AU2021402965A9

AU2021402965A9 - High hardness armored steel having excellent low-temperature impact toughness, and manufacturing method therefor

Info

Publication number: AU2021402965A9
Application number: AU2021402965A
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: 2024-04-18
Also published as: WO2022131536A1; KR20220088240A; KR102498149B1; EP4265786A1; AU2021402965A1

Abstract

The present invention can provide: armored steel having high hardness and excellent low-temperature impact toughness to provide excellent ferroelectricity; and a manufacturing method therefor.

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 on the battlefield. 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 most important physical properties for securing the performance of armor steel, but simple high hardness does not guarantee bulletproof performance. A high hardness characteristic is a factor that increases resistance to bullets 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

19906548_1 (GHMatters)P121840.AU the material.

[0005] (Prior art Document)

[0006] (Patent Document) 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: 0.29 to 0.37% 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] 10*[C]*[Si] 4

[0012] In Relational Expression 1, [C] and [Si] refer to contents (weight %) of carbon (C) and silicon (Si) included in the steel sheet, and 0 is substituted when the corresponding element is not intentionally added.

[0013] 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).

[0014] A fraction of the tempered martensite may be 90% or more

19906548_1 (GHMatters)P121840.AU by area, and a fraction of the retained austenite may be 1% by area to 10% by area.

[0015] The armored steel may have a surface hardness of 460 to 540 HB, and an impact absorption energy of 19 J or more at 400C.

[0016] The armored steel may have a thickness of 5 to 40 mm.

[0017] 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: 0.29 to 0.37% 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 12500C; rough rolling the heated steel slab in a temperature range of 950 to 11500C; subjecting the heated steel slab to finish hot rolling in a temperature range of 850 to 9500C after the rough rolling to manufacture a hot-rolled steel sheet; performing a primary heat-treatment of heating the hot-rolled steel sheet to a temperature range of 880 to 9300C and then cooling the same to a cooling end temperature of 1500C or lower at a cooling rate of 10°C/s or more; and performing a secondary heat treatment of heating the primarily heat-treated hot-rolled steel sheet to a temperature range of 3500C or lower and maintaining the same.

[0018] [Relational Expression 1]

[0019] 10*[C]*[Si] 4

[0020] In Relational Expression 1, [C] and [Si] refer to contents (weight %) of carbon (C) and silicon (Si) included in the steel slab, and 0 is substituted when the corresponding element is not intentionally added.

[0021] The steel slab 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).

[0022] A residence time during the primary heat treatment may be 1.3t * 10 minutes (t: plate thickness (mm)) or more.

19906548_1 (GHMatters)P121840.AU

[0023] A holding time during the secondary heat treatment may be 1.9t+10 minutes (t: plate thickness (mm)) or more.

[0024] 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

[0025] As set forth above, according to the present disclosure, armored steel having excellent low-temperature toughness while having ultra-high hardness may be provided.

[0026] The present disclosure may provide armored steel having a target level of physical properties without performing a further heat treatment from optimization of alloy compositions and manufacturing conditions, and thus, is economically favorable.

[0027] 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

[0028] 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.

[0029]

[0030] The present inventors have studied in depth, in order to 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.

19906548_1 (GHMatters)P121840.AU

[0031] 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.

[0032]

[0033] Hereinafter, armored steel according to an aspect of the present disclosure will be described in more detail.

[0034]

[0035] 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.

[0036]

[0037] Carbon (C): 0.29 to 0.37%

[0038] 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, 0.29% or more of carbon (C) may be included. Preferably, a lower limit of a content of carbon (C) may be 0.30%, and more preferably, the lower limit of the content of carbon (C) may be 0.31%. 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 0.37%. Preferably, the upper limit of the content of carbon (C) may be 0.36%.

[0039]

[0040] Silicon (Si): 1.0 to 2.0%

[0041] 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 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 silicon (Si) may be included. Preferably, a lower limit of a content of silicon (Si) may be 1.1%, and more

19906548_1 (GHMatters)P121840.AU 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%.

[0042]

[0043] Manganese (Mn): 0.5 to 1.6%

[0044] 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, so 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 1.45%.

[0045]

[0046] Nickel (Ni): 0.5 to 1.2%

[0047] Nickel (Ni) is an element favorable to improve both strength and toughness of steel. In order to obtain the effect described above, 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, 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 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%.

[0048]

[0049] Chromium (Cr): 0.4 to 1.5%

19906548_1 (GHMatters)P121840.AU

[0050] 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 chromium (Cr) is a relatively inexpensive element, chromium (Cr) is also an element for economically securing hardness and toughness. In order to obtain the effect described above, 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 0.5%. 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%.

[0051]

[0052] Phosphorous (P): 0.05% or less

[0053] 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.

[0054]

[0055] Sulfur (S): 0.02% or less

[0056] 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 (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.

[0057]

[0058] Nitrogen (N): 0.006% or less

[0059] Nitrogen (N) is an element which is favorable to improve

19906548_1 (GHMatters)P121840.AU 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.

[0060]

[0061] Aluminum (Al): 0.07% or less (excluding 0%)

[0062] 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%.

[0063] On the other hand, when the content of aluminum (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%.

[0064]

[0065] Molybdenum (Mo): 0.1 to 0.5%

[0066] 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 obtain the effect described above, in the present disclosure, 0.1% or more of molybdenum (Mo) may be included. Preferably, a lower limit of a content of molybdenum (Mo) may be 0.15%, and more preferably, the lower limit of the content of molybdenum (Mo) may be 0.2%. 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, the upper limit of the content of molybdenum (Mo) may be 0.48%, and more preferably, the upper limit of the content of molybdenum (Mo) may be 0.45%.

[0067]

[0068] Niobium (Nb): 0.01 to 0.05%

[0069] Niobium (Nb) is an element which is effective for increasing hardenability of austenite by being dissolved in

19906548_1 (GHMatters)P121840.AU 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, 0.01% 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%.

[0070]

[0071] Boron (B): 0.0002 to 0.005%

[0072] 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%.

[0073]

[0074] Calcium (Ca): 0.0005 to 0.004%

[0075] 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, CaS 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 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%.

19906548_1 (GHMatters)P121840.AU

[0076]

[0077] 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.

[0078] Specifically, the armored steel of the present disclosure may further include at least one of titanium (Ti) and vanadium (V).

[0079]

[0080] Titanium (Ti): 0.005 to 0.025%

[0081] 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%.

[0082]

[0083] Vanadium (V): 0.2% or less (including 0%)

[0084] 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.

[0085]

[0086] The armored steel according to an aspect of the present disclosure may include a remainder of Fe and other inevitable 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

19906548_1 (GHMatters)P121840.AU addition, further addition of effective ingredients other than the above-mentioned ingredients is not entirely excluded.

[0087]

[0088] The armored steel according to an aspect of the present disclosure may satisfy the following [Relational Expression 1].

[0089]

[0090] [Relational Expression 1]

[0091] 10*[C]*[Si] 4

[0092] In Relational Expression 1, [C] and [Si] refer to contents (weight %) of carbon (C) and silicon (Si) included in the steel sheet, and 0 is substituted if the corresponding element is not intentionally added.

[0093]

[0094] 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) and silicon (Si) is controlled to be within a certain range, as illustrated in [Relational Expression 1], so that high hard characteristics and excellent low-temperature impact toughness may be effectively compatible. 10*[C]*[Si] defined by the Relational Expression 1 may be 4.3 or more.

[0095]

[0096] The armored steel of the present disclosure having the alloy composition described above may havea tempered martensite base structure including retained austenite as a microstructure, and may further include other inevitable structures. In this case, preferably, 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.

[0097] 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 armor steel of the present disclosure may include 1% or more

19906548_1 (GHMatters)P121840.AU 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 5% by area, and a lower limit of the fraction of the tempered martensite may be 95% by area.

[0098]

[0099] Meanwhile, the armor steel of the present disclosure may have the above-described microstructural configuration over the entire thickness.

[00100]

[00101] The armor steel of the present disclosure having the above-described alloy composition and the proposed microstructure may have a thickness of 5 to 40 mm, and have a surface hardness of 460 to 540HB, exhibiting ultra-high hardness, and an impact absorption energy of 19 J or more at -40°C, exhibiting excellent low-temperature toughness.

[00102] 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).

[00103]

[00104] Hereinafter, a manufacturing method for armored steel according to an aspect of the present disclosure will be described in more detail.

[00105]

[00106] 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]), 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.

[00107]

[00108] 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 - primary heat treatment

19906548_1 (GHMatters)P121840.AU

(quenching) - secondary heat treatment (tempering)]. Hereinafter, each process condition will be described in detail.

[00109]

[00110] [Steel slab heating process]

[00111] First, a steel slab having the alloy composition proposed in the present disclosure is prepared, which may be then heated in a temperature range of 1050 to 12500C.

[00112] When the temperature is lower than 10500C during the 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.

[00113] Therefore, the steel slab may be heated in a temperature range of 1050 to 12500C.

[00114]

[00115] [Rolling process]

[00116] 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.

[00117] 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.

[00118] 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 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.

[00119] When the temperature is lower than 8500C during 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.

[00120]

[00121] [Primary heat treatment (quenching) process]

[00122] The hot-rolled steel sheet manufactured through the

19906548_1 (GHMatters)P121840.AU rolling process described above is air cooled to room temperature, and then heated to a residence time of 1.3t + 10 minutes (t: plate thickness (mm)) or more in a temperature range of 880 to 9300C.

[00123]

[00124] The heating is performed for reverse transformation of a hot-rolled steel sheet composed of ferrite and pearlite into an austenite single phase. When a heating temperature is lower than 8800C, austenitization is not sufficiently achieved, and coarse soft ferrite is mixed, and thus hardness of a final product may be deteriorated. On the other hand, when the temperature thereof is higher than 9300C, there is an effect of increasing quenching properties due to coarse austenite crystal grains, but there is a disadvantage in terms of thermal efficiency during mass production. Therefore, heating during a primary heat treatment is preferably performed in a range of 880 to 9300C. A lower limit of the heating temperature is more preferably 8850C, even more preferably 8900C, and most preferably 8950C. In addition, an upper limit of the heating temperature is more preferably 9250C, even more preferably 9200C, and most preferably 9150C.

[00125]

[00126] Meanwhile, when a residence time during the primary heat treatment is less than 1.3t + 10 minutes (t: plate thickness (mm)), austenitization does not sufficiently occur, so that phase transformation by subsequent rapid cooling, that is, a martensitic structure cannot be sufficiently obtained. Therefore, a residence time during the heating is preferably 1.3t + 10 minutes (t: plate thickness (mm)) or more. The residence time during the heating is more preferably 1.3t + 12 minutes (t: plate thickness (mm)) or more, even more preferably 1.3t + 13 minutes (t: plate thickness (mm)) or more, and most preferably 1.5t + 15 minutes (t: plate thickness (mm)) or more.

[00127]

[00128] In the present disclosure, an upper limit of the residence time during the primary heat treatment is not particularly limited. However, when the residence time during the heating exceeds 1.3 t + 60 minutes (t: plate thickness (mm)), austenite crystal grains become coarse, so that quenching properties may increase, but there may be a disadvantage in that productivity is relatively lowered. Therefore, the residence

19906548_1 (GHMatters)P121840.AU time during the heating is preferably 1.3t + 60 minutes (t: plate thickness (mm)) or less. The residence time during the heating is more preferably 1.3t + 50 minutes (t: plate thickness (mm)) or less, even more preferably 1.3t + 40 minutes (t: plate thickness (mm)) or less, and most preferably 1.3t + 30 minutes (t: plate thickness (mm)) or less.

[00129]

[00130] Thereafter, the heated hot-rolled steel sheet may be cooled to 1200C or lower at a cooling rate of 10°C/s or more with respect to a plate thickness center portion(e.g., 1/2t point, t: plate thickness (mm) ) . In this case, the cooling is preferably rapid cooling through water cooling. When the cooling rate is less than 10°C/s or a cooling end temperature is higher than 1200C, there is a concern that a ferrite phase may be formed or a bainite phase may be excessively formed during cooling. Therefore, the cooling is preferably performed to 120°C or lower at a cooling rate of 10°C/s or more. The faster the cooling rate, the more favorable it is to form the microstructure to be obtained in the present disclosure. Meanwhile, in the present disclosure, an upper limit of the cooling rate is not particularly limited, and it may be appropriately set in consideration of facility limitations by any person skilled in the art. The cooling end temperature is more preferably 1000C or lower, even more preferably 800C or lower, and most preferably 500C or lower.

[00131]

[00132] [Secondary heat treatment (tempering) process]

[00133] The hot-rolled steel sheet manufactured through the above-described primary heat treatment may be heated to a temperature range of 3500C or lower and maintained for 1.9t+10 minutes (t: plate thickness (mm)) or more.

[00134]

[00135] The reheating is performed to release internal stress of a hot-rolled steel sheet fully composed of martensite after quenching. As dislocation density inside a material thereof decreases through such a tempering heat treatment, hardness may decrease somewhat, but toughness may be secured. In the case of armor steel, since it is necessary not only to have high hardness but also to have excellent low-temperature impact toughness, such a subsequent tempering heat treatment is essential if no special element is added. When a tempering temperature exceeds

19906548_1 (GHMatters)P121840.AU

3500C, the dislocation density inside the martensite is excessively reduced, and thus hardness of a final product may be lowered. On the other hand, when the tempering temperature is too low, the decrease in hardness can be prevented, but the dislocation density becomes too high, which is disadvantageous in terms of securing impact toughness. In the present disclosure, a lower limit of the tempering temperature is not separately specified, but is preferably 1000C or higher in order to obtain the effect described above. It is preferable to perform tempering, more preferably at a temperature of 1250C or higher, and even more preferably 1500C or higher.

[00136] In the present disclosure, a lower limit of the holding time during the tempering is not particularly limited. However, when the holding time during the tempering is less than 1.9t

+ 10 minutes (t: plate thickness (mm)), a thickness center portion compared to the surface thereof may not be sufficiently heated, as the heat treatment is performed at a relatively low temperature for a short time. Therefore, the holding time during the tempering is preferably 1.9t + 10 minutes (t: plate thickness (mm) ) or more. The holding time during the tempering is more preferably 1.9t + 12 minutes (t: plate thickness (mm)) or more, more preferably 1.9t + 15 minutes (t: plate thickness (mm)) or less, and most preferably 1.9t + 20 minutes (t: plate thickness (mm)) or more.

[00137] After tempering, it can be cooled to room temperature by air cooling. Through such a tempering process, the hot-rolled steel sheet according to an aspect of the present disclosure may have softened tempered martensite as a base structure.

[00138]

[00139] The hot-rolled steel sheet obtained through the above described series of manufacturing processes is a steel material having a thickness of 5 to 40 mm, and can provide excellent bullet-proof resistance by securing high hardness and high toughness.

Mode for Invention

[00140] 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 disclosure, and are not intended to specify the scope of the present

19906548_1 (GHMatters)P121840.AU disclosure. The scope of the present disclosure may be determined by the matters described in the claims and the matters reasonably inferred therefrom.

[00141]

[00142] (Example)

[00143] After preparing a steel slab having alloy compositions of Table 1 below, [heating - rolling - heat treatment (quenching) - heat treatment (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 cooling was applied to room temperature. The tempering performed thereafter also applied air cooling to room temperature after performing a heat treatment at a specific temperature. Alloy compositions not listed in Table 1 refer to unavoidable 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.

[00144] [Table 1] St Alloy composition(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 A 0.4 1.2 1.1 74 16 1.1 0.8 0.2 0.0 0.0 0.0 27 0.01 20 50 6.13 9 5 6 2 1 7 3 3 3 5 B 0.2 0.2 0.8 72 20 0.2 0.5 0.4 0.0 - 0.0 21 - 19 45 0.50 4 1 9 5 6 4 1 4 C 0.3 1.4 0.9 71 21 0.9 0.7 0.3 0.0 0.0 0.0 20 - 17 44 4.43 1 3 4 2 2 9 2 4 3 D 0.3 1.2 1.2 75 23 0.7 0.5 0.4 0.0 - 0.0 19 - 18 49 4.39 4 9 2 9 6 2 4 3 E 0.3 1.3 1.4 76 19 1.1 0.6 0.2 0.0 - 0.0 16 0.01 21 45 4.93 6 7 5 3 8 8 3 4 2 F 0.2 1.0 0.6 73 20 0.6 0.4 0.1 0.0 - 0.0 18 0.01 20 43 3.13 9 8 2 6 3 5 2 3 4 P*, S*, Ca*, B*, and N* are represented in units of ppm

[00145] [Table 2] Spec Stee Thic Slab Rolling First heat treatment Second heat

19906548_1 (GHMatters)P121840.AU imen 1 knes heat (quenching) treatment No. type s ing (tempering) (mm) (°C) Rough Finish Heati Resid Cooli Cooli Heatin Holdin rollin hot ng ence ng end ng g g time g rolling tempe time tempe rate temper (min.) (°C) (°C) ratur (min. ratur (°C/s ature e ) e ) (°C) (°C) (°C) 1 A 12 1171 1034 886 908 31 23 50.6 224 46 2 A 18 1125 1018 924 910 37 29 38.8 206 57 3 A 40 1159 1046 911 905 68 22 25.7 217 100 4 B 40 1159 1046 911 905 25 19 63.4 432 40 5 B 10 1165 1040 887 909 47 23 45.5 561 58 6 B 20 1154 1035 916 915 74 24 26.6 306 97 7 C 5 1180 1065 871 902 31 17 71.1 214 38 8 C 15 1176 1063 899 900 45 26 47.5 421 52 9 C 25 1165 1025 923 910 54 23 44.6 223 68 10 D 12 1159 1059 890 911 38 25 64.7 212 44 11 D 25 1163 1024 915 904 55 21 49.8 230 59 12 D 40 1155 1030 922 906 72 224 27.9 226 94 13 E 40 1153 1027 934 899 73 46 26.3 215 14 14 E 25 1149 1029 928 913 54 37 45.9 227 60 15 E 25 1164 1022 909 907 57 29 43.6 391 62 16 E 10 1147 1055 861 909 36 30 65.2 208 39 17 F 15 1150 1062 892 903 40 28 47.3 294 41

[00146]

[00147] Thereafter, a microstructure and mechanical properties of each hot-rolled steel sheet were measured, and the results thereof were shown in Table 3.

[00148] 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 portion. In this case, a fraction of the microstructure was measured by electron back-scattered diffraction (EBSD) analysis.

[00149] In addition, hardness and toughness of each hot-rolled steel sheet were measured using a Brinell hardness tester (load:

19906548_1 (GHMatters)P121840.AU

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.

[00150]

[00151] [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 96 - 4 612 16 2 A 97 - 3 626 15 3 A 97 - 3 615 14 4 B 100 - 0 346 29 5 B 100 - 0 317 32 6 B 99 - 1 453 22 7 C 97 - 3 502 29 8 C 100 - 0 428 34 9 C 97 - 3 489 31 10 D 98 - 2 514 24 11 D 97 - 3 507 26 12 D 56 B: 42, F: 2 0 405 50 13 E 100 - 0 573 16 14 E 97 - 3 493 28 15 E 100 - 0 386 31 16 E 98 - 2 526 24 17 F 99 - 1 447 28 TM: Tempered martensite, B: Bainite, F: Ferrite R-y: Retained austenite

[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 460 to 540 HB and an impact absorption energy of 19 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 460 to 540 HB or an impact absorption energy of 19 J or more at -400C at the same time.

[00153]

19906548_1 (GHMatters)P121840.AU

[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.

19906548_1 (GHMatters) P121840.AU

Claims

1. A high-hardness armored steel having excellent low temperature impact toughness comprising, by weight: 0.29 to 0.37% 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] 10*[C]*[Si] 4 in Relational Expression 1, [C] and [Si] refer to contents (weight %) of carbon (C) and silicon (Si) included in the steel, 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 460 to 540 HB and an impact absorption energy of 19 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 5 to 40 mm.

19906548_1 (GHMatters)P121840.AU

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: 0.29 to 0.37% 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 9500C after the rough rolling to manufacture a hot-rolled steel sheet; performing a primary heat treatment of heating the hot rolled steel sheet to a temperature range of 880 to 9300C and then cooling the same to a cooling end temperature of 1500C or lower at a cooling rate of 10°C/s or more; and performing a secondary heat treatment of heating the primarily heat-treated hot-rolled steel sheet to a temperature range of 3500C or lower and maintaining the same,

[Relational Expression 1] 10*[C]*[Si] 4 in Relational Expression 1, [C] and [Si] refer to contents (weight %) of carbon (C) and silicon (Si) included in the steel slab, and 0 is substituted when the corresponding element is not intentionally added.

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

19906548_1 (GHMatters)P121840.AU

6, wherein a residence time during the primary heat treatment is 1.3t + 10 minutes (t: plate thickness (mm)) or more.

9. The manufacturing method for a high-hardness armored steel having excellent low-temperature impact toughness of claim 6, wherein a holding time during the secondary heat treatment is 1.9t + 10 minutes (t: plate thickness (mm)) or more.

19906548_1 (GHMatters)P121840.AU