HOT PRESSED MEMBER AND METHOD OF MANUFACTURING SAME

Abstract
A hot pressed member having all of: high strength of 1500 MPa or more in tensile strength TS; high ductility of 6.0% or more in uniform elongation uEl; and excellent heat treatment hardenability of increasing in yield stress YS by 150 MPa or more when subjected to heat treatment (baking finish) is provided. A hot pressed member comprises: a predetermined chemical composition (in particular, low C of 0.090% or more and less than 0.30% and high Mn of 3.5% or more and less than 11.0%); a microstructure including a martensite phase of 70.0% or more in volume fraction and a retained austenite phase of 3.0% or more and 30.0% or less in volume fraction; and a dislocation density of 1.0×1016/m2 or more.
Description
TECHNICAL FIELD

The present disclosure relates to a member obtained by hot press forming a thin steel sheet, i.e. a hot pressed member, and a method of manufacturing the same.


BACKGROUND

Recent years have seen strong demand to improve the fuel efficiency of vehicles, for global environment protection. This has led to intense need for lighter automotive bodies. To ensure safety even with thinner automotive members, steel sheets as blank sheets of such members needs to be strengthened. However, strengthening a steel sheet typically leads to lower formability. Hence, problems such as difficulty in forming and degraded shape fixability arise in the manufacture of members using high strength steel sheets as blank sheets.


In view of such problems, a technique of manufacturing a high strength automotive member by applying a hot press process to a steel sheet has been put into actual use. In the hot press process, after heating a steel sheet to an austenite region, the steel sheet is conveyed to a press machine. In the press machine, the steel sheet is formed into a member of a desired shape using a press tool, and simultaneously quenched. In this cooling process (quenching) in the press tool, the microstructure of the member undergoes phase transformation from austenite phase to martensite phase. A high strength member of a desired shape is thus obtained.


Demand to improve the anti-crash property of automotive members has also been growing recently, in order to ensure the safety of drivers and passengers. To meet this demand, increasing the uniform elongation of an automotive member is effective in enhancing the ability to absorb energy upon collision (collision energy absorbing performance). There has thus been strong demand for hot pressed members having excellent uniform elongation as well as high strength.


To meet this demand, JP 2013-79441 A (PTL 1) proposes a hot press formed part obtained by forming a thin steel sheet by a hot press forming method. The hot press formed part proposed in PTL 1 includes: a chemical composition containing, in mass %, C: 0.15% to 0.35%, Si: 0.5% to 3%, Mn: 0.5% to 2%, P: 0.05% or less, S: 0.05% or less, Al: 0.01% to 0.1%, Cr: 0.01% to 1%, B: 0.0002% to 0.01%, Ti: (N content)×4% to 0.1%, and N: 0.001% to 0.01%, with a balance consisting of Fe and incidental impurities; and a microstructure including, in area ratio, martensite: 80% to 97%, retained austenite: 3% to 20%, and a balance: 5% or less. PTL 1 states that, with the proposed technique, a metallic microstructure with an appropriate amount of retained austenite can be obtained, and a hot pressed member having higher ductility can be realized.


JP 2010-65293 A (PTL 2) proposes a hot pressed member having excellent ductility. The hot pressed member described in PTL 2 includes: a composition containing, in mass %, C: 0.20% to 0.40%, Si: 0.05% to 3.0%, Mn: 1.0% to 4.0%, P: 0.05% or less, S: 0.05% or less, Al: 0.005% to 0.1%, and N: 0.01% or less, with a balance consisting of Fe and incidental impurities; and a microstructure in which the area ratio of ferrite phase is 5% to 55% and the area ratio of martensite phase is 45% to 95% with respect to the whole microstructure, and the mean grain size of ferrite phase and martensite phase is 7 μm or less. The hot pressed member has high strength of 1470 MPa to 1750 MPa in tensile strength TS, and high ductility of 8% or more in total elongation El.


CITATION LIST
Patent Literatures

PTL 1: JP 2013-79441 A


PTL 2: JP 2010-65293 A


SUMMARY
Technical Problem

With the techniques described in PTL 1 and PTL 2, high strength of 1500 MPa or more in tensile strength TS is achieved by strengthening martensite phase by C, but there is a problem of insufficient uniform elongation in terms of enhancing collision energy absorbing performance.


A hot pressed member is typically subjected to a baking finish after the production. Heat treatment in this baking finish increases yield stress YS. To enhance anti-crash property, not only high uniform elongation but also high YS is important. Accordingly, a hot pressed member that has excellent heat treatment hardenability so that YS increases as high as possible as a result of the heat treatment in the baking finish is desired. The techniques described in PTL 1 and PTL 2 are, however, not concerned with such heat treatment hardenability.


It could therefore be helpful to provide a hot pressed member having all of: high strength of 1500 MPa or more in tensile strength TS; high ductility of 6.0% or more in uniform elongation uEl; and excellent heat treatment hardenability of increasing in yield stress YS by 150 MPa or more when subjected to heat treatment (baking finish), and an advantageous method of manufacturing the same. In this description, “excellent heat treatment hardenability” means a property that, when a hot pressed member is heat treated, the difference (hereafter denoted by “ΔYS”) between the yield stress YS after the heat treatment and the yield stress YS before the heat treatment is 150 MPa or more.


Solution to Problem

As a result of conducting extensive study on various factors that influence yield stress YS and uniform elongation uEl in a hot pressed member having high strength of 1500 MPa or more in tensile strength TS, we discovered the following.


(A) To achieve high uniform elongation uEl of 6.0% or more, a microstructure having an appropriate amount of retained austenite is necessary. To obtain a microstructure having an appropriate amount of retained austenite with less than 0.30 mass % C, the Mn content needs to be 3.5% or more. Mn contributes to increased strength, so that high strength can be ensured even with less than 0.30% C.


(B) The dislocation density and ΔYS of the hot pressed member correlate with each other. To achieve ΔYS of 150 MPa or more, the dislocation density of the hot pressed member needs to be 1.0×1016/m2 or more.


(C) An appropriate amount of retained austenite can be generated by, before hot pressing a steel sheet containing 3.5% or more Mn as mentioned above, performing heat treatment of heating the steel sheet to a ferrite-austenite dual phase temperature range and retaining the steel sheet at a predetermined temperature in the temperature range for 1 hr or more and 48 hr or less beforehand to cause Mn to concentrate in austenite. Moreover, by subjecting the obtained steel sheet to a predetermined heating process and a hot press forming process, a hot pressed member having a dislocation density of 1.0×1016/m2 or more can be yielded.


The present disclosure is based on these discoveries. We thus provide:


(1) A hot pressed member comprising: a chemical composition containing (consisting of), in mass %, C: 0.090% or more and less than 0.30%, Mn: 3.5% or more and less than 11.0%, Si: 0.01% to 2.5%, P: 0.05% or less, S: 0.05% or less, Al: 0.005% to 0.1%, and N: 0.01% or less, with a balance consisting of Fe and incidental impurities; a microstructure including a martensite phase of 70.0% or more in volume fraction and a retained austenite phase of 3.0% or more and 30.0% or less in volume fraction; a tensile property of 1500 MPa or more in tensile strength TS and 6.0% or more in uniform elongation uEl; and a dislocation density of 1.0×1016/m2 or more.


(2) The hot pressed member according to (1), wherein the chemical composition further contains, in mass %, one or more groups selected from A group: one or more selected from Ni: 0.01% to 5.0%, Cu: 0.01% to 5.0%, Cr: 0.01% to 5.0%, and Mo: 0.01% to 3.0%, B group: one or more selected from Ti: 0.005% to 3.0%, Nb: 0.005% to 3.0%, V: 0.005% to 3.0%, and W: 0.005% to 3.0%, C group: one or more selected from REM: 0.0005% to 0.01%, Ca: 0.0005% to 0.01%, and Mg: 0.0005% to 0.01%, D group: Sb: 0.002% to 0.03%, and E group: B: 0.0005% to 0.05%.


(3) The hot pressed member according to (1) or (2), comprising a coated layer on a surface thereof.


(4) The hot pressed member according to (3), wherein the coated layer is any of a zinc or zinc alloy coated layer and an aluminum or aluminum alloy coated layer.


(5) The hot pressed member according to (4), wherein the zinc or zinc alloy coated layer contains Ni: 10 mass % to 25 mass %.


(6) A method of manufacturing a hot pressed member, the method comprising: heating a slab and hot rolling the slab to obtain a hot rolled steel sheet, the slab having a chemical composition containing, in mass %, C: 0.090% or more and less than 0.30%, Mn: 3.5% or more and less than 11.0%, Si: 0.01% to 2.5%, P: 0.05% or less, S: 0.05% or less, Al: 0.005% to 0.1%, and N: 0.01% or less, with a balance consisting of Fe and incidental impurities; heating the hot rolled steel sheet to a first temperature that is an Ac1 point or more and an Ac3 point or less, retaining the hot rolled steel sheet at the first temperature for 1 hr or more and 48 hr or less, and then cooling the hot rolled steel sheet to obtain a first blank steel sheet; performing a heating process of heating the first blank steel sheet to a second temperature that is the Ac3 point or more and 1000° C. or less and retaining the first blank steel sheet at the second temperature for 900 sec or less; and thereafter performing a hot press forming process of simultaneously press forming and quenching the first blank steel sheet using a press tool for forming, to obtain a hot pressed member.


(7) The method of manufacturing a hot pressed member according to (6), further comprising: cold rolling the first blank steel sheet to obtain a cold rolled steel sheet, before the heating process; and annealing the cold rolled steel sheet to obtain a second blank steel sheet, the annealing including heating the cold rolled steel sheet to a temperature that is the Ac1 point or more and the Ac3 point or less, retaining the cold rolled steel sheet at the temperature, and then cooling the cold rolled steel sheet, wherein the heating process and the hot press forming process are performed on the second blank steel sheet instead of the first blank steel sheet.


(8) The method of manufacturing a hot pressed member according to (6) or (7), wherein the chemical composition further contains, in mass %, one or more groups selected from A group: one or more selected from Ni: 0.01% to 5.0%, Cu: 0.01% to 5.0%, Cr: 0.01% to 5.0%, and Mo: 0.01% to 3.0%, B group: one or more selected from Ti: 0.005% to 3.0%, Nb: 0.005% to 3.0%, V: 0.005% to 3.0%, and W: 0.005% to 3.0%, C group: one or more selected from REM: 0.0005% to 0.01%, Ca: 0.0005% to 0.01%, and Mg: 0.0005% to 0.01%, D group: Sb: 0.002% to 0.03%, and E group: B: 0.0005% to 0.05%.


(9) The method of manufacturing a hot pressed member according to any one of (6) to (8), further comprising forming a coated layer on a surface of the first blank steel sheet or the second blank steel sheet, before the heating process.


(10) The method of manufacturing a hot pressed member according to (9), wherein the coated layer is any of a zinc or zinc alloy coated layer and an aluminum or aluminum alloy coated layer.


(11) The method of manufacturing a hot pressed member according to (10), wherein the zinc or zinc alloy coated layer contains Ni: 10 mass % to 25 mass %.


(12) The method of manufacturing a hot pressed member according to any one of (9) to (11), wherein a coating weight of the coated layer is 10 g/m2 to 90 g/m2 per side.


Advantageous Effect

The hot pressed member according to the present disclosure has all of: high strength of 1500 MPa or more in tensile strength TS; high ductility of 6.0% or more in uniform elongation uEl; and excellent heat treatment hardenability of increasing in yield stress YS by 150 MPa or more when subjected to heat treatment (baking finish). Such a hot pressed member can be advantageously obtained by the method of manufacturing a hot pressed member according to the present disclosure.







DETAILED DESCRIPTION

(Chemical Composition)


The chemical composition of a hot pressed member according to one of the disclosed embodiments is described below. In the following description, “mass %” is simply written as “%” unless otherwise noted.


C: 0.090% or More and Less Than 0.30%


C is an element that increases the strength of the steel. In addition, in heat treatment for the hot pressed member, yield stress is increased by dislocation locking of solute C. To achieve the effects and ensure a tensile strength TS of 1500 MPa or more, the C content is 0.090% or more. If the C content is 0.30% or more, the degree of solid solution strengthening by C increases, which makes it difficult to adjust the tensile strength TS of the hot pressed member to less than 2300 MPa.


Mn: 3.5% or More and Less Than 11.0%


Mn is an element that increases the strength of the steel and also concentrates in austenite to improve the stability of austenite, and is the most important element in the present disclosure. To achieve the effects and ensure a tensile strength TS of 1500 MPa or more and a uniform elongation uEl of 6.0% or more, the Mn content is 3.5% or more. If the Mn content is 11.0% or more, the degree of solid solution strengthening by Mn increases, which makes it difficult to adjust the tensile strength TS of the hot pressed member to less than 2300 MPa.


If the C content and the Mn content are in the respective ranges mentioned above, a hot pressed member having tensile property of 6.0% or more in uniform elongation can be yielded stably, with a tensile strength TS of 1500 MPa or more and preferably less than 2300 MPa. In more detail, to ensure a strength of 1500 MPa or more and less than 1700 MPa in tensile strength TS, it is preferable to set C: 0.090% or more and less than 0.12% and Mn: 4.5% or more and less than 6.5%, or C: 0.12% or more and less than 0.18% and Mn: 3.5% or more and less than 5.5%. To ensure a strength of 1700 MPa or more and less than 1900 MPa in tensile strength TS, it is preferable to set C: 0.090% or more and less than 0.12% and Mn: 6.5% or more and less than 8.5%, or C: 0.12% or more and less than 0.18% and Mn: 5.5% or more and less than 7.5%. To ensure a strength of 1800 MPa or more and less than 1980 MPa in tensile strength TS, it is preferable to set C: 0.18% or more and less than 0.30% and Mn: 3.5% or more and less than 4.5%. To ensure a strength of 2000 MPa or more and less than 2300 MPa in tensile strength TS, it is preferable to set C: 0.090% or more and less than 0.12% and Mn: 8.5% or more and less than 11.0%, C: 0.12% or more and less than 0.18% and Mn: 7.5% or more and less than 11.0%, or C: 0.18% or more and less than 0.30% and Mn: 4.5% or more and less than 6.5%.


Si: 0.01% to 2.5%


Si is an element that increases the strength of the steel by solid solution strengthening. To achieve the effect, the Si content is 0.01% or more. If the Si content is more than 2.5%, surface defects called red scale occur significantly in hot rolling, and also the rolling load increases. The Si content is therefore 0.01% or more and 2.5% or less. The Si content is preferably 0.02% or more. The Si content is preferably 1.5% or less.


P: 0.05% or Less


P is an element that exists in the steel as an incidental impurity, and segregates to crystal grain boundaries and like and causes adverse effects such as a decrease in the toughness of the member. The P content is therefore desirably as low as possible, but 0.05% or less P is allowable. Accordingly, the P content is 0.05% or less, and more preferably 0.02% or less. Excessive dephosphorization leads to higher refining cost, and so the P content is desirably 0.0005% or more.


S: 0.05% or Less


S is contained in the steel incidentally. S exists in the steel as a sulfide inclusion, and decreases the ductility, toughness, and the like of the hot pressed member. The S content is therefore desirably as low as possible, but 0.05% or less S is allowable. Accordingly, the S content is 0.05% or less, and more preferably 0.005% or less. Excessive desulfurization leads to higher refining cost, and so the S content is desirably 0.0005% or more.


Al: 0.005% to 0.1%


Al is an element that acts as a deoxidizer. To achieve the effect, the Al content is 0.005% or more. If the Al content is more than 0.1%, Al combines with nitrogen to form a large amount of nitride. This causes a decrease in the blanking workability and quench hardenability of the steel sheet as a blank sheet. The Al content is therefore 0.005% or more and 0.1% or less. The Al content is preferably 0.02% or more. The Al content is preferably 0.05% or less.


N: 0.01% or Less


N is typically contained in the steel incidentally. If the N content is more than 0.01%, nitrides such as AlN form during heating in hot rolling or hot press. This causes a decrease in the blanking workability and quench hardenability of the steel sheet as a blank sheet. The N content is therefore 0.01% or less. The N content is more preferably 0.0030% or more. The N content is more preferably 0.0050% or less. In the case where N is contained incidentally without adjustment, the N content is approximately less than 0.0025%. To prevent an increase in refining cost, the N content is desirably 0.0025% or more.


In addition to the basic components described above, the chemical composition may contain the following optional components.


A Group: One or More Selected from Ni: 0.01% to 5.0%, Cu: 0.01% to 5.0%, Cr: 0.01% to 5.0%, and Mo: 0.01% to 3.0%


Ni, Cu, Cr, and Mo are each an element that increases the strength of the steel and improves quench hardenability. One or more of them may be selected and added according to need. To achieve the effect, the content of each element is 0.01% or more. To prevent an increase in material cost, the Ni, Cu, and Cr contents are each 5.0% or less, and the Mo content is 3.0% or less. The content of each element is preferably 0.01% or more and 1.0% or less.


B Group: One or More Selected from Ti: 0.005% to 3.0%, Nb: 0.005% to 3.0%, V: 0.005% to 3.0%, and W: 0.005% to 3.0%


Ti, Nb, V, and W are each an element that increases the strength of the steel by precipitation strengthening, and also improves toughness by crystal grain refinement. One or more of them may be selected and added according to need.


Ti has not only the effect of increasing strength and improving toughness, but also the effect of forming a nitride more preferentially than B and improving quench hardenability by solute B. To achieve the effects, the Ti content is 0.005% or more. If the Ti content is more than 3.0%, the rolling load increases extremely in hot rolling, and also the toughness of the hot pressed member decreases. Accordingly, in the case of containing Ti, the Ti content is 0.005% or more and 3.0% or less. The Ti content is preferably 0.01% or more. The Ti content is preferably 1.0% or less.


To achieve the above-mentioned effect by Nb, the Nb content is 0.005% or more. If the Nb content is more than 3.0%, the amount of carbonitride increases, and ductility and lagging destruction resistance decrease. Accordingly, in the case of containing Nb, the Nb content is 0.005% or more and 3.0% or less. The Nb content is preferably 0.01% or more. The Nb content is preferably 0.05%.


V has not only the effect of increasing strength and improving toughness, but also the effect of precipitating as a precipitate or a crystallized product and improving hydrogen embrittlement resistance as a hydrogen trap site. To achieve the effects, the V content is 0.005% or more. If the V content is more than 3.0%, the amount of carbonitride increases considerably, and ductility decreases. Accordingly, in the case of containing V, the V content is 0.005% or more and 3.0% or less. The V content is preferably 0.01% or more. The V content is preferably 2.0% or less.


W has not only the effect of increasing strength and improving toughness, but also the effect of improving hydrogen embrittlement resistance. To achieve the effects, the W content is 0.005% or more. If the W content is more than 3.0%, ductility decreases. Accordingly, in the case of containing W, the W content is 0.005% or more and 3.0% or less. The W content is preferably 0.01% or more. The W content is preferably 2.0% or less.


C Group: One or More Selected from REM: 0.0005% to 0.01%, Ca: 0.0005% to 0.01%, and Mg: 0.0005% to 0.01%


REM, Ca, and Mg are each an element that improves ductility and hydrogen embrittlement resistance by morphological control of an inclusion. One or more of them may be selected and added according to need. To achieve the effect, the content of each element is 0.0005% or more. To prevent a decrease in hot workability, the REM content and the Ca content are each 0.01% or less. To prevent a decrease in ductility caused by the formation of a coarse oxide or sulfide, the Mg content is 0.01% or less. The content of each element is preferably 0.0006% to 0.01%.


D Group: Sb: 0.002% to 0.03%


Sb inhibits the formation of a decarburized layer in the steel sheet surface layer when heating or cooling the steel sheet, and so may be added according to need. To achieve the effect, the Sb content is 0.002% or more. If the Sb content is more than 0.03%, the rolling load increases, and productivity decreases. Accordingly, in the case of containing Sb, the Sb content is 0.002% or more and 0.03% or less. The Sb content is preferably 0.002% or more and 0.02% or less.


E Group: B: 0.0005% to 0.05%


B improves quench hardenability during hot press and toughness after hot press, and so may be added according to need. To achieve the effect, the B content is 0.0005% or more. If the B content is more than 0.05%, the rolling load in hot rolling increases. Besides, martensite phase or bainite phase may form after hot rolling, and cause cracking in the steel sheet. Accordingly, in the case of containing B, the B content is 0.0005% or more and 0.05% or less, and preferably 0.0005% or more and 0.01% or less.


The balance other than the components described above consists of Fe and incidental impurities. As the incidental impurities, O (oxygen): 0.0100% or less is allowable.


(Microstructure)


The microstructure of the hot pressed member in this embodiment is described below.


Martensite Phase: 70.0% or More in Volume Fraction


To ensure a tensile strength TS of 1500 MPa or more, martensite phase of 70.0% or more in volume fraction needs to be the main phase. To contain the desired amount of retained austenite phase, martensite phase is preferably 97% or less.


Retained Austenite Phase: 3.0% to 30.0% in Volume Fraction


Retained austenite phase enhances uniform elongation by a transformation induced plasticity (TRIP) effect upon deformation, and is the most important microstructure in the present disclosure. In this embodiment, the volume fraction of retained austenite phase is 3.0% or more, to achieve a uniform elongation uEl of 6.0% or more. If the volume fraction of retained austenite phase is more than 30.0%, hard martensite phase transformed after the TRIP effect is developed increases excessively, and toughness decreases. The volume fraction of retained austenite phase is therefore 3.0% or more and 30.0% or less. The volume fraction of retained austenite phase is preferably 5.0 or more. The volume fraction of retained austenite phase is preferably 20.0% or less.


For the formation of the above-mentioned appropriate amount of retained austenite phase, it is important to use a steel sheet containing an appropriate amount of Mn, subject the steel sheet to predetermined heat treatment before hot press to cause Mn to concentrate in austenite, and appropriately adjusting a heating process in hot press.


As the balance other than martensite phase and retained austenite phase, 10% or less (including 0%) bainite phase, ferrite phase, cementite, and pearlite in volume fraction in total is allowable.


In the present disclosure, the volume fraction of each phase is determined as follows.


The volume fraction of retained austenite is determined by the following method. An X-ray diffraction test piece is cut out of the hot pressed member, mechanically polished and chemically polished so that the measurement plane is at a position of ¼ of the thickness, and then subjected to X-ray diffraction. Using CoKα radiation as an incident X-ray, the peak integrated intensity for the retained austenite (γ) planes of {200}, {220}, and {311} and the peak integrated intensity for the ferrite (α) planes of {200} and {211} are measured. For a total of six patterns of α{200}-γ{200}, α{200}-γ{220}, α{200}-γ{311}, α{211}-γ{200}, α{211}-γ{220}, and α{211}-γ{311}, the retained y volume fraction obtained from each integrated intensity ratio is calculated. Their mean value is set as “the volume fraction of retained austenite phase”.


The volume fraction of the balance is determined by the following method. A microstructure observation test piece is collected from the hot pressed member so that the observation plane is parallel to the rolling direction and perpendicular to the rolling plane. The observation plane is polished, and etched with a 3 vol % nital solution to expose the microstructure. The microstructure at a position of ¼ of the sheet thickness is observed using a scanning electron microscope (at 1500 magnifications) and photographed. From the obtained micrograph, the microstructure is identified and the microstructure proportion is calculated by image analysis. A phase observed as black with a relatively smooth surface is identified as ferrite phase. A phase observed as white in film or lump form in crystal grain boundaries is identified as cementite. A phase in which ferrite phase and cementite form in layers is identified as pearlite. A phase in which a carbide forms between laths and a phase made of bainitic ferrite having no carbide in grains are identified as bainite phase. The occupancy area ratio of each phase in the micrograph is calculated, and the area ratio is set as the volume fraction on the assumption that the microstructure is homogeneous three-dimensionally.


The volume fraction of martensite phase is calculated by subtracting the volume fraction of the balance and the volume fraction of the retained austenite phase from 100%.


(Dislocation Density)


Dislocation Density: 1.0×1016/m2 or More


The dislocation density of the hot pressed member influences ΔYS, and is the most important index in the present disclosure. It is considered that, when the hot pressed member is subjected to heat treatment (baking finish), solute C locks to mobile dislocations, as a result of which yield stress YS increases. To achieve ΔYS of 150 MPa or more, the dislocation density of the hot pressed member needs to be 1.0×1016/m2 or more. The upper limit of the dislocation density is substantially 5.0×1016/m2. The dislocation density of the hot pressed member is preferably 1.2×1016/m2 or more. The dislocation density of the hot pressed member is preferably 4.5×1016/m2 or less.


In the present disclosure, the dislocation density is determined by the following method. An X-ray diffraction test piece is cut out of the hot pressed member, mechanically polished and chemically polished so that the measurement plane is at a position of ¼ of the thickness, and then subjected to X-ray diffraction. Using CoKα1 radiation as an incident X-ray, the peak half-value widths of α{110}, α{211}, and α{220} are measured. The measured peak half-value widths of α{110}, α{211}, and α{220} are corrected to true half-value widths using a strain-free standard test piece (Si), and then strain (ε) is calculated based on the Willaimson-Hall method. The dislocation density (ρ) is calculated using the strain (ε) and the Burgers vector (b=0.286 nm), according to the following expression:





ρ=14.4×ε2/b2.


(Properties)


The hot pressed member in this embodiment has the following properties: high strength of 1500 MPa or more and preferably less than 2300 MPa in tensile strength TS; high ductility of 6.0% or more and substantially 20% or less in uniform elongation uEl; and ΔYS of 150 MPa or more and substantially 300 MPa or less.


(Coated Layer)


The hot pressed member in this embodiment preferably has a coated layer.


In the case where the steel sheet used as a blank sheet of the hot pressed member is a coated steel sheet, a coated layer remains in the surface layer of the yielded hot pressed member. In such a case, scaling is suppressed during heating in hot press. The hot pressed member can thus be put to use without descaling the surface, which contributes to improved productivity.


The coated layer is preferably a zinc or zinc alloy coated layer or an aluminum or aluminum alloy coated layer. In the case where corrosion resistance is required, a zinc or zinc alloy coated layer is better than an aluminum or aluminum alloy coated layer, because the corrosion rate of the steel substrate can be reduced by the sacrificial protection effect of zinc. Moreover, in the case of hot pressing the coated steel sheet, a zinc oxide film forms in the initial stage of heating in the hot press process, so that evaporation of Zn can be prevented in the subsequent treatment of the hot pressed member.


Examples of the zinc or zinc alloy coating include typical hot-dip galvanizing (GI), galvannealing (GA), and Zn-Ni-based coating. Zn-Ni-based coating is particularly preferable. A Zn-Ni-based coated layer can remarkably suppress scaling during hot press heating, and also prevent liquid metal embrittlement cracking. To achieve the effects, the Zn-Ni-based coated layer preferably contains 10 mass % to 25 mass % Ni. If more than 25% Ni is contained, the effects are saturated.


Examples of the aluminum or aluminum alloy coated layer include Al-10 mass % Si coating.


(Manufacturing Method)


A method of manufacturing a hot pressed member in this embodiment is described below. First, a slab having the above-mentioned chemical composition is heated, and hot rolled to obtain a hot rolled steel sheet. The hot rolled steel sheet is then subjected to predetermined heat treatment (Mn concentration heat treatment) (described later), to obtain a first blank steel sheet. After this, the first blank steel sheet is optionally cold rolled to obtain a cold rolled steel sheet. The cold rolled steel sheet is then subjected to predetermined annealing, to obtain a second blank steel sheet.


The first blank steel sheet or the second blank steel sheet obtained in this way is subjected to a predetermined heating process and a hot press forming process, to obtain a hot pressed member. Each process is described in detail below.


<Obtainment of Hot Rolled Steel Sheet>


The obtainment of the hot rolled steel sheet is not limited, and may be performed according to a usual method. It is preferable to obtain molten steel having the above-mentioned chemical composition by steelmaking in a converter or the like, and process the molten steel into a slab by a continuous casting method in order to prevent macrosegregation. An ingot casting method or a thin slab continuous casting method may be used instead of the continuous casting method.


The obtained slab is cooled to the room temperature, and then charged into a heating furnace for reheating. Alternatively, an energy saving process such as a process of charging the slab into the heating furnace as a warm slab without cooling the slab to the room temperature or a process of heat-retaining the slab for a short time and then immediately hot rolling the slab may be used.


The obtained slab is heated to a predetermined heating temperature, and then hot rolled to obtain a hot rolled steel sheet. The heating temperature is, for example, 1000° C. to 1300° C. The heated slab is typically hot rolled at a finisher entry temperature of 1100° C. or less and a finisher delivery temperature of 800° C. to 950° C., cooled at an average cooling rate of 5° C./s or more, and coiled at a coiling temperature of 300° C. to 750° C., to obtain a hot rolled steel sheet.


<Mn Concentration Heat Treatment>


Following this, the hot rolled steel sheet is heated to a first temperature that is Ac1 point or more and Ac3 point or less, retained at the first temperature for 1 hr or more and 48 hr or less, and then cooled to obtain the first blank steel sheet. This process causes Mn to concentrate in austenite, and is the most important process for manufacturing a hot pressed member that has the appropriate amount of retained austenite to achieve a uniform elongation uEl of 6.0% or more and has a dislocation density of 1.0×1016/m2 or more to achieve ΔYS of 150 MPa or more.


Heating Temperature: Ac1 Point or More and Ac3 Point or Less


The hot rolled steel sheet is heated to a ferrite-austenite dual phase temperature range, to cause Mn to concentrate in austenite. In Mn-concentrated austenite, the martensite transformation end temperature is the room temperature or less, and the formation of retained austenite is facilitated. If the heating temperature is less than Ac1 point, austenite does not form, and Mn cannot be concentrated in austenite. If the heating temperature is more than Ac3 point, the temperature is in an austenite single phase temperature range, and Mn does not concentrate in austenite. In both of the case where the heating temperature is less than Ac1 point and the case where the heating temperature is more than Ac3 point, a hot pressed member having a dislocation density of 1.0×1016/m2 or more cannot be obtained. The heating temperature is therefore Ac1 point or more and Ac3 point or less. The heating temperature is preferably (Ac1 point+20° C.) or more. The heating temperature is preferably (Ac3 point−20° C.) or less.


Ac1 point (° C.) and Ac3 point (° C.) are calculated according to the following expressions:





Ac1 point (° C.)=751−16C+11Si−28Mn−5.5Cu−16Ni+13Cr+3.4Mo





Ac3 point (° C.)=910−203C1/2+44.7Si−4Mn+11Cr


where C, Si, Mn, Ni, Cu, Cr, and Mo are each the content (mass %) of the corresponding element. In the case where the element is not contained, the content of the element is assumed to be 0.


Heating Retention Time: 1 Hr or More and 48 Hr or Less


The concentration of Mn in austenite progresses with the passage of the heating retention time. If the heating retention time is less than 1 hr, the concentration of Mn in austenite is insufficient, and the desired uniform elongation cannot be obtained. Besides, if the heating retention time is less than 1 hr, the concentration of Mn is insufficient, and Ms point does not decrease in the hot press process, so that a hot pressed member having a dislocation density of 1.0×1016/m2 or more cannot be obtained. If the heating retention time is more than 48 hr, pearlite forms, making it impossible to achieve the desired uniform elongation. Moreover, a hot pressed member having a dislocation density of 1.0×1016/m2 or more cannot be obtained. The heating retention time is therefore 1 hr or more and 48 hr or less. The heating retention time is preferably 1.5 hr or more. The heating retention time is preferably 24 hr or less.


Ms point (° C.) is calculated according to the following expression:





Ms point (° C.)=539−423C−30.4Mn−17.7Ni−12.1Cr−7.5Mo


where C, Mn, Ni, Cr, and Mo are each the content (mass %) of the corresponding element. In the case where the element is not contained, the content of the element is assumed to be 0.


The cooling after the heating retention is not limited. It is preferable to appropriately perform the cooling by natural cooling (gradual cooling) or controlled cooling depending on the heating furnace used and the like.


The Mn concentration heat treatment is preferably performed in a batch annealing furnace or a continuous annealing furnace. The treatment conditions in the batch annealing furnace other than the above-mentioned conditions are not limited. For example, it is preferable to set the heating rate to 40° C./hr or more and the cooling rate after the heating retention to 40° C./hr or more, in terms of Mn concentration. The treatment conditions in the continuous annealing furnace other than the above-mentioned conditions are not limited. For example, it is preferable to, after performing the above-mentioned heating retention, cool the hot rolled steel sheet at an average cooling rate of 10° C./s or more to a cooling stop temperature in a temperature range of 350° C. to 600° C., cause the hot rolled steel sheet to stay in the temperature range for 10 sec to 300 sec, and then cool and coil the steel sheet, in terms of manufacturability.


The first blank steel sheet produced in this way can be used as a steel sheet for hot press. The microstructure of the first blank steel sheet has a feature that Mns/Mnα is 1.2 or more, where Mns is the Mn concentration in lath secondary phase and Mnα is the Mn concentration in lath ferrite. Here, “secondary phase” denotes the balance (austenite, martensite, pearlite, bainite) other than ferrite. If Mns/Mnα is less than 1.2, the concentration of Mn in austenite is insufficient, making it impossible to achieve sufficient uniform elongation and dislocation density after the hot press.


<Obtainment of Cold Rolled Steel Sheet>


After this, the first blank steel sheet may be cold rolled to obtain a cold rolled steel sheet, instead of performing the below-mentioned heating process and hot press forming process on the first blank steel sheet. To prevent abnormal grain growth in the subsequent annealing or the heating process immediately before the hot press, the reduction ratio in the cold rolling is preferably 30% or more, and more preferably 50% or more. To prevent an increase in rolling load and a decrease in productivity, the reduction ratio is preferably 85% or less.


<Annealing>


After this, the cold rolled steel sheet is subjected to annealing of heating the cold rolled steel sheet to Ac1 point or more and Ac3 point or less, retaining it at the temperature, and then cooling it, to obtain the second blank steel sheet. The annealing temperature is preferably a predetermined temperature that is Ac1 point or more and Ac3 point or less. With this annealing temperature, the concentration of Mn in austenite is further facilitated in the annealing. The retention time at the predetermined temperature is not limited, but is preferably 30 sec or more and 300 sec or less. If the retention time is 30 sec or more, the effect of the concentration of Mn is sufficient. If the retention time is 300 sec or less, productivity is maintained.


Pickling and/or temper rolling may be performed as appropriate between the processes.


The second blank steel sheet produced in this way can be used as a steel sheet for hot press. The microstructure of the second blank steel sheet has a feature that the mean grain size of ferrite is 10 μm or less, the mean grain size of secondary phase is 10 μm or less, and Mns/Mnα is 1.5 or more, where Mns is the Mn concentration in secondary phase and Mnα is the Mn concentration in ferrite. The mean grain size of ferrite and the mean grain size of secondary phase are determined by the following method. A microstructure observation test piece is collected from the second blank steel sheet so that the observation plane is parallel to the rolling direction and perpendicular to the rolling plane. The observation plane is polished, and etched with a 3 vol % nital solution to expose the microstructure. The microstructure at a position of ¼ of the sheet thickness is observed using a scanning electron microscope (at 1500 magnifications) and photographed. From the obtained micrograph, the microstructure is identified based on the above-mentioned criteria. The mean grain size of each of ferrite and secondary phase is calculated according to linear analysis described in JIS G 0551 (2005).


Mns/Mnα is determined by the following method. A microstructure observation test piece is collected. Its observation plane is then polished, and etched with a 3 vol % nital solution to expose the microstructure. The microstructure at a position of ¼ of the sheet thickness is observed using an electron probe microanalyzer (EPMA), and quantitative analysis of Mn is performed on 30 particles for each of ferrite and secondary phase. Regarding the Mn quantitative analysis results, the mean value of ferrite is set as Mnα, the mean value of secondary phase is set as Mns, and the value obtained by dividing the mean value Mns of secondary phase by the mean value Mnα of ferrite is set as Mns/Mnα.


<Coating>


In the case where no coated layer is formed on the surface of the first blank steel sheet or the second blank steel sheet, descaling treatment such as shot blasting needs to be performed on the hot pressed member after the hot press. In the case where a coated layer is formed on the surface of the first blank steel sheet or the second blank steel sheet, on the other hand, scaling is suppressed during heating in the hot press, so that descaling treatment after the hot press is unnecessary. This improves productivity.


The coating weight of the coated layer is preferably 10 g/m2to 90 g/m2 per side, and more preferably 30 g/m2 to 70 g/m2 per side. If the coating weight is 10 g/m2 or more, the effect of suppressing scaling during heating is sufficient. If the coating weight is 90 g/m2 or less, productivity is not hampered. The components of the coated layer are as described above.


<Heating Process>


Following this, a heating process of heating the first blank steel sheet or the second blank steel sheet to a second temperature that is Ac3 point or more and 1000° C. or less and retaining it at the second temperature for 900 sec or less is performed.


Heating Temperature: Ac3 Point or More and 1000° C. or Less


If the heating temperature is less than Ac3 point which is in an austenite single phase region, austenitization is insufficient. As a result, the desired amount of martensite in the hot pressed member cannot be ensured, and the desired tensile strength cannot be achieved. Besides, the hot pressed member cannot have a dislocation density of 1.0×1016/m2 or more, making it impossible to achieve ΔYS of 150 MPa or more. If the heating temperature is more than 1000° C., Mn concentrated in austenite is made uniform. Consequently, the desired amount of retained austenite cannot be ensured, and the desired uniform elongation cannot be achieved. Moreover, uniform Mn makes it impossible to decrease Ms point, so that the hot pressed member cannot have a dislocation density of 1.0×1016/m2 or more and ΔYS of 150 MPa or more cannot be achieved. The heating temperature is therefore Ac3 point or more and 1000° C. or less. The heating temperature is preferably (Ac3 point+30)° C. or more. The heating temperature is preferably 950° C. or less.


The heating rate to the heating temperature (second temperature) is not limited, but is preferably 1° C./s to 400° C./s, and more preferably 10° C./s to 150° C./s. If the heating rate is 1° C./s or more, productivity is not hampered. If the heating rate is 400° C./s or less, stable temperature control is ensured.


Retention Time: 900 Sec or Less (Including 0 Sec)


With the passage of the retention time at the heating temperature (second temperature), concentrated Mn diffuses around and is made uniform. Accordingly, if the retention time is more than 900 sec, the desired amount of retained austenite cannot be ensured, and the desired uniform elongation cannot be achieved. Besides, uniform Mn makes it impossible to decrease Ms point, so that the hot pressed member cannot have a dislocation density of 1.0×1016/m2 or more and ΔYS of 150 MPa or more cannot be achieved. The retention time is therefore 900 sec or less. The retention time may be 0 sec, that is, the heating may be stopped immediately after the second temperature is reached.


The heating method is not limited, and may be any typical heating method such as an electric furnace, a gas furnace, infrared heating, high frequency heating, or direct current heating. The atmosphere is not limited, and may be any of an air atmosphere and an inert gas atmosphere.


<Hot Press Forming Process>


In the hot press forming process, the first blank steel sheet or the second blank steel sheet which has undergone the heating process is simultaneously press formed and quenched using a press tool for forming, to obtain a hot pressed member of a predetermined shape. Hot press forming is a process of press forming a heated thin steel sheet using a press tool and simultaneously quenching it, and is also referred to as “hot forming”, “hot stamping”, “die quenching”, etc.


The forming start temperature in the press machine is not limited, but is preferably Ms point or more. If the forming start temperature is less than Ms point, the load of press forming increases, and the load on the press machine increases. The conveyance of the blank steel sheet before the forming start is typically performed with air cooling. Accordingly, the upper limit of the forming start temperature is the heating temperature in the immediately previous heating process in the manufacturing process. In the case where the blank steel sheet is conveyed in an environment where the cooling rate is accelerated by a refrigerant such as gas or liquid, the cooling rate is preferably decreased by a heat insulation jig such as a heat retention box.


The cooling rate in the press tool is not limited. In terms of productivity, the average cooling rate to 200° C. is preferably 20° C./s or more, and more preferably 40° C./s or more.


The removal time from the press tool and the cooling rate after the removal are not limited. As the cooling method, for example, a punch press tool is held at the bottom dead center for 1 sec to 60 sec, and the hot pressed member is cooled using a die press tool and the punch press tool. After this, the hot pressed member is removed from the press tool, and cooled. The cooling in the press tool and the cooling after the removal from the press tool may be performed in combination with a cooling method using a refrigerant such as gas or liquid. This improves productivity.


EXAMPLES

Molten steel having the chemical composition (the balance consisting of Fe and incidental impurities) listed in Tables 1 and 4 was obtained by steelmaking in a small vacuum melting furnace, to yield a slab. The slab was heated to 1250° C., and further subjected to hot rolling including rough rolling and finish rolling, to obtain a hot rolled steel sheet. The finisher entry temperature was 1100° C., and the finisher delivery temperature was 850° C. The cooling rate after the hot rolling end was 15° C./s on average from 800° C. to 600° C., and the coiling temperature was 650° C.


The obtained hot rolled steel sheet was heated to the heating temperature T1 (first temperature) listed in Tables 2 and 5, retained at the temperature for the time listed in Tables 2 and 5, and then cooled to obtain a first blank steel sheet. In some test examples, the first blank steel sheet was pickled, and cold rolled at a reduction ratio of 54%, to obtain a cold rolled steel sheet (sheet thickness: 1.6 mm). The cold rolled steel sheet was further heated to the heating temperature T2 listed in Tables 2 and 5, and retained for the time listed in Tables 2 and 5. The cold rolled steel sheet was then cooled at a cooling rate of 15° C./s. The cooling was stopped at 500° C., and the cold rolled steel sheet was retained at the temperature for 150 sec, to obtain a second blank steel sheet.


In the test examples not involving cold rolling, the first blank steel sheet was subjected to microstructure observation, and Mns/Mnα was calculated by the above-mentioned method. The results are listed in Tables 2 and 5. In the other test examples, the second blank steel sheet was subjected to microstructure observation, and the mean grain size of ferrite, the mean grain size of secondary phase, and Mns/Mnα were calculated by the above-mentioned methods. The results are listed in Tables 2 and 5.


As listed in Tables 2 and 5, in some test examples, the second blank steel sheet was subjected to coating treatment. In Tables 2 and 5, “GI” denotes a hot-dip galvanized layer, “GA” denotes a galvannealed layer, “Zn—Ni” denotes a Zn-12 mass % Ni coated layer, and “Al—Si” denotes a Al-10 mass % Si coated layer. The coating weight of each coated layer was 60 g/m2 per side.


The hot rolled steel sheet (first blank steel sheet) or the cold rolled steel sheet (second blank steel sheet) obtained in this way was subjected to a heating process under the conditions listed in Tables 3 and 6 and a hot press forming process, to obtain a hat-shaped hot pressed member. The hot press was performed using a punch press tool having a width of 70 mm and a shoulder radius R of 6 mm and a die press tool having a shoulder radius R of 7.6 mm, with a forming depth of 30 mm.


Regarding the heating process before the hot press forming process, in the case of performing the heating process using an electric heating furnace in the air atmosphere, the heating rate from the room temperature to 750° C. was 7.5° C./s on average. The heating rate from 750° C. to the heating temperature was 2.0° C./s on average. After reaching the heating temperature, the steel sheet was retained at the heating temperature in the case of keeping temperature. In the case of performing the heating process using a direct current heater in the air atmosphere, the heating rate from the room temperature to the heating temperature was 100° C./s on average. The hot press starts at 750° C. The steel sheet was cooled to 150° C. or less by a combination of: clamping the steel sheet using the die press tool and the punch press tool with the punch press tool being held at the bottom dead center for 15 sec; and air cooling on the die after release from the clamping. The average cooling rate from the hot pressing start temperature to 200° C. was 100° C./s.


The obtained hot pressed member was heat treated (low temperature heat treatment) at 170° C. for 20 min. This corresponds to the baking finish condition in a typical automotive member manufacturing process. Before and after the low temperature heat treatment, a JIS No. 5 tensile test piece (parallel portion width: 25 mm, parallel portion length: 60 mm, GL=50 mm) was collected from a hat top portion, and a tensile test was conducted according to JIS Z 2241 to determine the yield stress YS, the tensile strength TS, the total elongation tEl, and the uniform elongation uEl. The results are listed in Tables 3 and 6.


Moreover, the volume fraction of martensite phase, the volume fraction of retained austenite phase, the volume fraction of the balance, and the dislocation density in the obtained hot pressed member were measured by the above-mentioned methods. The results are listed in Tables 3 and 6.




















TABLE 1













Ac1
Ac3
Ms



Steel
C
Mn
Si
P
S
Al
N
point
point
point



No.
(mass %)
(mass %)
(mass %)
(mass %)
(mass %)
(mass %)
(mass %)
(° C.)
(° C.)
(° C.)
Category







A
0.210
 4.22
0.26
0.012
0.0015
0.031
0.0025
632
812
322
Conforming steel


B
0.160
 3.80
0.25
0.013
0.0014
0.030
0.0022
645
825
356
Conforming steel


C
0.220
 8.20
0.02
0.011
0.0150
0.035
0.0030
518
783
197
Conforming steel


D
0.220
10.40
0.03
0.022
0.0220
0.037
0.0040
457
775
130
Conforming steel


E
0.292
 4.50
0.03
0.015
0.0220
0.042
0.0041
621
784
279
Conforming steel


F

0.350

 4.15
0.25
0.015
0.0300
0.035
0.0023
632
784
265
Comparative steel


G

0.083

 4.20
0.25
0.010
0.0400
0.035
0.0025
634
831
356
Comparative steel


H
0.221

12.50

0.26
0.015
0.0350
0.030
0.0020
400
776
 66
Comparative steel


I
0.165
2.50
0.26
0.010
0.0350
0.031
0.0032
653
825
363
Comparative steel



























TABLE 2












Heat treatment























Heat treatment
Micro-
of cold rolled
Microstructure







of hot rolled
structure
steel sheet
after annealing






















steel sheet
after
(annealing)
Mean
Mean


Surface






















Heating

heat
Heating

grain
grain


treatment



Blank

temper-
Reten-
treat-
temper-
Reten-
size
size of


of



steel

ature
tion
ment
ature
tion
of
secondary

Type of
blank



sheet
Steel
T1
time
Mns/
T2
time
ferrite
phase
Mns/
blank steel
steel



No.
No.
(° C.)
(hr)
Mnα
(° C.)
(s)
(μm)
(μm)
Mnα
sheet
sheet
Category






















A1
A
675
 2.0

675
32
2.3
2.7
2.0
Cold rolled steel sheet
Zn—Ni
Example


A2
A
640
 2.0

675
30
2.5
2.8
1.9
Cold rolled steel sheet
Zn—Ni
Example


A3
A
715
 2.0

675
30
2.3
2.6
2.0
Cold rolled steel sheet
Zn—Ni
Example


A4
A
750
 2.0

675
31
2.6
2.8
1.8
Cold rolled steel sheet
Zn—Ni
Example


A5
A
675
 2.0
1.4





Hot rolled steel sheet
None
Example


A6
A

835

 2.0

675
30
2.5
8.9

0.8

Cold rolled steel sheet
None
Comparative Example


A7
A

600

 2.5

675
32
3.5
5.2

0.6

Cold rolled steel sheet
GA
Comparative Example


A8
A
670
0.2

672
30
2.4
5.4

0.9

Cold rolled steel sheet
GI
Comparative Example


A9
A
675

50.0


674
30
2.9
5.9

0.8

Cold rolled steel sheet
None
Comparative Example


B1
B
675
 2.5

680
35
3.2
3.6
1.6
Cold rolled steel sheet
None
Example


B2
B
675
 2.5
1.3





Hot rolled steel sheet
None
Example


C1
C
620
 5.5

625
100
3.5
3.9
2.5
Cold rolled steel sheet
None
Example


C2
C
620
 5.3

625
100
3.5
3.8
2.5
Cold rolled steel sheet
None
Comparative Example


C3
C
620
 5.5

624
100
3.4
3.9
2.5
Cold rolled steel sheet
None
Comparative Example


D1
D
600
10.5

615
105
3.2
3.6
2.4
Cold rolled steel sheet
None
Example


E1
E
650
10.5

665
102
4.5
5.0
2.3
Cold rolled steel sheet
Zn—Ni
Example


E2
E
650
10.5

665
102
4.5
5.0
2.3
Cold rolled steel sheet
Zn—Ni
Example


E3
E
650
10.5

665
102
4.5
5.0
2.3
Cold rolled steel sheet
Zn—Ni
Example


E4
E
650
10.5

665
102
4.5
5.0
2.3
Cold rolled steel sheet
Al—Si
Example


F1

F

673
 2.0

675
32
2.5
2.9
2.1
Cold rolled steel sheet
Zn—Ni
Comparative Example


G1

G

673
 2.0

675
30
2.2
2.6
2.2
Cold rolled steel sheet
Zn—Ni
Comparative Example


H1

H

602
10.5

620
105
3.1
3.5
2.5
Cold rolled steel sheet
None
Comparative Example


I1

I

675
 2.5

685
35
3.1
3.5
1.7
Cold rolled steel sheet
None
Comparative Example


A10
A
675
 2.0

675
32
2.3
2.7
2.0
Cold rolled steel sheet
Zn—Ni
Example


A11
A
675
 2.0

675
32
2.3
2.7
2.0
Cold rolled steel sheet
Zn—Ni
Example


A12
A
675
 2.0

675
32
2.3
2.7
2.0
Cold rolled steel sheet
Zn—Ni
Example


A13
A
675
 2.0

675
32
2.3
2.7
2.0
Cold rolled steel sheet
Zn—Ni
Comparative Example



















TABLE 3









Heating process
Microstructure















Hot
Blank

Heating
Reten-
Volume
Volume
Dis-
Volume


pressed
steel

temperature
tion
fraction of
fraction of
location
fraction of


member
sheet

T3
time
RA
M
density
balance


No.
No.
Heating method
(° C.)
(s)
(%)
(%)
(×1016/m2)
(%)





1
A1
Electric heating furnace
 852
 30
 8.1
91.9
2.2



2
A2
Electric heating furnace
 850
 30
 8.2
91.8
2.1



3
A3
Direct current heater
 855
  0
 8.3
91.7
2.2



4
A4
Direct current heater
 852
  0
 8.1
91.9
2.1



5
A5
Electric heating furnace
 852
 30
 7.6
92.4
1.8



6

A6

Electric heating furnace
 850
 30
2.3
97.7

0.8




7

A7

Electric heating furnace
 850
 30
1.5
98.5

0.7




8

A8

Electric heating furnace
 855
 30
2.3
97.7

0.9




9

A9

Electric heating furnace
 856
 30
2.4
97.6

0.8




10
B1
Electric heating furnace
 865
 60
 4.2
95.8
1.5



11
B2
Electric heating fumace
 865
 60
 3.5
96.5
1.2



12
C1
Electric heating fumace
 823
 60
11.1
88.9
2.2



13
C2
Electric heating furnace
750
 30
21.5

63.5


0.5

α: 15%


14
C3
Electric heating furnace

1150

 30
1.2
98.8

0.9




15
D1
Electric heating furnace
 815
  0
23.8
76.2
2.3



16
E1
Electric heating furnace
 824
 30
 8.0
92.0
1.9



17
E2
Electric heating furnace
 870
 30
 8.1
91.9
1.9



18
E3
Electric heating furnace
 910
 30
 8.0
92.0
1.8



19
E4
Electric heating furnace
 910
 30
 8.2
91.8
1.9



20

F1

Electric heating furnace
 824
 30
 8.2
91.8
2.3



21

G1

Electric heating furnace
 871
 30
 8.5
91.5
2.2



22

H1

Electric heating furnace
 816
 30
25.6
74.4
2.5



23

I1

Electric heating furnace
 865
 30
2.2
97.8

0.8




24
A10
Electric heating furnace
 850
300
 8.2
91.8
2.2



25
A11
Electric heating furnace
 852
600
 8.1
91.9
2.1



26
A12
Electric heating furnace
 825
900
 8.2
91.8
2.2



27
A13
Electric heating furnace
 825

960

1.5
98.5

0.7


















Mechanical property before
Mechanical property after





Hot
low temperature heat treatment
low temperature heat treatment





















pressed


Uniform
Total


Uniform
Total





member
YS
TS
elongation
elongation
YS
TS
elongation
elongation
ΔYS




No.
(MPa)
(MPa)
(%)
(%)
(MPa)
(MPa)
(%)
(%)
(MPa)
Scaling
Category





1
1025
1845
 7.5
10.5
1217
1882
 7.7
10.6
192
No scaling
Example


2
1021
1840
 7.6
11.5
1206
1877
 7.8
11.6
185
No scaling
Example


3
1029
1842
 7.3
10.8
1218
1879
 7.4
10.9
189
No scaling
Example


4
1028
1850
 7.5
11.2
1211
1887
 7.7
11.3
183
No scaling
Example


5
1018
1821
 7.2
 9.8
1203
1857
 7.3
 9.9
185
Scaling
Example


6
1230
1750
4.5
 7.2
1350
1785
 4.6
 7.3

120

Scaling
Comparative













Example


7
1221
1723
4.7
 7.5
1346
1757
 4.8
 7.6

125

No scaling
Comparative













Example


8
1240
1731
4.3
 7.8
1359
1766
 4.4
 7.9

119

No scaling
Comparative













Example


9
1236
1653
5.2
 7.9
1338
1686
 5.3
 8.0

102

Scaling
Comparative













Example


10
 985
1520
 6.5
 9.2
1150
1550
 6.6
 9.3
165
Scaling
Example


11
 982
1515
 6.2
 9.3
1134
1545
 6.3
 9.3
152
Scaling
Example


12
1026
2212
 9.8
11.3
1226
2256
 9.9
11.3
200
Scaling
Example


13
 856

1182

25.2
28.3
 938
1206
25.5
28.5
82
Scaling
Comparative













Example


14
1025
2010
4.8
 7.2
1126
2050
 4.5
 7.0

101

Scaling
Comparative













Example


15
1120
2200
11.2
13.7
1315
2244
11.3
14.0
195
Scaling
Example


16
1220
1920
 8.3
10.8
1409
1958
 8.4
11.1
189
No scaling
Example


17
1221
1910
 8.2
10.7
1406
1948
 8.3
11.0
185
No scaling
Example


18
1198
1913
 8.6
11.1
1381
1951
 8.7
11.4
183
No scaling
Example


19
1225
1915
 8.5
11.0
1414
1953
 8.6
11.3
189
No scaling
Example


20
1350
2554
 7.2
 8.9
1505
2605
 7.3
 8.5
155
No scaling
Comparative













Example


21
 932

1358

 9.8
11.5
1097
1385
 9.9
11.3
165
No scaling
Comparative













Example


22
 953
2652
12.3
13.5
1105
2705
12.4
14.1
152
Scaling
Comparative













Example


23
 953

1320

 8.5
10.2
1068
1346
 8.6
10.8

115

Scaling
Comparative













Example


24
1022
1842
 7.6
10.5
1222
1879
 7.8
10.6
200
No scaling
Example


25
1020
1843
 7.7
10.6
1215
1880
 7.9
10.7
195
No scaling
Example


26
1023
1845
 7.5
10.9
1233
1882
 7.6
11.2
210
No scaling
Example


27
1220
1700
4.5
 7.2
1342
1734
 4.5
 7.4

122

No scaling
Comparative













Example




























TABLE 4













Ac1
Ac3
Ms




Steel
C
Mn
Si
P
S
Al
N
point
point
point
Others



No.
(mass %)
(mass %)
(mass %)
(mass %)
(mass %)
(mass %)
(mass %)
(° C.)
(° C.)
(° C.)
(mass %)
Category







J
0.205
6.23
0.03
0.015
0.004
0.031
0.003
573
795
263
Ni: 0.02
Conforming steel


K
0.210
6.25
0.02
0.015
0.003
0.031
0.004
573
793
260
Cu: 0.02
Conforming steel


L
0.223
6.35
0.02
0.010
0.004
0.032
0.003
574
793
248
Cr: 0.30
Conforming steel


M
0.221
6.15
0.03
0.011
0.004
0.035
0.003
576
791
257
Mo: 0.25
Conforming steel


N
0.225
4.20
0.02
0.032
0.004
0.035
0.005
630
798
316
Ti: 0.03
Conforming steel


O
0.215
4.31
0.03
0.034
0.003
0.035
0.004
627
800
317
Nb: 0.03
Conforming steel


P
0.205
4.15
0.04
0.035
0.005
0.035
0.003
632
803
326
V: 0.03
Conforming steel


Q
0.217
4.36
0.06
0.035
0.002
0.034
0.005
626
801
315
W: 0.03
Conforming steel


R
0.218
4.25
0.22
0.015
0.004
0.036
0.005
631
808
318
Ti: 0.02, B: 0.002
Conforming steel


S
0.213
6.25
0.27
0.016
0.003
0.036
0.005
576
803
259
Ti: 0.02, B: 0.002
Conforming steel


T
0.156
6.23
0.15
0.016
0.002
0.038
0.004
576
812
284
REM: 0.001
Conforming steel


U
0.224
6.20
0.16
0.025
0.002
0.050
0.003
576
796
256
B: 0.003
Conforming steel


V
0.152
6.22
0.22
0.025
0.005
0.065
0.004
577
816
286
Ca: 0.003
Conforming steel


W
0.148
6.22
0.16
0.035
0.004
0.058
0.003
576
814
287
Mg: 0.003
Conforming steel


X
0.203
4.31
0.13
0.035
0.003
0.065
0.006
629
807
322
Sb: 0.008
Conforming steel



























TABLE 5












Heat treatment

























Heat treatment
Micro-
of cold rolled























of hot rolled
structure
steel sheet
Microstructure after annealing






















steel sheet
after
(annealing)
Mean
Mean


Surface






















Heating

heat
Heating

grain
grain


treatment



Blank

temper-
Reten-
treat-
temper-
Reten-
size
size of


of



steel

ature
tion
ment
ature
tion
of
secondary

Type of
blank



sheet
Steel
T1
time
Mns/
T2
time
ferrite
phase
Mns/
blank steel
steel



No.
No.
(° C.)
(hr)
Mnα
(° C.)
(s)
(μm)
(μm)
Mnα
sheet
sheet
Category






















J1
J
625
2.0
1.4





Hot rolled steel sheet
None
Example


K1
K
630
2.0

680
45
3.5
5.6
2.3
Cold rolled steel sheet
Zn—Ni
Example


L1
L
631
2.1

685
48
2.5
7.8
2.5
Cold rolled steel sheet
Zn—Ni
Example


M1
M
635
2.5

675
45
2.4
8.5
2.2
Cold rolled steel sheet
None
Example


N1
N
675
2.5
1.4





Hot rolled steel sheet
None
Example


O1
O
675
3.0

675
40
3.2
6.2
2.4
Cold rolled steel sheet
Zn—Ni
Example


P1
P
670
3.5

672
150
4.5
7.5
2.5
Cold rolled steel sheet
Zn—Ni
Example


Q1
Q
675
3.5

680
44
5.2
8.0
3.2
Cold rolled steel sheet
Zn—Ni
Example


R1
R
675
40.0

680
46
3.5
5.9
3.5
Cold rolled steel sheet
Zn—Ni
Example


S1
S
630
35.0

645
52
2.6
8.2
3.4
Cold rolled steel sheet
Zn—Ni
Example


T1
T
625
2.5

630
55
4.2
6.5
3.0
Cold rolled steel sheet
Zn—Ni
Example


U1
U
630
1.7

645
56
5.0
6.3
2.5
Cold rolled steel sheet
Zn—Ni
Example


V1
V
615
1.7

630
52
5.2
7.2
2.2
Cold rolled steel sheet
Zn—Ni
Example


W1
W
620
3.0

635
105
5.1
6.4
2.6
Cold rolled steel sheet
None
Example


X1
X
680
35.0

690
115
5.0
4.3
2.2
Cold rolled steel sheet
None
Example



















TABLE 6









Heating process
Microstructure















Hot
Blank

Heating
Reten-
Volume
Volume
Dis-
Volume


pressed
steel

temperature
tion
fraction of
fraction of
location
fraction of


member
sheet

T3
time
RA
M
density
balance


No.
No.
Heating method
(° C.)
(s)
(%)
(%)
(×1016/m2)
(%)





28
J1
Electric heating furnace
830
30
10.1
89.9
2.3



29
K1
Electric heating furnace
850
30
11.2
88.8
2.4



30
L1
Electric heating furnace
855
30
12.5
87.5
2.2



31
M1
Direct current heater
845
30
11.5
88.5
2.0



32
N1
Direct current heater
850
30
9.5
90.5
1.8



33
O1
Electric heating furnace
855
30
9.4
90.6
1.9



34
P1
Direct current heater
855
30
9.6
90.4
1.9



35
Q1
Electric heating furnace
864
30
9.8
90.2
2.0



36
R1
Electric heating furnace
835
30
9.8
90.2
2.2



37
S1
Electric heating furnace
825
30
12.1
87.9
2.1



38
T1
Electric heating furnace
820
30
12.3
87.7
1.5



39
U1
Electric heating furnace
825
30
11.4
88.6
2.1



40
V1
Electric heating furnace
830
30
4.5
95.5
1.6



41
W1
Direct current heater
835
30
4.6
95.4
1.7



42
X1
Electric heating furnace
834
30
11.0
89.0
1.9

















Mechanical property before
Mechanical property after





Hot
low temperature heat treatment
low temperature heat treatment





















pressed


Uniform
Total


Uniform
Total





member
YS
TS
elongation
elongation
YS
TS
elongation
elongation
ΔYS




No.
(MPa)
(MPa)
(%)
(%)
(MPa)
(MPa)
(%)
(%)
(MPa)
Scaling
Category





28
1211
2115
9.2
12.5
1416
2157
9.4
12.6
205
Scaling
Example


29
1230
2121
10.1
13.4
1426
2163
10.3
13.5
196
No scaling
Example


30
1213
2123
11.1
13.5
1402
2165
11.3
13.6
189
No scaling
Example


31
1215
2095
11.2
14.0
1418
2137
11.4
14.1
203
Scaling
Example


32
1125
1923
7.8
12.0
1318
1961
8.0
12.1
193
Scaling
Example


33
1100
1890
8.2
11.1
1283
1928
8.4
11.2
183
No scaling
Example


34
1113
1860
8.1
11.5
1302
1897
8.3
11.6
189
No scaling
Example


35
1145
1896
9.5
11.3
1337
1934
9.7
11.4
192
No scaling
Example


36
1052
1860
9.2
10.9
1245
1897
9.4
11.0
193
No scaling
Example


37
1045
2120
10.2
12.3
1258
2162
10.4
12.4
213
No scaling
Example


38
1023
2125
7.2
12.4
1199
2168
7.3
12.5
176
No scaling
Example


39
1040
2124
9.8
11.5
1255
2166
10.0
11.6
215
No scaling
Example


40
1020
1652
7.8
11.2
1195
1685
8.0
11.3
175
No scaling
Example


41
1025
1650
7.5
11.5
1203
1683
7.7
11.6
178
Scaling
Example


42
1115
1920
8.7
11.8
1310
1958
8.9
11.9
195
Scaling
Example





In the table, RA denotes retained austenite, M denotes martensite, and α denotes ferrite.






All Examples achieved a tensile strength TS of 1500 MPa or more, a uniform elongation uEl of 6.0% or more, and ΔYS of 150 MPa or more. Comparative Examples, on the other hand, failed to satisfy at least one of the properties.


INDUSTRIAL APPLICABILITY

The hot pressed member according to the present disclosure is suitable as a structural member required to have high collision energy absorbing performance, such as an impact beam, a center pillar, or a bumper of a vehicle.

Claims
  • 1. A hot pressed member comprising: a chemical composition containing, in mass %,C: 0.090% or more and less than 0.30%,Mn: 3.5% or more and less than 11.0%,Si: 0.01% to 2.5%,P: 0.05% or less,S: 0.05% or less,Al: 0.005% to 0.1%, andN: 0.01% or less,with a balance consisting of Fe and incidental impurities;a microstructure including a martensite phase of 70.0% or more in volume fraction and a retained austenite phase of 3.0% or more and 30.0% or less in volume fraction;a tensile property of 1500 MPa or more in tensile strength TS and 6.0% or more in uniform elongation uEl; anda dislocation density of 1.0×1016/m2 or more.
  • 2. The hot pressed member according to claim 1, wherein the chemical composition further contains, in mass %, one or more groups selected fromA group: one or more selected from Ni: 0.01% to 5.0%, Cu: 0.01% to 5.0%, Cr: 0.01% to 5.0%, and Mo: 0.01% to 3.0%,B group: one or more selected from Ti: 0.005% to 3.0%, Nb: 0.005% to 3.0%, V: 0.005% to 3.0%, and W: 0.005% to 3.0%,C group: one or more selected from REM: 0.0005% to 0.01%, Ca: 0.0005% to 0.01%, and Mg: 0.0005% to 0.01%,D group: Sb: 0.002% to 0.03%, andE group: B: 0.0005% to 0.05%.
  • 3. The hot pressed member according to claim 1, comprising a coated layer on a surface thereof.
  • 4. The hot pressed member according to claim 3, wherein the coated layer is any of a zinc or zinc alloy coated layer and an aluminum or aluminum alloy coated layer.
  • 5. The hot pressed member according to claim 4, wherein the zinc or zinc alloy coated layer contains Ni: 10 mass % to 25 mass %.
  • 6. A method of manufacturing a hot pressed member, the method comprising: heating a slab and hot rolling the slab to obtain a hot rolled steel sheet, the slab having a chemical composition containing, in mass %,C: 0.090% or more and less than 0.30%,Mn: 3.5% or more and less than 11.0%,Si: 0.01% to 2.5%,P: 0.05% or less,S: 0.05% or less,Al: 0.005% to 0.1%, andN: 0.01% or less,with a balance consisting of Fe and incidental impurities;heating the hot rolled steel sheet to a first temperature that is an Ac1 point or more and an Ac3 point or less, retaining the hot rolled steel sheet at the first temperature for 1 hr or more and 48 hr or less, and then cooling the hot rolled steel sheet to obtain a first blank steel sheet;performing a heating process of heating the first blank steel sheet to a second temperature that is the Ac3 point or more and 1000° C. or less and retaining the first blank steel sheet at the second temperature for 900 sec or less; andthereafter performing a hot press forming process of simultaneously press forming and quenching the first blank steel sheet using a press tool for forming, to obtain a hot pressed member.
  • 7. The method of manufacturing a hot pressed member according to claim 6, further comprising: cold rolling the first blank steel sheet to obtain a cold rolled steel sheet, before the heating process; andannealing the cold rolled steel sheet to obtain a second blank steel sheet, the annealing including heating the cold rolled steel sheet to a temperature that is the Ac1 point or more and the Ac3 point or less, retaining the cold rolled steel sheet at the temperature, and then cooling the cold rolled steel sheet,wherein the heating process and the hot press forming process are performed on the second blank steel sheet instead of the first blank steel sheet.
  • 8. The method of manufacturing a hot pressed member according to claim 6, wherein the chemical composition further contains, in mass %, one or more groups selected fromA group: one or more selected from Ni: 0.01% to 5.0%, Cu: 0.01% to 5.0%, Cr: 0.01% to 5.0%, and Mo: 0.01% to 3.0%,B group: one or more selected from Ti: 0.005% to 3.0%, Nb: 0.005% to 3.0%, V: 0.005% to 3.0%, and W: 0.005% to 3.0%,C group: one or more selected from REM: 0.0005% to 0.01%, Ca: 0.0005% to 0.01%, and Mg: 0.0005% to 0.01%,D group: Sb: 0.002% to 0.03%, andE group: B: 0.0005% to 0.05%.
  • 9. The method of manufacturing a hot pressed member according to claim 6, further comprising forming a coated layer on a surface of the first blank steel sheet before the heating process.
  • 10. The method of manufacturing a hot pressed member according to claim 9, wherein the coated layer is any of a zinc or zinc alloy coated layer and an aluminum or aluminum alloy coated layer.
  • 11. The method of manufacturing a hot pressed member according to claim 10, wherein the zinc or zinc alloy coated layer contains Ni: 10 mass % to 25 mass %.
  • 12. The method of manufacturing a hot pressed member according to claim 9, wherein a coating weight of the coated layer is 10 g/m2 to 90 g/m2 per side.
  • 13. The method of manufacturing a hot pressed member according to claim 7, wherein the chemical composition further contains, in mass %, one or more groups selected fromA group: one or more selected from Ni: 0.01% to 5.0%, Cu: 0.01% to 5.0%, Cr: 0.01% to 5.0%, and Mo: 0.01% to 3.0%,B group: one or more selected from Ti: 0.005% to 3.0%, Nb: 0.005% to 3.0%, V: 0.005% to 3.0%, and W: 0.005% to 3.0%,C group: one or more selected from REM: 0.0005% to 0.01%, Ca: 0.0005% to 0.01%, and Mg: 0.0005% to 0.01%,D group: Sb: 0.002% to 0.03%, andE group: B: 0.0005% to 0.05%.
  • 14. The method of manufacturing a hot pressed member according to claim 7, further comprising forming a coated layer on a surface of the second blank steel sheet before the heating process.
  • 15. The method of manufacturing a hot pressed member according to claim 14, wherein the coated layer is any of a zinc or zinc alloy coated layer and an aluminum or aluminum alloy coated layer.
  • 16. The method of manufacturing a hot pressed member according to claim 15, wherein the zinc or zinc alloy coated layer contains Ni: 10 mass % to 25 mass %.
  • 17. The method of manufacturing a hot pressed member according to claim 14, wherein a coating weight of the coated layer is 10 g/m2 to 90 g/m2 per side.
Priority Claims (1)
Number Date Country Kind
2015-205751 Oct 2015 JP national
PCT Information
Filing Document Filing Date Country Kind
PCT/JP2016/004458 10/3/2016 WO 00