EP3594376B1 - Austenitic steel alloy for hot forming - Google Patents
Austenitic steel alloy for hot forming Download PDFInfo
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- EP3594376B1 EP3594376B1 EP18190883.1A EP18190883A EP3594376B1 EP 3594376 B1 EP3594376 B1 EP 3594376B1 EP 18190883 A EP18190883 A EP 18190883A EP 3594376 B1 EP3594376 B1 EP 3594376B1
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- 229910000851 Alloy steel Inorganic materials 0.000 title claims description 56
- 229910000831 Steel Inorganic materials 0.000 claims description 80
- 239000010959 steel Substances 0.000 claims description 80
- 238000000034 method Methods 0.000 claims description 30
- 230000032683 aging Effects 0.000 claims description 19
- 239000011572 manganese Substances 0.000 claims description 19
- 229910052799 carbon Inorganic materials 0.000 claims description 17
- 229910052750 molybdenum Inorganic materials 0.000 claims description 17
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 16
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 15
- 239000011651 chromium Substances 0.000 claims description 15
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 14
- 239000011733 molybdenum Substances 0.000 claims description 14
- 229910052748 manganese Inorganic materials 0.000 claims description 12
- 229910052804 chromium Inorganic materials 0.000 claims description 11
- 229910052782 aluminium Inorganic materials 0.000 claims description 10
- 238000010791 quenching Methods 0.000 claims description 9
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 8
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 7
- 229910052742 iron Inorganic materials 0.000 claims description 6
- 238000003723 Smelting Methods 0.000 claims description 5
- 239000010941 cobalt Substances 0.000 claims description 5
- 229910017052 cobalt Inorganic materials 0.000 claims description 5
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 5
- 238000005266 casting Methods 0.000 claims description 3
- 150000001247 metal acetylides Chemical class 0.000 description 16
- 229910045601 alloy Inorganic materials 0.000 description 10
- 239000000956 alloy Substances 0.000 description 10
- 230000000052 comparative effect Effects 0.000 description 10
- 238000001556 precipitation Methods 0.000 description 9
- 230000003287 optical effect Effects 0.000 description 8
- 229910001566 austenite Inorganic materials 0.000 description 6
- 238000010438 heat treatment Methods 0.000 description 6
- 239000011159 matrix material Substances 0.000 description 5
- 238000001816 cooling Methods 0.000 description 4
- 238000005336 cracking Methods 0.000 description 4
- 229910000734 martensite Inorganic materials 0.000 description 4
- 238000005259 measurement Methods 0.000 description 4
- 239000010955 niobium Substances 0.000 description 4
- 229910001339 C alloy Inorganic materials 0.000 description 3
- 238000002844 melting Methods 0.000 description 3
- 230000035882 stress Effects 0.000 description 3
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 3
- 229910052721 tungsten Inorganic materials 0.000 description 3
- 239000010937 tungsten Substances 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000005098 hot rolling Methods 0.000 description 2
- 229910052758 niobium Inorganic materials 0.000 description 2
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- 229910052720 vanadium Inorganic materials 0.000 description 2
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 2
- FGUUSXIOTUKUDN-IBGZPJMESA-N C1(=CC=CC=C1)N1C2=C(NC([C@H](C1)NC=1OC(=NN=1)C1=CC=CC=C1)=O)C=CC=C2 Chemical compound C1(=CC=CC=C1)N1C2=C(NC([C@H](C1)NC=1OC(=NN=1)C1=CC=CC=C1)=O)C=CC=C2 FGUUSXIOTUKUDN-IBGZPJMESA-N 0.000 description 1
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 229910003460 diamond Inorganic materials 0.000 description 1
- 239000010432 diamond Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000001330 spinodal decomposition reaction Methods 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 239000011593 sulfur Substances 0.000 description 1
- 238000009864 tensile test Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/18—Hardening; Quenching with or without subsequent tempering
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/18—Hardening; Quenching with or without subsequent tempering
- C21D1/25—Hardening, combined with annealing between 300 degrees Celsius and 600 degrees Celsius, i.e. heat refining ("Vergüten")
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/34—Methods of heating
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/56—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering characterised by the quenching agents
- C21D1/60—Aqueous agents
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/62—Quenching devices
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/78—Combined heat-treatments not provided for above
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/002—Heat treatment of ferrous alloys containing Cr
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/005—Heat treatment of ferrous alloys containing Mn
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/007—Heat treatment of ferrous alloys containing Co
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/10—Ferrous alloys, e.g. steel alloys containing cobalt
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/12—Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/22—Ferrous alloys, e.g. steel alloys containing chromium with molybdenum or tungsten
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/30—Ferrous alloys, e.g. steel alloys containing chromium with cobalt
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- C—CHEMISTRY; METALLURGY
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- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/38—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of manganese
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/001—Austenite
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D7/00—Modifying the physical properties of iron or steel by deformation
- C21D7/13—Modifying the physical properties of iron or steel by deformation by hot working
Definitions
- the disclosure relates to an austenitic steel alloy, and more particularly to an austenitic steel alloy for hot work tools.
- the disclosure also relates to a method for making an austenitic steel using the alloy, and an austenitic steel made by the method.
- Martensitic steel is a steel material commonly used for making hot work tools due to its superior mechanical properties such as hardness and toughness. However, since the martensitic steel has a relatively low ductility, the hot work tools made therefrom are liable to cracking.
- AISI H13 steel is an example of the martensitic steel commonly used for making the hot work tools, and includes carbon in an amount of from 0.32 wt% to 0.45 wt%, silicon in an amount of from 0.80 wt% to 1.20 wt%, manganese in an amount of from 0.20 wt% to 0.50 wt%, chromium in an amount of from 4.75 wt% to 5.50 wt%, molybdenum in an amount of from 1.10 wt% to 1.75 wt%, vanadium in an amount of from 0.80 wt% to 1.20 wt%, phosphorus in an amount of not more than 0.03 wt%, sulfur in an amount of not more than 0.03 wt%, and a balance of iron.
- the AISI H13 steel has a room temperature hardness of from 55 to 58, an elongation at room temperature of from 3% to 5%, an impact toughness of from 5 Joules (J) to 10 J, and a high temperature Rockwell C hardness (HRc) of from 33 to 41. Since the AISI H13 steel having a relatively low elongation is liable to cracking during usage, the room temperature hardness thereof is usually reduced to a range of from 42 to 50 so as to increase the elongation to a range of from 5% to 8%.
- QRO 90 steel is another example of the martensitic steel commonly used for making the hot work tools, and includes carbon in an amount of 0.38 wt%, silicon in an amount of 0.30 wt%, manganese in an amount of 0.75 wt%, chromium in an amount of 2.60 wt%, molybdenum in an amount of 2.25 wt%, vanadium in an amount of 0.9 wt%, and a balance of iron.
- the QRO 90 steel has a room temperature hardness of 45, an elongation of about 11 %, an impact toughness of 10 J, and a high temperature Rockwell C hardness (HRc) of from 26 to 41.
- austenitic Fe-Mn-Al-C steel has been subjected to extensive researches over the last several decades because of its promising application that is potential associated with high mechanical strength and high ductility.
- Conventional austenitic Fe-Mn-Al-C steel containing carbon in an amount of greater than about 1.2 wt% may be deteriorated in terms of ductility and may be even cracked. Therefore, the amount of carbon in the conventional austenitic Fe-Mn-Al-C steel is usually controlled within a range of from 0.54 wt% to 1.3 wt% and is added with molybdenum (Mo), niobium (Nb), and/or tungsten (W) to enhance the mechanical strength thereof.
- Mo molybdenum
- Nb niobium
- W tungsten
- ductility (i.e., elongation) of the conventional austenitic Fe-Mn-Al-C steel may be undesirably reduced due to precipitation of coarse carbides on the grain boundaries of the austenitic Fe-Mn-Al-C steel during an aging treatment. Accordingly, the hot work tools made therefrom are liable to cracking.
- Applicant's U.S. Patent No. 9,528,177 discloses a Fe-Mn-Al-C quarternary alloy which is essentially consisting of Fe, Mn, Al, and C in specific amounts. Specifically, the amount of carbon in the Fe-Mn-Al-C quarternary alloy is controlled within a range of from 1.4 wt% to 2.2 wt%.
- the Fe-Mn-Al-C quarternary alloy possesses superior ductility and high mechanical strength due to formation of a high density of fine K' carbides within an austenite matrix by a spinodal decomposition phase transition mechanism during quenching from a solution heat treatment temperature.
- US2013081740 is directed to Fe-Mn-Al-C alloys.
- Fe-Mn-Al-C alloys additionally comprising Mo, Cr, Co, and/or other elements, are disclosed.
- the disclosed alloys do not exhibit the desired level of high mechanical strength and high ductility.
- a first object of the disclosure is to provide an austenitic steel alloy which possesses superior mechanical properties without compromising ductility at room temperature, and which also possesses superior mechanical properties at high temperature.
- a second object of the disclosure is to provide a method for making an austenitic steel using the austenitic steel alloy.
- a third object of the disclosure is to provide an austenitic steel made by the method.
- an austenitic steel alloy which comprises manganese in an amount of from 25 wt% to 31 wt%, aluminum in an amount of from 7 wt% to 10 wt%, carbon in an amount of from 1.4 wt% to 1.6 wt%, molybdenum in an amount of from 2 wt% to 6 wt%, optionally chromium in an amount of less than 6 wt%, optionally cobalt in an amount of less than 5 wt%, and a balance of iron.
- an austenitic steel made by the method of the second aspect of the disclosure.
- the austenitic steel alloy according to the disclosure possesses superior mechanical properties both at room temperature and at high temperature (e.g., at about 500°C) which are achieved by adding molybdenum in an amount of less than 6 wt% into the austenitic steel alloy including manganese, aluminum, carbon, and iron in specific amounts.
- An austenitic steel alloy according to the disclosure comprises manganese (Mn) in an amount of from 25 wt% to 31 wt%, aluminum (Al) in an amount of from 7 wt% to 10 wt%, carbon (C) in an amount of from 1.4 wt% to 1.6 wt%, molybdenum (Mo) in an amount of from 2 wt% to 6 wt%, optionally chromium in an amount of less than 6 wt%, optionally cobalt in an amount of less than 5 wt%, and a balance of iron (Fe).
- the austenitic steel alloy according to the disclosure possesses superior mechanical properties and high ductility, and can be used for making general steel plates such as automobile steel plates, mechanical parts such as gears, hard work tools, and the like.
- Mn is a strong austenite-stabilizing element.
- An austenite phase is of face-center-cubic (FCC) structure with more dislocation slip systems, and thus possesses better ductility than other crystal structures, such as body-center-cubic (BCC) and hexagonal close packed (HCP) structures. Therefore, in order to obtain a fully austenite structure at room temperature, Mn is in an amount of from 25 wt% to 31 wt% in the austenitic steel alloy according to the disclosure. In certain embodiments, Mn is in an amount of from 26 wt% to 30 wt% . In certain embodiments, Mn is in an amount of from 27 wt% to 29 wt%.
- Al not only is a strong ferrite-stabilizing element, but also is one of the primary elements for forming (Fe,Mn) 3 AlC x carbides (i.e., ⁇ ' carbides).
- Al is in an amount of from 7 wt% to 10 wt% in the austenitic steel alloy according to the disclosure. In certain embodiments, Al is in an amount of from 8 wt% to 10 wt%. In certain embodiments, Al is in an amount of from 8 wt% to 9 wt%.
- C is in an amount of from 1.2 wt% to 1.6 wt% in the austenitic steel alloy according to the disclosure, which is relatively high as compared to the amount (i.e., up to 1.0 wt%) of C in the conventional austenitic Fe-Mn-Al-C steel, in which molybdenum (Mo), niobium (Nb), and/or tungsten (W) is added.
- Mo molybdenum
- Nb niobium
- W tungsten
- C is in an amount of from 1.4 wt% to 1.6 wt%.
- Mo is a very strong carbide-forming element. Mo is in an amount of more than 0 wt% and less than 6 wt% in the austenitic steel alloy according to the disclosure. In certain embodiments, Mo is in an amount of from 2 wt% to 6 wt%.
- the austenitic steel alloy according to the disclosure further comprises chromium (Cr).
- Cr is also a very strong carbide-forming element. Cr is in an amount of less than 6 wt% in the austenitic steel alloy according to the disclosure.
- the austenitic steel alloy according to the disclosure further comprises cobalt (Co).
- Co is also a very strong carbide-forming element. Co is in an amount of less than 5 wt% in the austenitic steel alloy according to the disclosure.
- the amounts of low-melting elements (e.g., Mn and Al) in the austenitic steel alloy according to the disclosure may be slightly different from those of the low-melting elements in the austenitic steel made from the alloy due to the smelting that causes evaporation effect of the low-melting elements. However, the difference is within an acceptable tolerance. Therefore, the properties of the austenitic steel made from the alloy will not be affected.
- an embodiment of a method for making an austenitic steel according to the disclosure comprises steps of:
- the hot-worked body has a thickness of less than 25% of that of the cast piece.
- the temperature for the aging treatment in step e) is from 480°C to 500°C, and the aging treatment is implemented for a period of from 5 hours to 12 hours.
- the temperature for the aging treatment in step e) is larger than 500°C and up to 600°C, and the aging treatment is implemented for a period of from 1 hour to 4 hours.
- the method for making the austenitic steel according to the disclosure is different from the method for making the conventional austenitic Fe-Mn-Al-C steel having a relatively low carbon amount and containing strong carbide-forming elements. Specifically, in the method for making the conventional austenitic Fe-Mn-Al-C steel, a solution heat treatment is required after the hot-working treatment to dissolve the coarse carbides precipitated on the grain boundaries into a matrix phase so as to enhance the ductility of the conventional austenitic Fe-Mn-Al-C steel.
- the temperature for implementing the hot-working treatment is controlled within a range of from 1100°C to 950°C such that the precipitation of the coarse carbides on the grain boundaries during the hot-working treatment can be avoided. Therefore, an austenitic steel having superior mechanical properties and high ductility can be made without the solution heat treatment, which is required in the method for making the conventional austenitic Fe-Mn-Al-C steel.
- the aged body can be cooled down naturally to room temperature.
- the solution heat treatment is not a requisite in the method for making the austenitic steel according to the disclosure, it may be optionally implemented, if desired.
- the austenitic steel made by the method according to the disclosure has a fully austenitic phase, a yield strength at 25°C of from 1200 MPa to 1400 MPa, a Rockwell C hardness (HRc) at 25°C of from 45 to 55, an ultimate tensile strength at 25°C of from 1200 MPa to 1500 MPa, and an elongation at 25°C of from 20% to 40%.
- the austenitic steel made by the method according to the disclosure has superior yield strength and ultimate tensile strength at high temperature up to 700°C. Therefore, the austenitic steel made by the method according to the disclosure can be used for making general steel plates such as automobile steel plates, mechanical parts such as gears, hard work tools, and the like.
- the austenitic steel alloy according to the disclosure comprises carbon in an amount of from 1.42 wt% to 1.5 wt% and molybdenum in an amount of from 3.5 wt% to 5 wt%.
- the austenitic steel made by the austenitic steel alloy according to the disclosure has an ultimate tensile strength at 25°C of from 1353 MPa to 1386 MPa, a yield strength at 25°C of from 1310 MPa and 1340 MPa, and a HRc at 25°C of from 47 to 47.7.
- the austenitic steel alloy according to the disclosure comprises carbon in an amount of from 1.42 wt% to 1.45 wt% and molybdenum in an amount of from 3.5 wt% to 4 wt%.
- the austenitic steel made by the austenitic steel alloy according to the disclosure has an elongation at 25°C of 25%.
- the austenitic steel alloy according to the disclosure comprises manganese in an amount of from 27.7 wt% to 30 wt% and aluminum in an amount of from 8.2 wt% to 8.5 wt% .
- the austenitic steel made by the austenitic steel alloy according to the disclosure has an ultimate tensile strength at 25°C of from 1280 MPa to 1386 MPa, a yield strength at 25°C of from 1250 MPa and 1350 MPa, a hardness (HRc) at 25°C of from 46.7 to 47.7, and an elongation at 25°C of from 20% to 32%.
- the austenitic steel alloy according to the disclosure comprises manganese in an amount of from 27 wt% to 29 wt%, aluminum in an amount of from 8.0 wt% to 8.5 wt%, and molybdenum in an amount of from 3.0 wt% to 6 wt%.
- the austenitic steel made by the austenitic steel alloy according to the disclosure has an elongation at 25°C of more than 20%, an ultimate tensile strength at 25°C of more than 1280 MPa, a yield strength at 25°C of more than 1230 MPa, an ultimate tensile strength at 300 °C of more than 1000 MPa, and a yield strength at 300 °C of more than 1000 MPa.
- the austenitic steel alloy according to the disclosure comprises molybdenum in an amount of 3.0 wt%, and further comprises chromium in an amount of 3 wt% or cobalt in an amount of 2 wt%.
- the austenitic steel made by the austenitic steel alloy according to the disclosure has an ultimate tensile strength at 25°C of from 1280 MPa to 1344 MPa, a yield strength at 25°C of from 1230 MPa and 1300 MPa, a hardness (HRc) at 25°C of from 45 to 46.8, and an elongation at 25°C of from 24% to 37%.
- the presently available steel for the hot work tools has a density of from 7.8 g/cm 3 to 7.9 g/cm 3 .
- the austenitic steel made by the method according to the disclosure has a density of from 6.6 g/cm 3 to 6.8 g/cm 3 , which is 14% less than the density of the presently available steel. Therefore, in addition to superior mechanical properties and high ductility, the austenitic steel made by the method according to the disclosure has a lightweight advantage.
- the conventional Fe-Mn-Al-C alloy having a relatively high amount of carbon of from 1.4 wt% to 2.2 wt% can possess a fully austenitic phase, form a high density of fine ⁇ ' carbides (i.e., (Fe,Mn) 3 AlC x carbides) within an austenite matrix, and avoid the precipitation of coarse carbides on the grain boundaries so as to possess superior mechanical strength and high ductility by controlling the hot-working treatment, the solution heat treatment, and the water-quenching treatment.
- fine ⁇ ' carbides i.e., (Fe,Mn) 3 AlC x carbides
- an austenitic steel according to the disclosure by adding specific amounts of the strong carbide-forming elements (i.e., Mo and optionally Cr and Co) in the austenitic steel alloy and by controlling the temperature for implementing the hot-working treatment within a specific range (i.e., from 1100°C to 950°C), the precipitation of coarse carbides on the grain boundaries during the hot-working treatment can be avoided. Therefore, an austenitic steel having superior mechanical properties and high ductility can be made without the solution heat treatment which is required in the method for making the conventional austenitic Fe-Mn-Al-C steel.
- the strong carbide-forming elements i.e., Mo and optionally Cr and Co
- a steel alloy containing 30 wt% of Mn, 8.5 wt% of Al, 1.45 wt% of C, 6 wt% of Mo, and a balance of Fe was smelted in a high-frequency smelting furnace under an atmosphere to obtain a molten steel alloy, followed by casting the molten steel alloy to obtain a cast piece having a thickness of 2 cm.
- the cast piece was heated in a furnace at 1100°C, followed by hot-rolling at a temperature of from 1100°C to 950°C to obtain a test piece having a thickness of less than 25% of that of the cast piece.
- test piece was subjected to an initial water-quenching treatment followed by cooling to room temperature to obtain a water-quenched body.
- the water-quenched body was polished to remove an oxide layer, followed by an aging treatment at 500°C to obtain an aged body.
- the aged body was subjected to a further water-quenching treatment followed by cooling to room temperature.
- Example 1 In each of Examples 2 to 11, the procedure of Example 1 was repeated using the steel alloy shown in Table 1.
- Example 1 In each of Comparative Examples 1 to 3, the procedure of Example 1 was repeated using the steel alloy shown in Table 1. Table 1: Steel Alloy Fe (wt%) Mn (wt%) Al (wt%) C (wt%) Mo (wt%) Cr (wt%) Co (wt%) Ex. 1 balance 30 8.5 1.45 6 - - Ex. 2 balance 30 8.5 1.45 4 - - Ex. 3 balance 30 8.5 1.50 3.5 - - Ex. 4 balance 27 8.5 1.48 6 - - Ex. 5 balance 27.5 8.3 1.43 5 - - Ex. 6 balance 28 8.2 1.42 3.5 - - Ex. 7 balance 28.5 8.4 1.46 2 - - Ex. 8 balance 30 8.5 1.45 3 3 - Ex.
- test pieces were subjected a tensile test according to the specification of ASTM E8/E8M using an Instron tensile tester at a strain rate of 10 -3 /sec at a desirable temperature (i.e., 25°C, 300°C, 500°C, or 700°C).
- a desirable temperature i.e., 25°C, 300°C, 500°C, or 700°C.
- a relationship between stress and strain was recorded to obtain a stress-strain curve at the desirable temperature as that shown below.
- L2 and L3 are parallel to L1.
- Yield Strength Yield strength is defined as the stress obtained at 0.2% offset strain in the stress-strain curve, as shown by point A in the stress-strain curve.
- Ultimate Tensile Strength is defined as a maximum stress obtained before failure, as shown by point B in the stress-strain curve.
- Elongation is defined as the strain shown by point C in the stress-strain curve.
- the test pieces of Examples 1 to 11 have a yield strength at 25°C of from 1230 MPa to 1350 MPa, an ultimate tensile strength at 25°C of from 1280 MPa to 1386 MPa, an elongation at 25° of from 20% to 37%, and a Rockwell C hardness (HRc) of from 45.0 to 47.7. It is demonstrated that the test pieces of Examples 1 to 11 have superior mechanical strength and ductility as compared to the test pieces of Comparative Examples 1 and 2.
- the austenitic steel alloy of Examples 1 to 11 has superior mechanical strength and ductility at room temperature (i.e., 25°C) and sufficient mechanical strength at high temperature as well, by controlling the Mo amount in the steel alloy within a range of from 2 wt% to 6 wt% as compared to the steel alloy of Comparative Examples 1 to 3 and conventional AISI H13 and QRO 90 alloys. Therefore, when the austenitic steel alloy according to the disclosure is used to make hot work tools, the cracking problem encountered in the prior art can be avoided.
- the mechanical strength of each of the test pieces of Examples 1 to 11 is not significantly affected by the aging time of from 5 hours to 12 hours. It is demonstrated that the precipitation of coarse carbides on the grain boundaries of the austenitic steel can be avoided by controlling the temperature during the hot-working treatment. Therefore, the time period for the aging treatment of the austenitic steel alloy according to the disclosure can be more flexible, and the problem of significant precipitation of coarse carbides due to the longer aging time can be alleviated or even avoided.
- the test pieces of Examples 4, 7, and 9 has a yield strength at 300°C of from 970 MPa to 1030 MPa, an ultimate tensile strength at 300°C of from 1022 MPa to 1070 MPa, a yield strength at 500°C of from 650 MPa to 700 MPa, an ultimate tensile strength at 500°C of from 719 MPa to 786 MPa, a yield strength at 700°C of from 410 MPa to 420 MPa, and an ultimate tensile strength at 700°C of from 440 MPa to 449 MPa.
- the test piece of Comparative Example 3 has good ductility at 25°C, the yield strengths and the ultimate tensile strengths at 25°C, 300°C, and 500°C are relatively low as compared to the test pieces of Examples 4, 7, and 9. It is demonstrated that the austenitic steel made by the austenitic steel alloy according to the disclosure has superior mechanical strength both at room temperature (i.e., 25°C) and at high temperature, and thus can be used for making a hot work tools.
- the ductility of the austenitic steel made thereby can be improved by adding relatively low amount (s) of the strong carbide-forming element (s) such as molybdenum and/or tungsten.
- the mechanical strength of the austenitic steel cannot be significantly enhanced.
- the mechanical strength thereof can be improved by adding relatively high amount(s) of the strong carbide-forming element(s).
- the ductility thereof cannot be maintained.
- an austenitic steel possessing superior mechanical strength and high ductility both at room temperature and at high temperature can be made using the austenitic steel alloy via a method of this disclosure that includes a hot-working treatment at a temperature of from 1100°C to 950°C.
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Description
- The disclosure relates to an austenitic steel alloy, and more particularly to an austenitic steel alloy for hot work tools. The disclosure also relates to a method for making an austenitic steel using the alloy, and an austenitic steel made by the method.
- Martensitic steel is a steel material commonly used for making hot work tools due to its superior mechanical properties such as hardness and toughness. However, since the martensitic steel has a relatively low ductility, the hot work tools made therefrom are liable to cracking.
- AISI H13 steel is an example of the martensitic steel commonly used for making the hot work tools, and includes carbon in an amount of from 0.32 wt% to 0.45 wt%, silicon in an amount of from 0.80 wt% to 1.20 wt%, manganese in an amount of from 0.20 wt% to 0.50 wt%, chromium in an amount of from 4.75 wt% to 5.50 wt%, molybdenum in an amount of from 1.10 wt% to 1.75 wt%, vanadium in an amount of from 0.80 wt% to 1.20 wt%, phosphorus in an amount of not more than 0.03 wt%, sulfur in an amount of not more than 0.03 wt%, and a balance of iron. The AISI H13 steel has a room temperature hardness of from 55 to 58, an elongation at room temperature of from 3% to 5%, an impact toughness of from 5 Joules (J) to 10 J, and a high temperature Rockwell C hardness (HRc) of from 33 to 41. Since the AISI H13 steel having a relatively low elongation is liable to cracking during usage, the room temperature hardness thereof is usually reduced to a range of from 42 to 50 so as to increase the elongation to a range of from 5% to 8%.
- QRO 90 steel is another example of the martensitic steel commonly used for making the hot work tools, and includes carbon in an amount of 0.38 wt%, silicon in an amount of 0.30 wt%, manganese in an amount of 0.75 wt%, chromium in an amount of 2.60 wt%, molybdenum in an amount of 2.25 wt%, vanadium in an amount of 0.9 wt%, and a balance of iron. The QRO 90 steel has a room temperature hardness of 45, an elongation of about 11 %, an impact toughness of 10 J, and a high temperature Rockwell C hardness (HRc) of from 26 to 41.
- Alternatively, austenitic Fe-Mn-Al-C steel has been subjected to extensive researches over the last several decades because of its promising application that is potential associated with high mechanical strength and high ductility.
- Conventional austenitic Fe-Mn-Al-C steel containing carbon in an amount of greater than about 1.2 wt% may be deteriorated in terms of ductility and may be even cracked. Therefore, the amount of carbon in the conventional austenitic Fe-Mn-Al-C steel is usually controlled within a range of from 0.54 wt% to 1.3 wt% and is added with molybdenum (Mo), niobium (Nb), and/or tungsten (W) to enhance the mechanical strength thereof. However, ductility (i.e., elongation) of the conventional austenitic Fe-Mn-Al-C steel may be undesirably reduced due to precipitation of coarse carbides on the grain boundaries of the austenitic Fe-Mn-Al-C steel during an aging treatment. Accordingly, the hot work tools made therefrom are liable to cracking.
- Applicant's
U.S. Patent No. 9,528,177 -
US2013081740 is directed to Fe-Mn-Al-C alloys. InUS4975335 ,DE1262613 , andFR2634221 - A first object of the disclosure is to provide an austenitic steel alloy which possesses superior mechanical properties without compromising ductility at room temperature, and which also possesses superior mechanical properties at high temperature.
- A second object of the disclosure is to provide a method for making an austenitic steel using the austenitic steel alloy.
- A third object of the disclosure is to provide an austenitic steel made by the method.
- According to a first aspect of the disclosure, there is provided an austenitic steel alloy which comprises manganese in an amount of from 25 wt% to 31 wt%, aluminum in an amount of from 7 wt% to 10 wt%, carbon in an amount of from 1.4 wt% to 1.6 wt%, molybdenum in an amount of from 2 wt% to 6 wt%, optionally chromium in an amount of less than 6 wt%, optionally cobalt in an amount of less than 5 wt%, and a balance of iron.
- According to a second aspect of the disclosure, there is provided a method for making an austenitic steel using the austenitic steel alloy of the first aspect of the disclosure.
- According to a third aspect of the disclosure, there is provided an austenitic steel made by the method of the second aspect of the disclosure.
- The austenitic steel alloy according to the disclosure possesses superior mechanical properties both at room temperature and at high temperature (e.g., at about 500°C) which are achieved by adding molybdenum in an amount of less than 6 wt% into the austenitic steel alloy including manganese, aluminum, carbon, and iron in specific amounts.
- Other features and advantages of the disclosure will become apparent in the following detailed description of the embodiment (s) with reference to the accompanying drawings, of which:
-
Figure 1 is a flow diagram of an embodiment of a process for making an austenitic steel according to the disclosure; -
Figure 2 is an optical microscope photograph of an austenitic steel of Example 1 after a hot-working treatment; -
Figure 3 is an optical microscope photograph of an austenitic steel of Example 3 after a hot-working treatment; -
Figure 4 is an optical microscope photograph of an austenitic steel of Example 8 after a hot-working treatment; -
Figure 5 is an optical microscope photograph of an austenitic steel of Example 1 after an aging treatment; -
Figure 6 is an optical microscope photograph of an austenitic steel of Example 3 after an aging treatment; -
Figure 7 is an optical microscope photograph of an austenitic steel of Example 8 after an aging treatment; -
Figure 8 is an optical microscope photograph of an austenitic steel of Comparative Example 1 after a hot-working treatment; and -
Figure 9 is an optical microscope photograph of an austenitic steel of Comparative Example 2 after a hot-working treatment. - An austenitic steel alloy according to the disclosure comprises manganese (Mn) in an amount of from 25 wt% to 31 wt%, aluminum (Al) in an amount of from 7 wt% to 10 wt%, carbon (C) in an amount of from 1.4 wt% to 1.6 wt%, molybdenum (Mo) in an amount of from 2 wt% to 6 wt%, optionally chromium in an amount of less than 6 wt%, optionally cobalt in an amount of less than 5 wt%, and a balance of iron (Fe). The austenitic steel alloy according to the disclosure possesses superior mechanical properties and high ductility, and can be used for making general steel plates such as automobile steel plates, mechanical parts such as gears, hard work tools, and the like.
- Mn is a strong austenite-stabilizing element. An austenite phase is of face-center-cubic (FCC) structure with more dislocation slip systems, and thus possesses better ductility than other crystal structures, such as body-center-cubic (BCC) and hexagonal close packed (HCP) structures. Therefore, in order to obtain a fully austenite structure at room temperature, Mn is in an amount of from 25 wt% to 31 wt% in the austenitic steel alloy according to the disclosure. In certain embodiments, Mn is in an amount of from 26 wt% to 30 wt% . In certain embodiments, Mn is in an amount of from 27 wt% to 29 wt%.
- Al not only is a strong ferrite-stabilizing element, but also is one of the primary elements for forming (Fe,Mn)3AlCx carbides (i.e., κ' carbides). Al is in an amount of from 7 wt% to 10 wt% in the austenitic steel alloy according to the disclosure. In certain embodiments, Al is in an amount of from 8 wt% to 10 wt%. In certain embodiments, Al is in an amount of from 8 wt% to 9 wt%.
- C is in an amount of from 1.2 wt% to 1.6 wt% in the austenitic steel alloy according to the disclosure, which is relatively high as compared to the amount (i.e., up to 1.0 wt%) of C in the conventional austenitic Fe-Mn-Al-C steel, in which molybdenum (Mo), niobium (Nb), and/or tungsten (W) is added. In certain embodiments, C is in an amount of from 1.4 wt% to 1.6 wt%.
- Mo is a very strong carbide-forming element. Mo is in an amount of more than 0 wt% and less than 6 wt% in the austenitic steel alloy according to the disclosure. In certain embodiments, Mo is in an amount of from 2 wt% to 6 wt%.
- In certain embodiments, the austenitic steel alloy according to the disclosure further comprises chromium (Cr). Cr is also a very strong carbide-forming element. Cr is in an amount of less than 6 wt% in the austenitic steel alloy according to the disclosure.
- In certain embodiments, the austenitic steel alloy according to the disclosure further comprises cobalt (Co). Co is also a very strong carbide-forming element. Co is in an amount of less than 5 wt% in the austenitic steel alloy according to the disclosure.
- It should be noted that the amounts of low-melting elements (e.g., Mn and Al) in the austenitic steel alloy according to the disclosure may be slightly different from those of the low-melting elements in the austenitic steel made from the alloy due to the smelting that causes evaporation effect of the low-melting elements. However, the difference is within an acceptable tolerance. Therefore, the properties of the austenitic steel made from the alloy will not be affected.
- According to
Figure 1 , an embodiment of a method for making an austenitic steel according to the disclosure comprises steps of: - a) smelting the austenitic steel alloy according to the disclosure in a high-frequency smelting furnace under an atmosphere to obtain a molten steel alloy;
- b) casting the molten steel alloy to obtain a cast piece;
- c) subjecting the cast piece to a hot-working treatment such as hot-rolling, hot-forging, and the like at a temperature of from 1100°C to 950°C to obtain a hot-worked body having a predetermined shape;
- d) subjecting the hot-worked body to an initial water-quenching treatment followed by cooling to room temperature to obtain a water-quenched body;
- e) subjecting the water-quenched body to an aging treatment at a temperature of from 480°C to 600°C to obtain an aged body; and
- f) subjecting the aged body to a further water-quenching treatment followed by cooling to room temperature.
- In certain embodiments, in step c), the hot-worked body has a thickness of less than 25% of that of the cast piece.
- In certain embodiments, the temperature for the aging treatment in step e) is from 480°C to 500°C, and the aging treatment is implemented for a period of from 5 hours to 12 hours.
- In certain embodiments, the temperature for the aging treatment in step e) is larger than 500°C and up to 600°C, and the aging treatment is implemented for a period of from 1 hour to 4 hours.
- The method for making the austenitic steel according to the disclosure is different from the method for making the conventional austenitic Fe-Mn-Al-C steel having a relatively low carbon amount and containing strong carbide-forming elements. Specifically, in the method for making the conventional austenitic Fe-Mn-Al-C steel, a solution heat treatment is required after the hot-working treatment to dissolve the coarse carbides precipitated on the grain boundaries into a matrix phase so as to enhance the ductility of the conventional austenitic Fe-Mn-Al-C steel. In the method for making the austenitic steel according to the disclosure, although the austenitic steel alloy for making the austenitic steel has a relatively high carbon amount and contains strong carbide-forming elements, the temperature for implementing the hot-working treatment is controlled within a range of from 1100°C to 950°C such that the precipitation of the coarse carbides on the grain boundaries during the hot-working treatment can be avoided. Therefore, an austenitic steel having superior mechanical properties and high ductility can be made without the solution heat treatment, which is required in the method for making the conventional austenitic Fe-Mn-Al-C steel.
- It should be noted that instead of implementing the further water-quenching treatment in step f), the aged body can be cooled down naturally to room temperature. In addition, although the solution heat treatment is not a requisite in the method for making the austenitic steel according to the disclosure, it may be optionally implemented, if desired.
- The austenitic steel made by the method according to the disclosure has a fully austenitic phase, a yield strength at 25°C of from 1200 MPa to 1400 MPa, a Rockwell C hardness (HRc) at 25°C of from 45 to 55, an ultimate tensile strength at 25°C of from 1200 MPa to 1500 MPa, and an elongation at 25°C of from 20% to 40%. In addition, the austenitic steel made by the method according to the disclosure has superior yield strength and ultimate tensile strength at high temperature up to 700°C. Therefore, the austenitic steel made by the method according to the disclosure can be used for making general steel plates such as automobile steel plates, mechanical parts such as gears, hard work tools, and the like.
- In certain embodiments, the austenitic steel alloy according to the disclosure comprises carbon in an amount of from 1.42 wt% to 1.5 wt% and molybdenum in an amount of from 3.5 wt% to 5 wt%. The austenitic steel made by the austenitic steel alloy according to the disclosure has an ultimate tensile strength at 25°C of from 1353 MPa to 1386 MPa, a yield strength at 25°C of from 1310 MPa and 1340 MPa, and a HRc at 25°C of from 47 to 47.7.
- In certain embodiments, the austenitic steel alloy according to the disclosure comprises carbon in an amount of from 1.42 wt% to 1.45 wt% and molybdenum in an amount of from 3.5 wt% to 4 wt%. The austenitic steel made by the austenitic steel alloy according to the disclosure has an elongation at 25°C of 25%.
- In certain embodiments, the austenitic steel alloy according to the disclosure comprises manganese in an amount of from 27.7 wt% to 30 wt% and aluminum in an amount of from 8.2 wt% to 8.5 wt% . The austenitic steel made by the austenitic steel alloy according to the disclosure has an ultimate tensile strength at 25°C of from 1280 MPa to 1386 MPa, a yield strength at 25°C of from 1250 MPa and 1350 MPa, a hardness (HRc) at 25°C of from 46.7 to 47.7, and an elongation at 25°C of from 20% to 32%.
- In certain embodiments, the austenitic steel alloy according to the disclosure comprises manganese in an amount of from 27 wt% to 29 wt%, aluminum in an amount of from 8.0 wt% to 8.5 wt%, and molybdenum in an amount of from 3.0 wt% to 6 wt%. The austenitic steel made by the austenitic steel alloy according to the disclosure has an elongation at 25°C of more than 20%, an ultimate tensile strength at 25°C of more than 1280 MPa, a yield strength at 25°C of more than 1230 MPa, an ultimate tensile strength at 300 °C of more than 1000 MPa, and a yield strength at 300 °C of more than 1000 MPa.
- In certain embodiments, the austenitic steel alloy according to the disclosure comprises molybdenum in an amount of 3.0 wt%, and further comprises chromium in an amount of 3 wt% or cobalt in an amount of 2 wt%. The austenitic steel made by the austenitic steel alloy according to the disclosure has an ultimate tensile strength at 25°C of from 1280 MPa to 1344 MPa, a yield strength at 25°C of from 1230 MPa and 1300 MPa, a hardness (HRc) at 25°C of from 45 to 46.8, and an elongation at 25°C of from 24% to 37%.
- Furthermore, the presently available steel for the hot work tools has a density of from 7.8 g/cm3 to 7.9 g/cm3. The austenitic steel made by the method according to the disclosure has a density of from 6.6 g/cm3 to 6.8 g/cm3, which is 14% less than the density of the presently available steel. Therefore, in addition to superior mechanical properties and high ductility, the austenitic steel made by the method according to the disclosure has a lightweight advantage.
- The conventional Fe-Mn-Al-C alloy having a relatively high amount of carbon of from 1.4 wt% to 2.2 wt% can possess a fully austenitic phase, form a high density of fine κ' carbides (i.e., (Fe,Mn)3AlCxcarbides) within an austenite matrix, and avoid the precipitation of coarse carbides on the grain boundaries so as to possess superior mechanical strength and high ductility by controlling the hot-working treatment, the solution heat treatment, and the water-quenching treatment. However, in the method for making an austenitic steel according to the disclosure, by adding specific amounts of the strong carbide-forming elements (i.e., Mo and optionally Cr and Co) in the austenitic steel alloy and by controlling the temperature for implementing the hot-working treatment within a specific range (i.e., from 1100°C to 950°C), the precipitation of coarse carbides on the grain boundaries during the hot-working treatment can be avoided. Therefore, an austenitic steel having superior mechanical properties and high ductility can be made without the solution heat treatment which is required in the method for making the conventional austenitic Fe-Mn-Al-C steel.
- Examples of the disclosure will be described hereinafter. It is to be understood that these examples are exemplary and explanatory and should not be construed as a limitation to the disclosure.
- A steel alloy containing 30 wt% of Mn, 8.5 wt% of Al, 1.45 wt% of C, 6 wt% of Mo, and a balance of Fe was smelted in a high-frequency smelting furnace under an atmosphere to obtain a molten steel alloy, followed by casting the molten steel alloy to obtain a cast piece having a thickness of 2 cm.
- The cast piece was heated in a furnace at 1100°C, followed by hot-rolling at a temperature of from 1100°C to 950°C to obtain a test piece having a thickness of less than 25% of that of the cast piece.
- The test piece was subjected to an initial water-quenching treatment followed by cooling to room temperature to obtain a water-quenched body.
- The water-quenched body was polished to remove an oxide layer, followed by an aging treatment at 500°C to obtain an aged body.
- The aged body was subjected to a further water-quenching treatment followed by cooling to room temperature.
- In each of Examples 2 to 11, the procedure of Example 1 was repeated using the steel alloy shown in Table 1.
- In each of Comparative Examples 1 to 3, the procedure of Example 1 was repeated using the steel alloy shown in Table 1.
Table 1: Steel Alloy Fe (wt%) Mn (wt%) Al (wt%) C (wt%) Mo (wt%) Cr (wt%) Co (wt%) Ex. 1 balance 30 8.5 1.45 6 - - Ex. 2 balance 30 8.5 1.45 4 - - Ex. 3 balance 30 8.5 1.50 3.5 - - Ex. 4 balance 27 8.5 1.48 6 - - Ex. 5 balance 27.5 8.3 1.43 5 - - Ex. 6 balance 28 8.2 1.42 3.5 - - Ex. 7 balance 28.5 8.4 1.46 2 - - Ex. 8 balance 30 8.5 1.45 3 3 - Ex. 9 balance 28.5 8.0 1.52 3 3 - Ex. 10 balance 30 8.5 1.45 3 - 2 Ex. 11 balance 27 8.2 1.42 3 - 2 Comp. Ex. 1 balance 28.5 8.2 1.45 9 - - Comp. Ex. 2 balance 28 8.3 1.53 9 5 - Comp. Ex. 3 balance 28.5 8.3 1.5 - - - - Each of the test pieces of Examples 1 to 11 and Comparative Examples 1 to 3 was subjected to yield strength (YS), ultimate tensile strength (UTS), elongation (El), and Rockwell C hardness (HRc) measurements at 25°C according to the procedures described below. The results are shown in Table 2.
- Each of the test pieces of Examples 4, 7, and 9 and Comparative Examples 1 to 3 was subjected to yield strength (YS) and ultimate tensile strength (UTS) measurements at 300°C, 500°C, and 700°C according to the procedures described below. The results are shown in Table 3.
- Each of the test pieces was subjected a tensile test according to the specification of ASTM E8/E8M using an Instron tensile tester at a strain rate of 10-3/sec at a desirable temperature (i.e., 25°C, 300°C, 500°C, or 700°C). For each of the test pieces, a relationship between stress and strain was recorded to obtain a stress-strain curve at the desirable temperature as that shown below.
- 1. Yield Strength (YS):
Yield strength is defined as the stress obtained at 0.2% offset strain in the stress-strain curve, as shown by point A in the stress-strain curve. - 2. Ultimate Tensile Strength (UTS):
Ultimate tensile strength is defined as a maximum stress obtained before failure, as shown by point B in the stress-strain curve. - 3. Elongation (El) :
Elongation is defined as the strain shown by point C in the stress-strain curve. - 4. Rockwell C Hardness (HRc)
Rockwell C hardness of each of the test pieces was measured using a Rockwell hardness machine at a load of 150 kgf. A diamond conical indenter was used for the measurement. The results are shown in Table 2.Table 2 Steel Alloy YS (MPa) UTS (MPa) El (%) Rockwell C hardness (HRc) Aging time (500°C/h) Ex. 1 1350 1375 20 47.4 12 Ex. 2 1340 1366 25 47.0 12 Ex. 3 1330 1386 22 47.7 6 Ex. 4 1230 1308 21 46.3 12 Ex. 5 1320 1365 20 47.4 12 Ex. 6 1310 1353 24 47.0 6 Ex. 7 1250 1314 20 46.5 12 Ex. 8 1300 1322 26 45.0 12 Ex. 9 1300 1344 24 46.8 12 Ex. 10 1250 1280 32 46.7 5 Ex. 11 1230 1280 37 46.7 5 Comp. Ex. 1 1400 1464 7 50.2 6 Comp. Ex. 2 1360 1410 5 49.0 5 Comp. Ex. 3 1210 1262 38 45.6 2.5 Table 3: Steel Alloy 300°C 500°C 700°C YS UTS YS UTS YS UTS Ex. 4 1000 1033 690 758 410 440 Ex. 7 970 1022 650 719 410 449 Ex. 9 1030 1070 700 786 420 444 Comp. Ex. 1 1020 1047 750 827 420 442 Comp. Ex. 2 1010 1068 680 749 400 427 Comp. Ex. 3 850 938 600 670 530 559 - As shown in Table 2, the test pieces of Examples 1 to 11 have a yield strength at 25°C of from 1230 MPa to 1350 MPa, an ultimate tensile strength at 25°C of from 1280 MPa to 1386 MPa, an elongation at 25° of from 20% to 37%, and a Rockwell C hardness (HRc) of from 45.0 to 47.7. It is demonstrated that the test pieces of Examples 1 to 11 have superior mechanical strength and ductility as compared to the test pieces of Comparative Examples 1 and 2. Specifically, the austenitic steel alloy of Examples 1 to 11 has superior mechanical strength and ductility at room temperature (i.e., 25°C) and sufficient mechanical strength at high temperature as well, by controlling the Mo amount in the steel alloy within a range of from 2 wt% to 6 wt% as compared to the steel alloy of Comparative Examples 1 to 3 and conventional AISI H13 and QRO 90 alloys. Therefore, when the austenitic steel alloy according to the disclosure is used to make hot work tools, the cracking problem encountered in the prior art can be avoided.
- In addition, as shown in Table 2, the mechanical strength of each of the test pieces of Examples 1 to 11 is not significantly affected by the aging time of from 5 hours to 12 hours. It is demonstrated that the precipitation of coarse carbides on the grain boundaries of the austenitic steel can be avoided by controlling the temperature during the hot-working treatment. Therefore, the time period for the aging treatment of the austenitic steel alloy according to the disclosure can be more flexible, and the problem of significant precipitation of coarse carbides due to the longer aging time can be alleviated or even avoided.
- Referring to
Figures 2 to 4 , there is no precipitation of coarse carbides seen in each of the test pieces of Examples 1, 3, and 8 after the hot-working treatment at a temperature of from 1100°C to 950°C. Referring toFigures 5 to 7 , there is also no precipitation of coarse carbides seen in each of the test pieces of Examples 1, 3, and 8 after the hot-working treatment at a temperature of from 1100°C to 950°C, followed by the aging treatment. Referring toFigures 8 and 9 , however, there is significant precipitation of coarse carbides seen in each of the test pieces of Comparative Examples 1 and 2, in which the strong carbide-forming elements are added in an excess amount. - Furthermore, as shown in Table 3, the test pieces of Examples 4, 7, and 9 has a yield strength at 300°C of from 970 MPa to 1030 MPa, an ultimate tensile strength at 300°C of from 1022 MPa to 1070 MPa, a yield strength at 500°C of from 650 MPa to 700 MPa, an ultimate tensile strength at 500°C of from 719 MPa to 786 MPa, a yield strength at 700°C of from 410 MPa to 420 MPa, and an ultimate tensile strength at 700°C of from 440 MPa to 449 MPa. Although the test piece of Comparative Example 3 has good ductility at 25°C, the yield strengths and the ultimate tensile strengths at 25°C, 300°C, and 500°C are relatively low as compared to the test pieces of Examples 4, 7, and 9. It is demonstrated that the austenitic steel made by the austenitic steel alloy according to the disclosure has superior mechanical strength both at room temperature (i.e., 25°C) and at high temperature, and thus can be used for making a hot work tools.
- In view of the aforesaid, in a conventional austenitic Fe-Mn-Al-C steel containing carbon in an amount of not more than 1 wt%, the ductility of the austenitic steel made thereby can be improved by adding relatively low amount (s) of the strong carbide-forming element (s) such as molybdenum and/or tungsten. However, the mechanical strength of the austenitic steel cannot be significantly enhanced. On the other hand, in such austenitic Fe-Mn-Al-C steel, the mechanical strength thereof can be improved by adding relatively high amount(s) of the strong carbide-forming element(s). However, the ductility thereof cannot be maintained. In
U.S. Patent No. 9,528,177 - In the description above, for the purposes of explanation, numerous specific details have been set forth in order to provide a thorough understanding of the embodiment (s). It will be apparent, however, to one skilled in the art, that one or more other embodiments may be practiced without some of these specific details. It should also be appreciated that reference throughout this specification to "one embodiment," "an embodiment," an embodiment with an indication of an ordinal number and so forth means that a particular feature, structure, or characteristic may be included in the practice of the disclosure. It should be further appreciated that in the description, various features are sometimes grouped together in a single embodiment, figure, or description thereof for the purpose of streamlining the disclosure and aiding in the understanding of various inventive aspects, and that one or more features or specific details from one embodiment may be practiced together with one or more features or specific details from another embodiment, where appropriate, in the practice of the disclosure.
Claims (12)
- An austenitic steel alloy comprising:manganese in an amount of from 25 wt% to 31 wt%;aluminum in an amount of from 7 wt% to 10 wt%;carbon in an amount of from 1.4 wt% to 1.6 wt%; characterized by molybdenum in an amount of from 2 wt% to 6 wt%;optionally chromium in an amount of less than 6 wt%;optionally cobalt in an amount of less than 5 wt%; anda balance of iron.
- The austenitic steel alloy according to Claim 1, characterized in that said manganese is in an amount of from 26 wt% to 30 wt% and said aluminum is in an amount of from 8 wt% to 10 wt%.
- The austenitic steel alloy according to Claim 2, characterized in that said aluminum is in an amount of from 8 wt% to 9 wt%.
- A method for making an austenitic steel, characterized by steps of:a) smelting the austenitic steel alloy of any one of Claims 1 to 3 to obtain a molten steel alloy;b) casting the molten steel alloy to obtain a cast piece;c) subjecting the cast piece to a hot-working treatment at a temperature of from 1100°C to 950°C to obtain a hot-worked body;d) subjecting the hot-worked body to an initial water-quenching treatment to obtain a water-quenched body; ande) subjecting the water-quenched body to an aging treatment at a temperature of from 480°C to 600°C to obtain an aged body, wherein the aging treatment is implemented for a period of from 5 hours to 12 hours.
- The method according to Claim 4, characterized in that the temperature for the aging treatment is from 480°C to 500°C, and the aging treatment is implemented for a period of from 5 hours to 12 hours.
- The method according to Claim 4 or 5, further characterized by a step of subjecting the aged body to a further water-quenching treatment.
- The method according to any one of Claims 4 to 6, characterized in that in step c), the hot-worked body has a thickness of less than 25% of that of the cast piece.
- An austenitic steel made from the austenitic steel alloy according to any one of Claims 1 to 3, characterized in that said austenitic steel has a fully austenitic phase, a yield strength at 25°C of from 1200 MPa to 1400 MPa, a Rockwell C hardness at 25°C of from 45 to 55, an ultimate tensile strength at 25°C of from 1200 MPa to 1500 MPa, and an elongation at 25°C of from 20% to 40%.
- The austenitic steel according to Claim 8, characterized in that said austenitic steel has an ultimate tensile strength at 300°C of larger than 1000 MPa.
- The austenitic steel according to Claim 8 or 9, characterized in that said austenitic steel has a yield strength at 300°C of larger than 970 MPa.
- The austenitic steel according to any one of Claims 8 to 10, characterized in that said austenitic steel has a yield strength at 500°C of larger than 650 MPa and an ultimate tensile strength at 500°C of larger than 700 MPa.
- The austenitic steel according to any one of Claims 8 to 11, characterized in that said austenitic steel has a yield strength at 700°C of from 410 MPa to 420 MPa and an ultimate tensile strength at 700°C of from 440 MPa to 449 MPa.
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TW107123925A TWI715852B (en) | 2018-07-11 | 2018-07-11 | Austenitic alloy steel |
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EP (1) | EP3594376B1 (en) |
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