temperature.

[00131]

[00132] The cooling is performed to obtain a martensite base structure to satisfy high hardness, and when a cooling end temperature is higher than 250 0C, phase transformation from austenite particles produced by hot rolling into martensite may not be completed, and thus hardness of a final product may be deteriorated. On the other hand, when the cooling end temperature is lower than 50 0C, the phase transformation therefrom into martensite is completely completed, which is favorable in terms of securing hardness, but latent heat in a material decreases, so that a self-tempering effect cannot be obtained. Self tempering is a method that can produce an effect similar to that of normal tempering through latent heat of a material, which is rapidly cooled without a separate subsequent process. Therefore, an end of the cooling of the hot-rolled steel sheet is preferably performed in a range of 50 to 250 0C. A lower limit of the cooling end temperature is more preferably 60 0C, even more preferably 70 °C, and most preferably 80 °C. In addition, an upper limit of the cooling end temperature is more preferably 220 0C, even more preferably 2000C, and most preferably 1800C.

[00133]

[00134] Meanwhile, if a cooling rate during the cooling is less than 3 °C/s, bainite and ferrite, which are relatively soft phases, may be generated, so that phase transformation by rapid cooling, that is a martensite structure cannot be sufficiently

199120021 (GHMatters) P121860.AU obtained. However, as a thickness of the steel sheet increases, the cooling rate inevitably decreases physically, so there is no separate upper limit. Therefore, the cooling rate is preferably 3 °C/s or more. The cooling rate is more preferably 3.5 °C/s or more, more preferably 4 °C/s or more, and most preferably 5 °C/s or more.

[00135]

[00136] In a process of cooling the steel sheet to a temperature range of 50 to 250 °C, and then air cooling the same to room temperature, self-tempering may be performed by latent heat in a central portion thereof, and martensite introduced during cooling may be softened through self-tempering, thereby effectively securing low-temperature impact toughness. In the present disclosure, the thickness of the hot-rolled steel sheet manufactured through a series of manufacturing processes does not be specifically limited, but in terms of securing the self tempering effect, a lower limit of the thickness thereof may be limited to 25 mm. Preferably, the hot-rolled steel sheet may have a thickness of 25 to 60 mm.

Mode for Invention

[00137] Hereinafter, armored steel of the present disclosure and a manufacturing method therefor will be described in more detail through specific examples. It should be noted that the following examples are only for understanding of the present invention, and are not intended to specify the scope of the present invention. The scope of the present invention may be determined by the matters described in the claims and the matters reasonably inferred therefrom. It should be noted that the following examples are only for understanding of the present invention, and are not intended to specify the scope of the present invention. The scope of the present invention may be determined by the matters described in the claims and the matters reasonably inferred therefrom.

[00138]

[00139] (Example)

[00140] After preparing a steel slab having alloy compositions of Table 1 below, [heating-rolling-cooling-self tempering] were performed according to process conditions illustrated in Table 2 below to manufacture each hot-rolled steel sheet. In this case, after being water cooled to a cooling end temperature, air

199120021 (GHMatters) P121860.AU cooling was applied to room temperature. Alloy compositions not listed in Table 1 refers to inevitable impurities and iron (Fe). In addition, a part marked with"-" in Table 1 means that the corresponding component was not intentionally added, which is preferable to be interpreted as 0% by weight within an error range.

[00141]

[00142] [Table 1]

[st Alloy composition(by weight%) [Relatio ee C Si Mn P* S* Ni Cr Mo Nb V Al Ca* Ti B* N* nal 1 Expressi ty on 1]

pe 0.4 1.1 0.8 0.4 0.4 0.0 0.0 0.0 0.01 A 4 9 5 73 24 3 2 - 3 4 3 21 7 15 50 1.14 0.3 1.4 1.2 0.9 0.5 0.3 0.0 0.0 B 6 2 6 70 23 5 7 3 2 - 4 20 - 18 46 1.22

0.4 1.7 1.1 0.7 0.8 0.4 0.0 0.0 0.0 C 2 5 7 69 20 4 5 5 2 2 3 19 - 21 48 0.99 0.4 1.4 0.8 1.1 0.6 0.3 0.0 0.0 0.01 D 9 1 8 71 19 2 6 4 2 - 4 22 2 20 47 0.75 0.4 1.3 1.0 0.8 0.7 0.4 0.0 0.0 E 5 4 4 75 24 7 2 1 3 - 3 20 - 19 45 0.90

0.4 1.0 0.5 0.6 1.1 0.3 0.0 0.0 0.01 F 1 8 3 72 21 6 6 7 2 - 3 21 4 20 44 1.21 P*, S*, Ca*, B*, and N* are represented in units of ppm

[00143]

[00144] [Table 2] Speci Steel Thickn Slab Rolling Cooling men type ess heating Rough Finish Cooling end Cooling rate No. (mm) (°C) rolling hot temperature (°C/s)

(°C) rolling (°C)

(°C) 1 A 25 1127 1073 899 289 45.7 2 A 40 1124 1065 923 27 17.8 3 A 50 1150 1004 915 19 10.6 4 B 30 1137 1065 908 156 32.5 5 B 50 1148 1000 934 178 11.3 6 B 60 1161 986 927 144 8.6 7 C 25 1126 1061 910 146 42.1

199120021 (GHMatters) P121860.AU

8 C 40 1145 1049 936 263 14.8 9 C 60 1129 1002 941 145 7.5 10 D 50 1163 1037 911 128 2.2 11 D 50 1162 1028 944 122 10.4 12 D 60 1155 1033 925 121 6.6 13 E 25 1129 1075 909 136 40.5 14 E 40 1146 1034 932 21 15.2 15 E 40 1150 1038 938 137 11.9 16 E 60 1165 997 922 129 8.4 17 F 50 1137 1030 925 170 10.5

[00145]

[00146] Thereafter, a microstructure and mechanical properties of each hot-rolled steel sheet were measured, and the results thereof were shown in Table 3.

[00147] The microstructure of each hot-rolled steel sheet was cut into an arbitrary size as a specimen to manufacture a mirror surface, a Nital etching solution was used to corrode the specimen, and then an optical microscope and a scanning electron microscope (SEM) were used to observe a 1/2t point which was a thickness center part. In this case, a fraction of the microstructure was measured by electron back-scattered diffraction (EBSD) analysis.

[00148] In addition, hardness and toughness of each hot-rolled steel sheet were measured using a Brinell hardness tester (load: 3000 kgf, 10 mm tungsten injection port) and a Charpy impact tester, respectively. In this case, in the surface hardness, an average value of three measurements after a milling process of the surface of the hot-rolled sheet at 2 mm was used, and in the Charpy impact test, a specimen was collected at 1/4t point in the thickness direction, and then an average value of three measurements at -40°C was used.

[00149]

[00150] [Table 3] Specime Steel Microstructure Surface Impact n type (area %) hardness toughness No. TM F or B R-y (HB) (J,@-40°C) 1 A 23 B: 77 0 465 76 2 A 100 - 0 647 6 3 A 100 - 0 652 5 4 B 95 - 5 514 23

199120021 (GHMatters) P121860.AU

5 B 96 - 4 496 22 6 B 96 - 4 521 19 7 C 97 - 3 589 16 8 C 18 B: 82 0 473 65 9 C 96 - 4 582 19 10 D 0 F: 74, P: 26 0 267 102 11 D 94 - 6 612 17 12 D 95 - 5 620 16 13 E 96 - 4 594 21 14 E 99 - 1 668 4 15 E 97 - 3 602 15 16 E 97 - 3 599 18 17 F 98 - 2 551 15 TM: Tempered martensite, B: Bainite, F: Ferrite, P: Pearlite, R-y: Retained austenite

[00151]

[00152] As shown in Tables 1 to 3, it can be seen that specimens satisfying the alloy composition and process conditions of the present disclosure have a surface harness of 560 to 630 HB and an impact absorption energy of 12 J or more at -40°C, but specimens not satisfying at least one of the alloy compositions or process conditions of the present disclosure do not have a surface hardness of 560 to 630 HB or an impact absorption energy of 12 J or more at -400C at the same time.

[00153]

[00154] While example embodiments have been shown and described above, it will be apparent to those skilled in the art that modifications and variations could be made without departing from the scope of the present disclosure as defined by the appended claims.

199120021 (GHMatters) P121860.AU

Claims

1. A high-hardness armored steel having excellent low temperature impact toughness, comprising by weight: 0.41 to 0.50% of carbon (C), 1.0 to 2.0% of silicon (Si), 0.5 to 1.6% of manganese (Mn), 0.5 to 1.2% of nickel (Ni), 0.4 to 1.5% of chromium (Cr), 0.05% or less of phosphorus (P), 0.02% or less of sulfur (S), 0.006% or less of nitrogen (N), 0.07% or less of aluminum (Al) (excluding 0%), 0.1 to 0.5% of molybdenum (Mo), 0.01 to 0.05% of niobium (Nb), 0.0002 to 0.005% of boron (B), 0.0005 to 0.004% of calcium (Ca), with a balance of iron (Fe) and inevitable impurities, satisfying the following

[Relational Expression 1], wherein a tempered martensite base structure including retained austenite is included as a microstructure,

[Relational Expression 1] (A-200) / 100 1.0 in the Relational Expression 1, A refers to a value calculated by the following Relational Expression 2,

[Relational Expression 2] A = 539 - 423*[C] - 30.4*[Mn] - 17.7*[Ni] - 12.1*[Cr] 7.5*[Mo] in the Relational Expression 2, [C], [Mn], [Ni], [Cr], and

[Mo] refer to contents (weight %)of carbon (C), manganese (Mn), nickel (Ni), chromium (Cr) and molybdenum (Mo) included in a steel sheet, and 0 is substituted when the corresponding element is not intentionally added.

2. The high-hardness armored steel having excellent low temperature impact toughness of claim 1, wherein the armored steel further comprises, by weight: at least one of 0.005 to 0.025% of titanium (Ti) and 0.2% or less of vanadium (V).

3. The high-hardness armored steel having excellent low temperature impact toughness of claim 1, wherein a fraction of the tempered martensite is 90% or more by area, and a fraction of the retained austenite is 1% by area to 10% by area.

4. The high-hardness armored steel having excellent low temperature impact toughness of claim 1, wherein the armored steel has a surface hardness of 560 to 630 HB and an impact

199120021 (GHMatters) P121860.AU absorption energy of 12 J or more at -40°C.

5. The high-hardness armored steel having excellent low temperature impact toughness of claim 1, wherein the armored steel has a thickness of 25 to 60 mm.

6. A manufacturing method for a high-hardness armored steel having excellent low-temperature impact toughness, comprising operations of: preparing a steel slab including by weight: 0.41 to 0.50% of carbon (C), 1.0 to 2.0% of silicon (Si), 0.5 to 1.6% of manganese (Mn), 0.5 to 1.2% of nickel (Ni), 0.4 to 1.5% of chromium (Cr), 0.05% or less of phosphorus (P), 0.02% or less of sulfur (S), 0.006% or less of nitrogen (N), 0.07% or less of aluminum (Al) (excluding 0%), 0.1 to 0.5% of molybdenum (Mo), 0.01 to 0.05% of niobium (Nb), 0.0002 to 0.005% of boron (B), 0.0005 to 0.004% of calcium (Ca), with a balance of iron (Fe) and inevitable impurities, satisfying the following

[Relational Expression 1]; heating the steel slab in a temperature range of 1050 to 1250 °C; rough rolling the heated steel slab in a temperature range of 950 to 1150 °C; subjecting the heated steel slab to finish hot rolling in a temperature range of 850 to 950 0C after the rough rolling to manufacture a hot-rolled steel sheet; and cooling the hot-rolled steel sheet to a cooling end temperature of 50 to 250 °C at a cooling rate of 3 °C/s or more and then air cooling the same to room temperature,

[Mo] refer to contents (weight %) of carbon (C), manganese (Mn), nickel (Ni), chromium (Cr), and molybdenum (Mo) included in the steel slab, and 0 is substituted when the corresponding element is not intentionally added.

199120021 (GHMatters) P121860.AU

7. The manufacturing method for a high-hardness armored steel having excellent low-temperature impact toughness of claim 6, wherein the steel slab further comprises, by weight: at least one of 0.005 to 0.025% of titanium (Ti) and 0.2 % or less of vanadium (V).

8. The manufacturing method for a high-hardness armored steel having excellent low-temperature impact toughness of claim 6, wherein the hot-rolled steel sheet has a thickness of 25 to 60 mm.

199120021 (GHMatters) P121860.AU