CA3066726A1 - Impact resistant high strength steel - Google Patents
Impact resistant high strength steel Download PDFInfo
- Publication number
- CA3066726A1 CA3066726A1 CA3066726A CA3066726A CA3066726A1 CA 3066726 A1 CA3066726 A1 CA 3066726A1 CA 3066726 A CA3066726 A CA 3066726A CA 3066726 A CA3066726 A CA 3066726A CA 3066726 A1 CA3066726 A1 CA 3066726A1
- Authority
- CA
- Canada
- Prior art keywords
- plate
- steel
- steel sheet
- alloy
- less
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 229910000831 Steel Inorganic materials 0.000 title claims abstract description 140
- 239000010959 steel Substances 0.000 title claims abstract description 140
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims abstract description 64
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 49
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 48
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims abstract description 46
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 46
- 239000010936 titanium Substances 0.000 claims abstract description 46
- 229910000734 martensite Inorganic materials 0.000 claims abstract description 39
- 238000010791 quenching Methods 0.000 claims abstract description 38
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 37
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 32
- 229910000851 Alloy steel Inorganic materials 0.000 claims abstract description 31
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 28
- 229910052802 copper Inorganic materials 0.000 claims abstract description 27
- 239000010949 copper Substances 0.000 claims abstract description 27
- 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 claims abstract description 26
- 230000000171 quenching effect Effects 0.000 claims abstract description 22
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims abstract description 19
- 229910052796 boron Inorganic materials 0.000 claims abstract description 19
- 229910052742 iron Inorganic materials 0.000 claims abstract description 18
- 229910001567 cementite Inorganic materials 0.000 claims abstract description 8
- KSOKAHYVTMZFBJ-UHFFFAOYSA-N iron;methane Chemical compound C.[Fe].[Fe].[Fe] KSOKAHYVTMZFBJ-UHFFFAOYSA-N 0.000 claims abstract description 4
- 229910045601 alloy Inorganic materials 0.000 claims description 52
- 239000000956 alloy Substances 0.000 claims description 52
- 238000000034 method Methods 0.000 claims description 18
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 14
- 229910052725 zinc Inorganic materials 0.000 claims description 14
- 239000011701 zinc Substances 0.000 claims description 14
- 238000010438 heat treatment Methods 0.000 claims description 12
- 239000013078 crystal Substances 0.000 claims description 11
- 229910052751 metal Inorganic materials 0.000 claims description 10
- 239000002184 metal Substances 0.000 claims description 10
- 238000004519 manufacturing process Methods 0.000 claims description 9
- 229910000765 intermetallic Inorganic materials 0.000 claims description 8
- 229910052782 aluminium Inorganic materials 0.000 claims description 6
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 6
- 230000007704 transition Effects 0.000 claims description 6
- 238000006073 displacement reaction Methods 0.000 claims description 5
- 229910000859 α-Fe Inorganic materials 0.000 claims description 5
- 238000005097 cold rolling Methods 0.000 claims description 4
- 238000005098 hot rolling Methods 0.000 claims description 4
- 238000003618 dip coating Methods 0.000 claims description 3
- 239000000463 material Substances 0.000 description 9
- 229910001566 austenite Inorganic materials 0.000 description 6
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 5
- 229910052748 manganese Inorganic materials 0.000 description 5
- 239000011572 manganese Substances 0.000 description 5
- 229910052758 niobium Inorganic materials 0.000 description 5
- 239000010955 niobium Substances 0.000 description 5
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 5
- 229910001220 stainless steel Inorganic materials 0.000 description 4
- 238000007792 addition Methods 0.000 description 3
- 230000032683 aging Effects 0.000 description 3
- 229910001563 bainite Inorganic materials 0.000 description 3
- 239000011159 matrix material Substances 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 229910001339 C alloy Inorganic materials 0.000 description 2
- 229910000975 Carbon steel Inorganic materials 0.000 description 2
- 229910001240 Maraging steel Inorganic materials 0.000 description 2
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 229910052750 molybdenum Inorganic materials 0.000 description 2
- 239000011733 molybdenum Substances 0.000 description 2
- 239000004033 plastic Substances 0.000 description 2
- 238000003303 reheating Methods 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 238000010583 slow cooling Methods 0.000 description 2
- 238000002791 soaking Methods 0.000 description 2
- 229910052715 tantalum Inorganic materials 0.000 description 2
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 2
- WGACMNAUEGCUHG-VYBOCCTBSA-N (2s)-2-[[(2s)-2-[[(2s)-2-acetamidopropanoyl]amino]propanoyl]amino]-n-[(2s)-6-amino-1-[[(2s)-1-[(2s)-2-[[(2s)-1-[[(2s)-5-amino-1-[[(2s)-1-[[(2s)-1-[[(2s)-6-amino-1-[[(2s)-1-amino-3-(4-hydroxyphenyl)-1-oxopropan-2-yl]amino]-1-oxohexan-2-yl]amino]-3-hydroxy- Chemical compound CC(=O)N[C@@H](C)C(=O)N[C@@H](C)C(=O)N[C@@H](CCC(N)=O)C(=O)N[C@@H](CCCCN)C(=O)N[C@@H](CCCN=C(N)N)C(=O)N1CCC[C@H]1C(=O)N[C@@H](CO)C(=O)N[C@@H](CCC(N)=O)C(=O)N[C@@H](CCCN=C(N)N)C(=O)N[C@@H](CO)C(=O)N[C@@H](CCCCN)C(=O)N[C@H](C(N)=O)CC1=CC=C(O)C=C1 WGACMNAUEGCUHG-VYBOCCTBSA-N 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 150000001721 carbon Chemical class 0.000 description 1
- 125000004432 carbon atom Chemical group C* 0.000 description 1
- 229910052729 chemical element Inorganic materials 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 239000000306 component Substances 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 239000002826 coolant Substances 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 108010074544 myelin peptide amide-12 Proteins 0.000 description 1
- 108010074682 myelin peptide amide-16 Proteins 0.000 description 1
- UFMBFIIJKCBBHN-MEKJRKEKSA-N myelin peptide amide-16 Chemical compound C([C@@H](C(=O)N[C@@H](CC(C)C)C(=O)N[C@@H](C)C(=O)N[C@@H](CO)C(=O)N[C@@H](C)C(N)=O)NC(=O)[C@H](CCCCN)NC(=O)[C@H](CO)NC(=O)[C@H](CCCNC(N)=N)NC(=O)[C@H](CCC(N)=O)NC(=O)[C@H](CO)NC(=O)[C@H]1N(CCC1)C(=O)[C@H](CCCNC(N)=N)NC(=O)[C@H](CCCCN)NC(=O)[C@H](CCC(N)=O)NC(=O)[C@H](C)NC(=O)[C@H](C)NC(C)=O)C1=CC=C(O)C=C1 UFMBFIIJKCBBHN-MEKJRKEKSA-N 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 230000000737 periodic effect Effects 0.000 description 1
- 230000001376 precipitating effect Effects 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 238000004881 precipitation hardening Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 230000035945 sensitivity Effects 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- 238000004627 transmission electron microscopy Methods 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Classifications
-
- 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
- C22C38/14—Ferrous alloys, e.g. steel alloys containing titanium or zirconium
-
- 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
- C21D1/19—Hardening; Quenching with or without subsequent tempering by interrupted quenching
-
- 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
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
-
- 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
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0226—Hot rolling
-
- 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
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0236—Cold rolling
-
- 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
-
- 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
-
- 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
- C22C38/08—Ferrous alloys, e.g. steel alloys containing nickel
-
- 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
- C22C38/16—Ferrous alloys, e.g. steel alloys containing copper
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
- C23C2/022—Pretreatment of the material to be coated, e.g. for coating on selected surface areas by heating
- C23C2/0224—Two or more thermal pretreatments
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/04—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor characterised by the coating material
- C23C2/06—Zinc or cadmium or alloys based thereon
-
- 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
- C21D2211/004—Dispersions; Precipitations
-
- 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
- C21D2211/008—Martensite
-
- 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
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Crystallography & Structural Chemistry (AREA)
- Heat Treatment Of Sheet Steel (AREA)
- Heat Treatment Of Steel (AREA)
Abstract
The present invention describes a novel steel sheet or plate formed of a martensitic steel alloy having iron, at least some of the iron having dislocations; less than 5% of any combination of nickel, manganese, and copper; from about 0.0001% to about 0.01% boron; from about 0.075% to about 6.5% titanium; more than 0.003% and less than 0.1% carbon; and less than 7% of all other elements. The steel has substantially no cementite, the titanium has clustered at the dislocations, and the steel sheet or plate has been formed by quenching off of a hot sheet or plate mill.
Description
IMPACT RESISTANT HIGH STRENGTH STEEL
CROSS REFERENCE TO RELATED APPLICATIONS
[0001] In those jurisdictions where a priority claim is proper, this application claims the benefit of U.S. Patent Application Serial No. 15/989,705 entitled "IMPACT RESISTANT
HIGH
STRENGTH STEEL," filed on May 25, 2018, and claims the benefit of PCT
Application Serial No. PCT/U52018/036332 entitled "IMPACT RESISTANT HIGH STRENGTH STEEL," filed on June 6, 2018, the contents of all of which are incorporated in this disclosure by reference in their entirety.
BACKGROUND
CROSS REFERENCE TO RELATED APPLICATIONS
[0001] In those jurisdictions where a priority claim is proper, this application claims the benefit of U.S. Patent Application Serial No. 15/989,705 entitled "IMPACT RESISTANT
HIGH
STRENGTH STEEL," filed on May 25, 2018, and claims the benefit of PCT
Application Serial No. PCT/U52018/036332 entitled "IMPACT RESISTANT HIGH STRENGTH STEEL," filed on June 6, 2018, the contents of all of which are incorporated in this disclosure by reference in their entirety.
BACKGROUND
[0002] In order to decrease fuel consumption, increase safety and accelerate commercialization of aircraft, automobiles and other motor driven platforms, high strength materials have been developed with advantageous properties such as reduced weight and increased strength. However, many of these new materials have the disadvantage of high cost, making widespread usage unaffordable, thus restricting these materials to niche applications.
[0003] The steel industry has met this need with a general family of steels collectively known as Advanced High Strength Steels. These steels, including interstitial free steels, Dual/Complex Phase, Transformation Induced Plasticity and martensite have been used in the automotive industry; however, they are reaching limits on specific mechanical properties and affordability. Therefore, there is a need for a new type of steel that has advantageous properties and reduced cost, thereby reducing weight, increasing safety, and maintaining or increasing affordability.
SUMMARY
SUMMARY
[0004] The present invention provides a steel sheet or plate formed of a martensitic steel alloy comprising: a) iron, at least some of the iron having dislocations; b) less than 5% of any combination of nickel, manganese, and copper; c) from about 0.0001 to about 0.01% boron; d) from about 0.05% to about 6.5 % titanium; e) more than 0.003% and less than 0.1% carbon; and 0 less than 7% of all other elements. The alloy has substantially no copper and substantially no cementite. In one aspect, the alloy is substantially a martensitic structure with minor ferrite zones and the titanium has clustered at the dislocations.
[0005] In one aspect, the alloy comprises more than 0.1% titanium. In another aspect, the alloy comprises more than 0.12% titanium. In another aspect, the alloy comprises more than 0.14% titanium. In another aspect, the alloy comprises more than 0.2%
titanium.
titanium.
[0006] In one aspect, the alloy comprises less than 0.5% of any combination of nickel, manganese, and copper. In another aspect, the alloy comprises less than 1% of any combination of nickel, manganese, and copper. In another aspect, the alloy comprises less than 1.5% of any combination of nickel, manganese, and copper. In another aspect, the alloy comprises less than 2% of any combination of nickel, manganese, and copper. In another aspect, the alloy comprises less than 2.5% of any combination of nickel, manganese, and copper. In another aspect, the alloy comprises less than 3% of any combination of nickel, manganese and copper.
[0007] In one aspect, the alloy comprises less than 0.05% carbon. In another aspect, the alloy comprises less than 0.04% carbon. In another aspect, the alloy comprises less than 0.03% carbon.
In another aspect, the alloy comprises less than 0.02% carbon. In another aspect, the alloy comprises less than 0.01% carbon.
10008} In one aspect, the alloy comprises at least 0.025% aluminum.
100091 In one aspect, the steel sheet or plate can be cold rolled.
Optionally, the steel sheet or plate has been hot dip coated in zinc or an alloy containing zinc without substantially crystallizing the martensitic steel structure. Optionally, the steel sheet or plate can be formed by quenching off of a hot sheet or plate mill.
100101 After quenching, or after cold roll, the sheet can be reheated to a temperature of between 200 C and 750 C and maintained at that temperature for more than one minute.
[0011] In another aspect, the present invention is a method of making a steel sheet or plate formed of a martensitic steel alloy. The method comprises the steps of: a) heating the alloy steel to a sufficiently high temperature that the steel transitions to an austenitic, face centered cubic lattice phase and the titanium removes substantially all of the carbon from the crystal lattice by forming a metal carbide other than iron carbide; b) hot rolling the heated alloy steel of step (a);
and c) quenching the hot rolled steel of step (b) a quench temperature with a quench faster than still air such that a body centered cubic lattice is formed by displacement.
[0012] In one aspect, the method comprises cold rolling the alloy steel to form the sheet or plate before the step of quenching.
[0013] In one aspect, the quench temperature is from about 200 to about 750 degrees C.
[0014] In one aspect, the step of heating comprises heating to a temperature greater than 1000 degree C.
[0015] In one aspect, after quenching, the hot rolled steel is maintained at a temperature of greater than 200 degree C for a sufficient time to form order intermetallics.
[0016] In one aspect, after quenching, the rolled steel is heated to a reheat temperature of between 200 C and 750 C and maintaining it at the reheat temperature for more than one minute.
[0017] In one aspect, the method comprises the additional step of hot dip coating the rolled steel in zinc or an alloy containing zinc without substantially crystallizing the martensitic steel structure.
[0018] This invention has applications outside the automotive industry, and is useful wherever high strength, low cost steel is desirable.
DRAWINGS
[0019] The detailed description of some embodiments of the invention is made below with reference to the accompanying Figures 1A-1B.
[00201 Figure IA is a schematic of steps involved in a method of making steel according to the present invention; and 100211 Figure 1B is a schematic of steps involved in the method of making steel according to the present invention.
DESCRIPTION
100221 As used herein, the following terms and variations thereof have the meanings given below, unless a different meaning is clearly intended by the context in which such term is used.
100231 The terms "a," "an," and "the" and similar referents used herein are to be construed to cover both the singular and the plural unless their usage in context indicates otherwise.
100241 Definitions of chemical terms and general terms used throughout the specification are described in more detail herein, but unless otherwise indicated the chemical elements are identified in accordance with the Periodic Table of the Elements, CAS version, Handbook of Chemistry and Physics, 75th Ed., inside cover, or are terms that are well known to one of skill in the art.
100251 Percentages referred to herein are percentages by weight.
100261 As used in this disclosure, the term "comprises" and variations of the term, such as "comprising" and "comprises," are not intended to exclude other additives, components, ingredients or steps.
100271 As used herein, "dislocation" refers to a crystallographic defect or irregularity within a crystal structure of a material on an atomic scale. The presence of dislocations influences many of the properties of materials. Transmission electron microscopy (TEM) can be used to observe dislocations within the crystal structure of the material.
100281 Interstitial free steel is well known in the steel industry where the higher cost of these types of steels are acceptable due to the excellent forming properties and a lack of yield point elongation. These steels typically have low yield strength, high plastic strain ratio, high strain rate sensitivity and good formability. Interstitial free steels have interstitial free body centered cubic ferrite matrix. Carbon is kept very low and is stabilized, or removed, from the crystal lattice structure of the steel, normally with titanium, niobium or both. The disadvantage of these steels is the relatively low strength of the ferrite.
100291 Austenite steel has a face-centered cubic crystal structure. The carbon atoms lie in the interstices (holes) between the larger iron atoms. At slow cooling rates, the carbon moves ahead of the interface into the austenite iron by diffusion. Austenite steel may be strengthened by rapid cooling (quenching) by, for example, immersing the hot metal into liquid coolants such as water, oil, or liquid salts. Steels can also be quenched by air.
[0030] The term "martensitic steel alloy" is defined herein to be any steel or alloy steel that transitions from a face centered cubic lattice phase to a body centered cubic lattice phase predominantly by displacement and/or shear and not by substitution. When austenite is rapidly cooled, a martensite phase is formed. Martensite, tempered martensite and bainite are high strength steels that are well known in the steel industry where very high strength is required.
Bainite steel is within the definition of martensitic steel alloy.
[0031] In tempered martensite and bainite, the carbon migrates out of the lattice structure and forms a metal carbide. The disadvantage of these steels is the high carbon content required to form martensite. This causes a reduction in elongation and toughness with an inverse relationship to the increase in strength.
[0032] Additionally, Maraging and PH stainless steels are well known in the aerospace industry, where the higher cost of these types of steels are acceptable due to the excellent properties inherent in precipitating a nickel intermetallic. All current generation advanced high strength steels rely on carbon to some extent to add strength and/or facilitate other reactions.
Maraging and PH stainless steels rely on formation of a martensitic steel matrix and, with aging, precipitation of a nickel intermetallic with aluminum, molybdenum, titanium, niobium, tantalum or other metals known to those skilled in the art. A typical Maraging steel may be composed of 18% - 19% nickel, 8% - 10% cobalt, 3% - 5.5% molybdenum, 0.15% - 1.6% titanium and 0.5%
niobium, and after aging exceed 2,400 Ivfl'a yield and tensile strength. A
typical PH stainless steel may be composed of 15% chrome, 4% nickel, 3% copper, and 0.15% - 0.45%
of tantalum and niobium. Carbon is kept low. This family of alloys will form martensite upon slow heat of the metal to a solution treatment temperature, and then let the metal air cool to room temperature, which forms intermetallics. The disadvantage of these steels is the high alloy content required to form a martensite steel matrix with slow cooling rates. The high alloy content also increases cost beyond what a high-volume application can justify.
[0033] Thus, there is a need for high strength interstitial free or predominantly interstitial free steel that is capable of forming shear martensite without high alloy additions and without carbon in the crystal lattice structure.
[0034] This invention provides a material that contains low alloy additions that remove carbon from the high temperature face centered crystal lattice and enable an industry standard quench to transform the steel to an interstitial free martensite without a temper treatment. When higher strength is required, the material of the invention may be heated to a precipitation hardening temperature to form an additional ordered intermetallic. The martensitic steel of the invention has substantially all of the carbon removed from the crystal lattice of the austenite prior to forming martensite, forming an interstitial free martensite that is strengthened not with carbon/carbon iron but by pinning the dislocations with an intermetallic.
[0035] In particular, the present invention provides a new type of a steel sheet or plate formed of a martensitic steel alloy comprising: a) iron, at least some of the iron having dislocations; b) less than about 5% of any combination of nickel, manganese, and copper; c) from about 0.0001% to about 0.01% boron; d) from about 0.05% to about 6.5%
titanium; e) more than about 0.003% and less than about 0.1% carbon; and f) less than about 7%
of all other elements. "All other elements" means elements other than iron, nickel, manganese, copper, boron, titanium, and carbon.
[0036] The steel preferably has substantially no cementite, substantially no interstitial carbon, substantially no interstitial nitrogen, and substantially no copper.
The steel has titanium dispersed in the iron with the titanium clustered at the dislocations.
Optionally, the steel is substantially a martensitic structure with minor ferrite zones. The sheet or plate is typically formed by quenching off of a hot sheet or plate mill. The method of making the steel is discussed in more detail below.
[0037] Titanium and boron are very strong hardenability agents that are believed to work synergistically together to form martensite without the normal carbon additions that are used in plain carbon and alloy steel or the high alloy concentrations used in Maraging and PH stainless steels. Boron may also increase elongation and blunt crack propagation at grain boundaries and at the nickel intermetallic.
[00381 The titanium serves as a carbide former. Other carbide formers that can optionally be used are vanadium, niobium, zirconium, or a combination thereof.
[0039] The steel has less than about 6.5% titanium. Optionally, the steel can have more than about 0.10/0 and less than about 6.5% titanium, more than about 0.12% and less than about 6.5%
titanium, more than about 0.14% and less than about 6.5% titanium, or more than about 0.2%
and less than about 6.5% titanium. If more than 6.5% titanium is used, the steel may not properly form the desired crystalline structure and increases cost without a commensurate improvement in performance.
[0040] In one aspect of the invention, the iron in the steel is at least about 80% by weight.
[0041] In one aspect, less than about 5% of any combination of nickel, manganese, and copper is in the steel (alloy). Optionally, the alloy comprises less than about 0.5%, less than about 1%, less than about 1.5%, less than about 2%, less than about 2.5%, or less than about 3%, of any combination of nickel, manganese and copper. If more than about 5%
nickel, manganese, or copper, or combinations thereof, are used to form the steel sheet or plate, the costs unduly increase without a corresponding improvement in performance. Preferably, the steel sheet or plate has substantially no copper [0042] The boron percentage is important because if the range of about 0.0001% to about 0.01% is not used, the steel will not form martensite when quenched. If more than about 0.01% is used, the steel will be too brittle and can crack in use and it may even be difficult to get the steel out of the caster. The optimum boron range is about 0.002% to about 0.003%.
[0043] The steel alloy includes only small amounts of carbon; at least about 0.003% carbon, and up to about 0.1% carbon. Optionally, the steel comprises less than about 0.05%, less than about 0.04%, less than about 0.03%, less than about 0.02%, or less than about 0.01% carbon.
[0044] Optionally, the steel comprises at least about 0.025% aluminum.
Applicant believes the steel forms more intermetallics, thus making the steel stronger.
[0045] The present invention includes a method of making a high strength steel as shown in Figures IA and 1B. First, as shown in Figure 1A, the steel of the invention comprising iron and carbon is combined in, for example, a vessel (10) with titanium as a strong carbide former, and boron, and poured (20) from the vessel (10) into an ingot or a slab (30). The constituents can be combined in any order or any way so that the result is the combination. Then the combination is heated to a sufficiently high temperature, such as, for example, 1200 C, such that the steel transitions to an austenitic, face centered cubic lattice phase (30) and the titanium removes substantially all of the carbon from the crystal lattice by forming a metal carbide other than iron carbide. Depending on the application, a hot slab (30) can be rolled between rollers (40) to prepare a hot rolled coil or hot rolled plate (50), as shown in Figure 1B. The hot rolled coil or hot rolled plate (50) of alloy steel is quenched to a quench temperature with a quench faster than still air such that a body centered cubic lattice is formed by displacement, and ordered intermetallics are formed in the alloy steel. The hot rolled coil or the hot rolled plate (50) can be coiled (60) after it is rolled. A hot rolled coil or hot rolled plate (50) or coil (60) can be either maintained at temperature or heated to form additional ordered intermetallics. The invention also includes the steel made by the method.
[0046] In another aspect, the present invention is a method of making a steel sheet or plate formed of a martensitic steel alloy. The method comprises the steps of: a) heating the alloy steel to a sufficiently high temperature that the steel transitions to an austenitic, face centered cubic lattice phase and the titanium removes substantially all of the carbon from the crystal lattice by forming a metal carbide other than iron carbide; b) hot rolling the heated alloy steel of step (a);
and c) quenching the hot rolled steel of step (b) to a quench temperature with a quench faster than still air such that a body centered cubic lattice is formed by displacement.
[0047] In one aspect, the step of heating comprises heating to a temperature greater than 1000 degree C.
[0048] Optionally, the steel can be cold rolled. In this instance, the method comprises cold rolling the alloy steel to form the sheet or plate before the step of quenching.
100491 In one aspect, the quench temperature is from about 200 to about 750 degrees C.
[0050] In one aspect, after quenching, the rolled steel is heated to a reheat temperature of between 200 C and 750 C and maintaining it at the reheat temperature for more than one minute.
This improves the strength of the steel. In another aspect, the method comprises heating the alloy steel after quenching. In another aspect, the method comprises having the alloy steel at the quench temperature or higher for more than one minute after quenching.
In another aspect, the alloy comprises less than 0.02% carbon. In another aspect, the alloy comprises less than 0.01% carbon.
10008} In one aspect, the alloy comprises at least 0.025% aluminum.
100091 In one aspect, the steel sheet or plate can be cold rolled.
Optionally, the steel sheet or plate has been hot dip coated in zinc or an alloy containing zinc without substantially crystallizing the martensitic steel structure. Optionally, the steel sheet or plate can be formed by quenching off of a hot sheet or plate mill.
100101 After quenching, or after cold roll, the sheet can be reheated to a temperature of between 200 C and 750 C and maintained at that temperature for more than one minute.
[0011] In another aspect, the present invention is a method of making a steel sheet or plate formed of a martensitic steel alloy. The method comprises the steps of: a) heating the alloy steel to a sufficiently high temperature that the steel transitions to an austenitic, face centered cubic lattice phase and the titanium removes substantially all of the carbon from the crystal lattice by forming a metal carbide other than iron carbide; b) hot rolling the heated alloy steel of step (a);
and c) quenching the hot rolled steel of step (b) a quench temperature with a quench faster than still air such that a body centered cubic lattice is formed by displacement.
[0012] In one aspect, the method comprises cold rolling the alloy steel to form the sheet or plate before the step of quenching.
[0013] In one aspect, the quench temperature is from about 200 to about 750 degrees C.
[0014] In one aspect, the step of heating comprises heating to a temperature greater than 1000 degree C.
[0015] In one aspect, after quenching, the hot rolled steel is maintained at a temperature of greater than 200 degree C for a sufficient time to form order intermetallics.
[0016] In one aspect, after quenching, the rolled steel is heated to a reheat temperature of between 200 C and 750 C and maintaining it at the reheat temperature for more than one minute.
[0017] In one aspect, the method comprises the additional step of hot dip coating the rolled steel in zinc or an alloy containing zinc without substantially crystallizing the martensitic steel structure.
[0018] This invention has applications outside the automotive industry, and is useful wherever high strength, low cost steel is desirable.
DRAWINGS
[0019] The detailed description of some embodiments of the invention is made below with reference to the accompanying Figures 1A-1B.
[00201 Figure IA is a schematic of steps involved in a method of making steel according to the present invention; and 100211 Figure 1B is a schematic of steps involved in the method of making steel according to the present invention.
DESCRIPTION
100221 As used herein, the following terms and variations thereof have the meanings given below, unless a different meaning is clearly intended by the context in which such term is used.
100231 The terms "a," "an," and "the" and similar referents used herein are to be construed to cover both the singular and the plural unless their usage in context indicates otherwise.
100241 Definitions of chemical terms and general terms used throughout the specification are described in more detail herein, but unless otherwise indicated the chemical elements are identified in accordance with the Periodic Table of the Elements, CAS version, Handbook of Chemistry and Physics, 75th Ed., inside cover, or are terms that are well known to one of skill in the art.
100251 Percentages referred to herein are percentages by weight.
100261 As used in this disclosure, the term "comprises" and variations of the term, such as "comprising" and "comprises," are not intended to exclude other additives, components, ingredients or steps.
100271 As used herein, "dislocation" refers to a crystallographic defect or irregularity within a crystal structure of a material on an atomic scale. The presence of dislocations influences many of the properties of materials. Transmission electron microscopy (TEM) can be used to observe dislocations within the crystal structure of the material.
100281 Interstitial free steel is well known in the steel industry where the higher cost of these types of steels are acceptable due to the excellent forming properties and a lack of yield point elongation. These steels typically have low yield strength, high plastic strain ratio, high strain rate sensitivity and good formability. Interstitial free steels have interstitial free body centered cubic ferrite matrix. Carbon is kept very low and is stabilized, or removed, from the crystal lattice structure of the steel, normally with titanium, niobium or both. The disadvantage of these steels is the relatively low strength of the ferrite.
100291 Austenite steel has a face-centered cubic crystal structure. The carbon atoms lie in the interstices (holes) between the larger iron atoms. At slow cooling rates, the carbon moves ahead of the interface into the austenite iron by diffusion. Austenite steel may be strengthened by rapid cooling (quenching) by, for example, immersing the hot metal into liquid coolants such as water, oil, or liquid salts. Steels can also be quenched by air.
[0030] The term "martensitic steel alloy" is defined herein to be any steel or alloy steel that transitions from a face centered cubic lattice phase to a body centered cubic lattice phase predominantly by displacement and/or shear and not by substitution. When austenite is rapidly cooled, a martensite phase is formed. Martensite, tempered martensite and bainite are high strength steels that are well known in the steel industry where very high strength is required.
Bainite steel is within the definition of martensitic steel alloy.
[0031] In tempered martensite and bainite, the carbon migrates out of the lattice structure and forms a metal carbide. The disadvantage of these steels is the high carbon content required to form martensite. This causes a reduction in elongation and toughness with an inverse relationship to the increase in strength.
[0032] Additionally, Maraging and PH stainless steels are well known in the aerospace industry, where the higher cost of these types of steels are acceptable due to the excellent properties inherent in precipitating a nickel intermetallic. All current generation advanced high strength steels rely on carbon to some extent to add strength and/or facilitate other reactions.
Maraging and PH stainless steels rely on formation of a martensitic steel matrix and, with aging, precipitation of a nickel intermetallic with aluminum, molybdenum, titanium, niobium, tantalum or other metals known to those skilled in the art. A typical Maraging steel may be composed of 18% - 19% nickel, 8% - 10% cobalt, 3% - 5.5% molybdenum, 0.15% - 1.6% titanium and 0.5%
niobium, and after aging exceed 2,400 Ivfl'a yield and tensile strength. A
typical PH stainless steel may be composed of 15% chrome, 4% nickel, 3% copper, and 0.15% - 0.45%
of tantalum and niobium. Carbon is kept low. This family of alloys will form martensite upon slow heat of the metal to a solution treatment temperature, and then let the metal air cool to room temperature, which forms intermetallics. The disadvantage of these steels is the high alloy content required to form a martensite steel matrix with slow cooling rates. The high alloy content also increases cost beyond what a high-volume application can justify.
[0033] Thus, there is a need for high strength interstitial free or predominantly interstitial free steel that is capable of forming shear martensite without high alloy additions and without carbon in the crystal lattice structure.
[0034] This invention provides a material that contains low alloy additions that remove carbon from the high temperature face centered crystal lattice and enable an industry standard quench to transform the steel to an interstitial free martensite without a temper treatment. When higher strength is required, the material of the invention may be heated to a precipitation hardening temperature to form an additional ordered intermetallic. The martensitic steel of the invention has substantially all of the carbon removed from the crystal lattice of the austenite prior to forming martensite, forming an interstitial free martensite that is strengthened not with carbon/carbon iron but by pinning the dislocations with an intermetallic.
[0035] In particular, the present invention provides a new type of a steel sheet or plate formed of a martensitic steel alloy comprising: a) iron, at least some of the iron having dislocations; b) less than about 5% of any combination of nickel, manganese, and copper; c) from about 0.0001% to about 0.01% boron; d) from about 0.05% to about 6.5%
titanium; e) more than about 0.003% and less than about 0.1% carbon; and f) less than about 7%
of all other elements. "All other elements" means elements other than iron, nickel, manganese, copper, boron, titanium, and carbon.
[0036] The steel preferably has substantially no cementite, substantially no interstitial carbon, substantially no interstitial nitrogen, and substantially no copper.
The steel has titanium dispersed in the iron with the titanium clustered at the dislocations.
Optionally, the steel is substantially a martensitic structure with minor ferrite zones. The sheet or plate is typically formed by quenching off of a hot sheet or plate mill. The method of making the steel is discussed in more detail below.
[0037] Titanium and boron are very strong hardenability agents that are believed to work synergistically together to form martensite without the normal carbon additions that are used in plain carbon and alloy steel or the high alloy concentrations used in Maraging and PH stainless steels. Boron may also increase elongation and blunt crack propagation at grain boundaries and at the nickel intermetallic.
[00381 The titanium serves as a carbide former. Other carbide formers that can optionally be used are vanadium, niobium, zirconium, or a combination thereof.
[0039] The steel has less than about 6.5% titanium. Optionally, the steel can have more than about 0.10/0 and less than about 6.5% titanium, more than about 0.12% and less than about 6.5%
titanium, more than about 0.14% and less than about 6.5% titanium, or more than about 0.2%
and less than about 6.5% titanium. If more than 6.5% titanium is used, the steel may not properly form the desired crystalline structure and increases cost without a commensurate improvement in performance.
[0040] In one aspect of the invention, the iron in the steel is at least about 80% by weight.
[0041] In one aspect, less than about 5% of any combination of nickel, manganese, and copper is in the steel (alloy). Optionally, the alloy comprises less than about 0.5%, less than about 1%, less than about 1.5%, less than about 2%, less than about 2.5%, or less than about 3%, of any combination of nickel, manganese and copper. If more than about 5%
nickel, manganese, or copper, or combinations thereof, are used to form the steel sheet or plate, the costs unduly increase without a corresponding improvement in performance. Preferably, the steel sheet or plate has substantially no copper [0042] The boron percentage is important because if the range of about 0.0001% to about 0.01% is not used, the steel will not form martensite when quenched. If more than about 0.01% is used, the steel will be too brittle and can crack in use and it may even be difficult to get the steel out of the caster. The optimum boron range is about 0.002% to about 0.003%.
[0043] The steel alloy includes only small amounts of carbon; at least about 0.003% carbon, and up to about 0.1% carbon. Optionally, the steel comprises less than about 0.05%, less than about 0.04%, less than about 0.03%, less than about 0.02%, or less than about 0.01% carbon.
[0044] Optionally, the steel comprises at least about 0.025% aluminum.
Applicant believes the steel forms more intermetallics, thus making the steel stronger.
[0045] The present invention includes a method of making a high strength steel as shown in Figures IA and 1B. First, as shown in Figure 1A, the steel of the invention comprising iron and carbon is combined in, for example, a vessel (10) with titanium as a strong carbide former, and boron, and poured (20) from the vessel (10) into an ingot or a slab (30). The constituents can be combined in any order or any way so that the result is the combination. Then the combination is heated to a sufficiently high temperature, such as, for example, 1200 C, such that the steel transitions to an austenitic, face centered cubic lattice phase (30) and the titanium removes substantially all of the carbon from the crystal lattice by forming a metal carbide other than iron carbide. Depending on the application, a hot slab (30) can be rolled between rollers (40) to prepare a hot rolled coil or hot rolled plate (50), as shown in Figure 1B. The hot rolled coil or hot rolled plate (50) of alloy steel is quenched to a quench temperature with a quench faster than still air such that a body centered cubic lattice is formed by displacement, and ordered intermetallics are formed in the alloy steel. The hot rolled coil or the hot rolled plate (50) can be coiled (60) after it is rolled. A hot rolled coil or hot rolled plate (50) or coil (60) can be either maintained at temperature or heated to form additional ordered intermetallics. The invention also includes the steel made by the method.
[0046] In another aspect, the present invention is a method of making a steel sheet or plate formed of a martensitic steel alloy. The method comprises the steps of: a) heating the alloy steel to a sufficiently high temperature that the steel transitions to an austenitic, face centered cubic lattice phase and the titanium removes substantially all of the carbon from the crystal lattice by forming a metal carbide other than iron carbide; b) hot rolling the heated alloy steel of step (a);
and c) quenching the hot rolled steel of step (b) to a quench temperature with a quench faster than still air such that a body centered cubic lattice is formed by displacement.
[0047] In one aspect, the step of heating comprises heating to a temperature greater than 1000 degree C.
[0048] Optionally, the steel can be cold rolled. In this instance, the method comprises cold rolling the alloy steel to form the sheet or plate before the step of quenching.
100491 In one aspect, the quench temperature is from about 200 to about 750 degrees C.
[0050] In one aspect, after quenching, the rolled steel is heated to a reheat temperature of between 200 C and 750 C and maintaining it at the reheat temperature for more than one minute.
This improves the strength of the steel. In another aspect, the method comprises heating the alloy steel after quenching. In another aspect, the method comprises having the alloy steel at the quench temperature or higher for more than one minute after quenching.
8 [0051] When being quenched, the temperature has to start above the austenite transition temperature. After the quench, the steel goes from the face centered cubic lattice to the body centered cubic lattice. "Hot" as used in the claims means substantially all face centered cubic lattice; going from face centered cubic lattice to body centered cubic lattice.
[0052] In one aspect, after quenching, the hot rolled steel is maintained at a temperature of greater than 200 degree C for a sufficient time to form order intermetallics.
[0053] Formation of ordered intermetallics in the alloy steel according to the present invention can be done in several ways. The first way is to keep the alloy steel at the same temperature as the temperature in which it was quenched. The second way is to raise the alloy steel above the temperature in which it was quenched. The third way is, after the quench, to allow the alloy steel to cool down, such as with, for example, air cooling, and then reheat, where the reheat temperature is more or less than the quench temperature.
[0054] Optionally, the steel has been hot dip coated in zinc or an alloy containing zinc without substantially recrystallizing the martensitic steel structure. In this instance, the method comprises the additional step of hot dip coating the rolled steel in zinc or an alloy containing zinc without substantially crystallizing the martensitic steel structure.
[0055] In one example, a low carbon alloy steel was made with 1.72% nickel, 0.38%
titanium, 0.03% aluminum, 0.0022% boron, 0.021% carbon and 0.34% manganese.
The steel was made by reheating the ingots to 1200 C, soaking in air for 1 hour per 25 mm of thickness, and then hot rolled with a finish rolling temperature of between 900 C and 955 C.
[0056] After quenching from about 900 C in water, the low carbon alloy steel of the invention formed an interstitial free martensite structure with a very high dislocation density.
This steel is very tough, plastic or viscous-like compared to typical high carbon steels. Typical properties of the steel are:
Tensile Yield Total Elongation (TE) 820 MPa 680 MPa 12%
[0057] After cold rolling and aging at 510 C for three hours, the nickel and titanium
[0052] In one aspect, after quenching, the hot rolled steel is maintained at a temperature of greater than 200 degree C for a sufficient time to form order intermetallics.
[0053] Formation of ordered intermetallics in the alloy steel according to the present invention can be done in several ways. The first way is to keep the alloy steel at the same temperature as the temperature in which it was quenched. The second way is to raise the alloy steel above the temperature in which it was quenched. The third way is, after the quench, to allow the alloy steel to cool down, such as with, for example, air cooling, and then reheat, where the reheat temperature is more or less than the quench temperature.
[0054] Optionally, the steel has been hot dip coated in zinc or an alloy containing zinc without substantially recrystallizing the martensitic steel structure. In this instance, the method comprises the additional step of hot dip coating the rolled steel in zinc or an alloy containing zinc without substantially crystallizing the martensitic steel structure.
[0055] In one example, a low carbon alloy steel was made with 1.72% nickel, 0.38%
titanium, 0.03% aluminum, 0.0022% boron, 0.021% carbon and 0.34% manganese.
The steel was made by reheating the ingots to 1200 C, soaking in air for 1 hour per 25 mm of thickness, and then hot rolled with a finish rolling temperature of between 900 C and 955 C.
[0056] After quenching from about 900 C in water, the low carbon alloy steel of the invention formed an interstitial free martensite structure with a very high dislocation density.
This steel is very tough, plastic or viscous-like compared to typical high carbon steels. Typical properties of the steel are:
Tensile Yield Total Elongation (TE) 820 MPa 680 MPa 12%
[0057] After cold rolling and aging at 510 C for three hours, the nickel and titanium
9 combined to form very hard, nanometer sized reinforcing rod-like structures with an average diameter of about 4 nm and length of about 15 nm that pin the dislocations and increase the strength of the steel. The titanium also formed additional intermetallic structures with the iron.
Typical properties of the steel are:
Tensile Yield TE
990 MPa 980 MPa 7%
[0058] The strength, ductility and fracture toughness of the steel can be directly altered as required by the final application by reducing or increasing the amount of each of carbon, nickel, titanium, manganese, and other elements known to one of skill in the art, and changing the time and temperature of the heat treatment(s). The mechanical properties of the steel can also be altered by the order in which they are added to the steel.
[0059] In another example of the invention, an intermediate strength alloy steel was formed with manganese replacing nickel. For this, the material was made up of 1.48%
manganese, 0.32% titanium, 0.033% aluminum, 0.0023% boron, 0.039% carbon with the balance iron and normal production and tramp elements.
[0060] In this example, the steel of the invention was made by reheating the ingots to 1200 C, soaking for 1 hour per 25 mm of thickness, and then hot rolled with a finish rolling temperature of between 900 C and 955 C. The hot rolled coil was then quenched from about 900 C in water to about 500 C. The hot rolled coil was then reheated to 500 C
and held for 24 hours to simulate a production hot rolling sequence. Average properties of the steel are:
Tensile Yield TE
854 MPa 765 MPa 16%
100611 Other combinations of carbon, nickel, titanium, manganese, intermetallic forming metals and martensite stabilization elements may be used by those skilled in the art.
[0062] In another example, steel was made with 0.003% carbon, 0.3%
manganese, 0.12%
titanium, and 0.002% boron. The steel was quenched to 200 C.
Tensile Yield TE
367 MPa 212 MPa 36%
100631 In another example, steel was made with 0.15% carbon, 0.3%
manganese, 0.14%
titanium, and 0.002% boron. The steel was quenched to 200 C.
Tensile Yield TE
602 MPa 502 MPa 15%
[0064] In these last two examples, it is demonstrated that more than 0.003%
carbon is needed. The system does not work at this carbon level.
[0065] In another example, steel was made with 0.35 A carbon, 0.55%
manganese, 0.16%
titanium, and less than 0.0001% boron. The steel was quenched to 550 C.
Tensile Yield TE
444 MPa 383 MPa 30%
[0066] In another example, steel was made with 0.035% carbon, 0.55%
manganese, 0.16%
titanium, and 0.003% boron. The steel was quenched to 550 C.
Tensile Yield TE
684 MPa 593 IVTa 14%
[0067] In these last two examples, it is demonstrated that the system only works if boron is present. A key feature is the combination of titanium and boron. The low amounts of nickel, manganese and copper distinguish the invention form a conventional maraging steel. The top limitation(s) on the carbon are to ensure the present invention is not a quenched martensitic low carbon steel. Although the present invention has been described in considerable detail with reference to certain preferred embodiments, other embodiments are possible.
The steps disclosed for the present methods, for example, are not intended to be limiting nor are they intended to indicate that each step is necessarily essential to the method, but instead are exemplary steps only. Therefore, the scope of the appended claims should not be limited to the description of preferred embodiments contained in this disclosure.
Typical properties of the steel are:
Tensile Yield TE
990 MPa 980 MPa 7%
[0058] The strength, ductility and fracture toughness of the steel can be directly altered as required by the final application by reducing or increasing the amount of each of carbon, nickel, titanium, manganese, and other elements known to one of skill in the art, and changing the time and temperature of the heat treatment(s). The mechanical properties of the steel can also be altered by the order in which they are added to the steel.
[0059] In another example of the invention, an intermediate strength alloy steel was formed with manganese replacing nickel. For this, the material was made up of 1.48%
manganese, 0.32% titanium, 0.033% aluminum, 0.0023% boron, 0.039% carbon with the balance iron and normal production and tramp elements.
[0060] In this example, the steel of the invention was made by reheating the ingots to 1200 C, soaking for 1 hour per 25 mm of thickness, and then hot rolled with a finish rolling temperature of between 900 C and 955 C. The hot rolled coil was then quenched from about 900 C in water to about 500 C. The hot rolled coil was then reheated to 500 C
and held for 24 hours to simulate a production hot rolling sequence. Average properties of the steel are:
Tensile Yield TE
854 MPa 765 MPa 16%
100611 Other combinations of carbon, nickel, titanium, manganese, intermetallic forming metals and martensite stabilization elements may be used by those skilled in the art.
[0062] In another example, steel was made with 0.003% carbon, 0.3%
manganese, 0.12%
titanium, and 0.002% boron. The steel was quenched to 200 C.
Tensile Yield TE
367 MPa 212 MPa 36%
100631 In another example, steel was made with 0.15% carbon, 0.3%
manganese, 0.14%
titanium, and 0.002% boron. The steel was quenched to 200 C.
Tensile Yield TE
602 MPa 502 MPa 15%
[0064] In these last two examples, it is demonstrated that more than 0.003%
carbon is needed. The system does not work at this carbon level.
[0065] In another example, steel was made with 0.35 A carbon, 0.55%
manganese, 0.16%
titanium, and less than 0.0001% boron. The steel was quenched to 550 C.
Tensile Yield TE
444 MPa 383 MPa 30%
[0066] In another example, steel was made with 0.035% carbon, 0.55%
manganese, 0.16%
titanium, and 0.003% boron. The steel was quenched to 550 C.
Tensile Yield TE
684 MPa 593 IVTa 14%
[0067] In these last two examples, it is demonstrated that the system only works if boron is present. A key feature is the combination of titanium and boron. The low amounts of nickel, manganese and copper distinguish the invention form a conventional maraging steel. The top limitation(s) on the carbon are to ensure the present invention is not a quenched martensitic low carbon steel. Although the present invention has been described in considerable detail with reference to certain preferred embodiments, other embodiments are possible.
The steps disclosed for the present methods, for example, are not intended to be limiting nor are they intended to indicate that each step is necessarily essential to the method, but instead are exemplary steps only. Therefore, the scope of the appended claims should not be limited to the description of preferred embodiments contained in this disclosure.
Claims (33)
1. A steel sheet or plate formed of a martensitic steel alloy comprising:
a) iron, at least some of the iron having dislocations;
b) less than 5% of any combination of nickel, manganese, and copper;
c) from about 0.0001 to about 0.01% boron;
d) from about 0.05% to about 6.5 % titanium;
e) more than 0.003% and less than 0.1% carbon; and f) less than 7% of all other elements.
a) iron, at least some of the iron having dislocations;
b) less than 5% of any combination of nickel, manganese, and copper;
c) from about 0.0001 to about 0.01% boron;
d) from about 0.05% to about 6.5 % titanium;
e) more than 0.003% and less than 0.1% carbon; and f) less than 7% of all other elements.
2. The steel sheet or plate of claim 1 wherein the alloy comprises more than 0.1% titanium.
3. The steel sheet or plate of claim 1 wherein the alloy comprises more than 0.12% titanium.
4. The steel sheet or plate of claim 1 wherein the alloy comprises more than 0.14% titanium.
5. The steel sheet or plate of claim 1 wherein the alloy comprises more than 0.2% titanium.
6. The steel sheet or plate of claim 1 wherein the alloy comprises less than 0.5% of any combination of nickel, manganese, and copper.
7. The steel sheet or plate of claim 1 wherein the alloy comprises less than 1% of any combination of nickel, manganese, and copper.
8. The steel sheet or plate of claim 1 wherein the alloy comprises less than 1.5% of any combination of nickel, manganese, and copper.
9. The steel sheet or plate of claim 1 wherein the alloy comprises less than 2% of any combination of nickel, manganese, and copper.
10. The steel sheet or plate of claim 1 wherein the alloy comprises less than 2.5% of any combination of nickel, manganese, and copper.
11. The steel sheet or plate of claim 1 wherein the alloy comprises less than 3% of any combination of nickel, manganese, and copper.
12. The steel sheet or plate of claim 1 wherein the alloy comprises less than 0.05% carbon.
13. The steel sheet or plate of claim 1 wherein the alloy comprises less than 0.04% carbon.
14. The steel sheet or plate of claim 1 wherein the alloy comprises less than 0.03% carbon.
15. The steel sheet or plate of claim 1 wherein the alloy comprises less than 0.02% carbon.
16. The steel sheet or plate of claim 1 wherein the alloy comprises less than 0.01% carbon.
17. The steel sheet or plate of claim 1, wherein the alloy comprises at least 0.025% aluminum.
18. The steel sheet or plate of claim 1 that has been cold rolled.
19. The steel sheet or plate of claim 1, after quenching, that has been reheated to a temperature of between 200 C and 750 C and maintained at that temperature for more than one minute.
20. The steel sheet or plate of claim 1, wherein the alloy is substantially a martensitic structure with minor ferrite zones.
21. The steel sheet or plate of claim 18 that has been hot dip coated in zinc or an alloy containing zinc without substantially crystallizing the martensitic steel structure.
22. The steel sheet or plate of claim 1, wherein the alloy comprises substantially no copper.
23. The steel sheet or plate of claim 1, wherein the alloy has substantially no cementite.
24. A steel sheet or plate formed of a martensitic steel alloy comprising:
a) iron, at least some of the iron having dislocations;
b) less than 5% of any combination of nickel, manganese, and copper;
c) from about 0.0001 to about 0.01% boron;
d) from about 0.05% to about 6.5 % titanium;
e) more than 0.003% and less than 0.1% carbon; and f) less than 7% of all other elements;
wherein the sheet or plate has been formed by quenching off of a hot sheet or plate mill.
a) iron, at least some of the iron having dislocations;
b) less than 5% of any combination of nickel, manganese, and copper;
c) from about 0.0001 to about 0.01% boron;
d) from about 0.05% to about 6.5 % titanium;
e) more than 0.003% and less than 0.1% carbon; and f) less than 7% of all other elements;
wherein the sheet or plate has been formed by quenching off of a hot sheet or plate mill.
25. The steel sheet or plate of claim 1, wherein the titanium has clustered at the dislocations.
26. A method of making a steel sheet or plate formed of a martensitic steel alloy, the method comprising the steps of:
a) heating the alloy steel defined in claim 1 to a sufficiently high temperature that the steel transitions to an austenitic, face centered cubic lattice phase and the titanium removes substantially all of the carbon from the crystal lattice by forming a metal carbide other than iron carbide;
b) hot rolling the heated alloy steel of step (a); and c) quenching the hot rolled steel of step (b) to a quench temperature with a quench faster than still air such that a body centered cubic lattice is formed by displacement.
a) heating the alloy steel defined in claim 1 to a sufficiently high temperature that the steel transitions to an austenitic, face centered cubic lattice phase and the titanium removes substantially all of the carbon from the crystal lattice by forming a metal carbide other than iron carbide;
b) hot rolling the heated alloy steel of step (a); and c) quenching the hot rolled steel of step (b) to a quench temperature with a quench faster than still air such that a body centered cubic lattice is formed by displacement.
27. The method of claim 26 comprising cold rolling the alloy steel to form the sheet or plate before the step of quenching.
28. The method of claim 26 wherein the quench temperature is from about 200 to about 750 degrees C.
29. The method of claim 26 wherein the step of heating comprises heating to a temperature greater than 1000 degree C.
30. The method of claim 26 wherein after quenching the hot rolled steel is maintained at a temperature of greater than 200 degree C for a sufficient time to form order intermetallics.
31. The method of claim 26 wherein, after quenching, heating the rolled steel to a reheat temperature of between 200 C and 750 C and maintaining it at the reheat temperature for more than one minute.
32. The method of claim 26 comprising the additional step of hot dip coating the rolled steel in zinc or an alloy containing zinc without substantially crystallizing the martensitic steel structure.
33. The steel sheet or plate of claim 24 that has been hot dip coated in zinc or an alloy containing zinc without substantially crystallizing the martensitic steel structure.
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US15/989,705 | 2018-05-25 | ||
US15/989,705 US20190017155A1 (en) | 2017-06-08 | 2018-05-25 | Impact resistant high strength steel |
PCT/US2018/036332 WO2018226879A1 (en) | 2017-06-08 | 2018-06-06 | Impact resistant high strength steel |
USPCT/US2018/036332 | 2018-06-06 | ||
PCT/US2018/064451 WO2019226197A1 (en) | 2018-05-25 | 2018-12-07 | Impact resistant high strength steel |
Publications (1)
Publication Number | Publication Date |
---|---|
CA3066726A1 true CA3066726A1 (en) | 2019-11-28 |
Family
ID=68615913
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA3066726A Abandoned CA3066726A1 (en) | 2018-05-25 | 2018-12-07 | Impact resistant high strength steel |
Country Status (2)
Country | Link |
---|---|
CA (1) | CA3066726A1 (en) |
WO (1) | WO2019226197A1 (en) |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7235212B2 (en) * | 2001-02-09 | 2007-06-26 | Ques Tek Innovations, Llc | Nanocarbide precipitation strengthened ultrahigh strength, corrosion resistant, structural steels and method of making said steels |
JP5744575B2 (en) * | 2010-03-29 | 2015-07-08 | 新日鐵住金ステンレス株式会社 | Double phase stainless steel sheet and strip, manufacturing method |
DE102010025287A1 (en) * | 2010-06-28 | 2012-01-26 | Stahlwerk Ergste Westig Gmbh | Chromium-nickel steel |
WO2012153009A1 (en) * | 2011-05-12 | 2012-11-15 | Arcelormittal Investigación Y Desarrollo Sl | Method for the production of very-high-strength martensitic steel and sheet thus obtained |
US10196726B2 (en) * | 2013-02-26 | 2019-02-05 | Nippon Steel & Sumitomo Metal Corporation | High-strength hot-rolled steel sheet having excellent baking hardenability and low temperature toughness with maximum tensile strength of 980 MPa or more |
JP6369537B2 (en) * | 2014-04-23 | 2018-08-08 | 新日鐵住金株式会社 | Hot-rolled steel sheet for tailored rolled blanks, tailored rolled blanks, and production methods thereof |
-
2018
- 2018-12-07 WO PCT/US2018/064451 patent/WO2019226197A1/en active Application Filing
- 2018-12-07 CA CA3066726A patent/CA3066726A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
WO2019226197A1 (en) | 2019-11-28 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US5545269A (en) | Method for producing ultra high strength, secondary hardening steels with superior toughness and weldability | |
KR930010321B1 (en) | Metallic material having ultra-fine grain structure and method for its manufacture | |
KR100543956B1 (en) | Steel plate excellent in shape freezing property and method for production thereof | |
US4578124A (en) | High strength low carbon steels, steel articles thereof and method for manufacturing the steels | |
KR101747052B1 (en) | High-carbon hot-rolled steel sheet and method for manufacturing the same | |
CA3135015A1 (en) | Steel sheet having excellent toughness, ductility and strength, and manufacturing method thereof | |
WO1999002747A1 (en) | Ultra high strength, secondary hardening steels with superior toughness and weldability | |
KR102493548B1 (en) | Cold-rolled and heat-treated steel sheet and its manufacturing method | |
JP5339765B2 (en) | High strength hot rolled steel sheet and method for producing the same | |
JP2005336526A (en) | High strength steel sheet having excellent workability and its production method | |
US11401569B2 (en) | High-strength cold-rolled steel sheet and method for manufacturing same | |
CA2996198A1 (en) | Corrosion and cracking resistant high manganese austenitic steels containing passivating elements | |
JP4109619B2 (en) | High strength steel plate with excellent elongation and stretch flangeability | |
KR101892526B1 (en) | High-carbon hot-rolled steel sheet and method for manufacturing the same | |
KR20160010579A (en) | High-carbon hot-rolled steel sheet and production method for same | |
JP6972153B2 (en) | Hot-rolled bainite steel products with a tensile strength of at least 1100 MPa and a total elongation of 18% or more. | |
EP2641989A2 (en) | High-toughness cold-drawn non-heat-treated wire rod, and method for manufacturing same | |
JP7211554B2 (en) | Steel suitable for use in sour environments | |
JP7442645B2 (en) | High-strength steel plate with excellent workability and its manufacturing method | |
EP3748030A1 (en) | High-carbon hot-rolled steel sheet and method for manufacturing same | |
JP4697844B2 (en) | Manufacturing method of steel material having fine structure | |
EP3395988B1 (en) | High-strength structural steel sheet excellent in hot resistance and manufacturing method thereof | |
EP2527481B1 (en) | Quenched steel sheet having excellent hot press formability, and method for manufacturing same | |
KR20210014055A (en) | High strength steel sheet and manufacturing method thereof | |
US20210095362A1 (en) | Impact resistant high strength steel |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
FZDE | Discontinued |
Effective date: 20230607 |