US20150267282A1 - Steel alloy for a low-alloy high-strength steel - Google Patents
Steel alloy for a low-alloy high-strength steel Download PDFInfo
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- US20150267282A1 US20150267282A1 US14/428,286 US201314428286A US2015267282A1 US 20150267282 A1 US20150267282 A1 US 20150267282A1 US 201314428286 A US201314428286 A US 201314428286A US 2015267282 A1 US2015267282 A1 US 2015267282A1
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- 229910000831 Steel Inorganic materials 0.000 title claims abstract description 41
- 239000010959 steel Substances 0.000 title claims abstract description 41
- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 19
- 239000000956 alloy Substances 0.000 title claims abstract description 19
- 229910000851 Alloy steel Inorganic materials 0.000 title claims description 22
- 230000015572 biosynthetic process Effects 0.000 claims abstract description 18
- 229910052750 molybdenum Inorganic materials 0.000 claims abstract description 11
- 238000001556 precipitation Methods 0.000 claims abstract description 11
- 229910052758 niobium Inorganic materials 0.000 claims abstract description 10
- 239000000203 mixture Substances 0.000 claims abstract description 9
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 9
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 8
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 8
- 229910001567 cementite Inorganic materials 0.000 claims abstract description 7
- KSOKAHYVTMZFBJ-UHFFFAOYSA-N iron;methane Chemical compound C.[Fe].[Fe].[Fe] KSOKAHYVTMZFBJ-UHFFFAOYSA-N 0.000 claims abstract description 7
- 229910052720 vanadium Inorganic materials 0.000 claims abstract description 6
- 229910052721 tungsten Inorganic materials 0.000 claims abstract description 5
- 229910052742 iron Inorganic materials 0.000 claims abstract description 4
- 229910052726 zirconium Inorganic materials 0.000 claims abstract description 4
- 239000000126 substance Substances 0.000 claims abstract description 3
- 229910001566 austenite Inorganic materials 0.000 claims description 31
- 229910052782 aluminium Inorganic materials 0.000 claims description 30
- 230000009466 transformation Effects 0.000 claims description 25
- 239000000463 material Substances 0.000 claims description 19
- 238000001816 cooling Methods 0.000 claims description 18
- 229910000734 martensite Inorganic materials 0.000 claims description 17
- 229910001563 bainite Inorganic materials 0.000 claims description 15
- 229910052799 carbon Inorganic materials 0.000 claims description 13
- 229910052757 nitrogen Inorganic materials 0.000 claims description 13
- 229910052804 chromium Inorganic materials 0.000 claims description 9
- 238000010276 construction Methods 0.000 claims description 8
- 229910052748 manganese Inorganic materials 0.000 claims description 8
- 229910052710 silicon Inorganic materials 0.000 claims description 6
- 241000446313 Lamella Species 0.000 claims description 3
- 238000004519 manufacturing process Methods 0.000 claims description 2
- 229910052751 metal Inorganic materials 0.000 claims 1
- 239000002184 metal Substances 0.000 claims 1
- 150000002739 metals Chemical class 0.000 claims 1
- 230000006641 stabilisation Effects 0.000 claims 1
- 238000011105 stabilization Methods 0.000 claims 1
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 20
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 19
- 239000010955 niobium Substances 0.000 description 13
- 238000007792 addition Methods 0.000 description 12
- 239000011651 chromium Substances 0.000 description 11
- 239000011572 manganese Substances 0.000 description 11
- 229910000859 α-Fe Inorganic materials 0.000 description 10
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 8
- 230000000694 effects Effects 0.000 description 8
- 229920001296 polysiloxane Polymers 0.000 description 8
- 238000012360 testing method Methods 0.000 description 8
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 7
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 7
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 6
- 238000005275 alloying Methods 0.000 description 6
- 239000010936 titanium Substances 0.000 description 6
- 230000002411 adverse Effects 0.000 description 5
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 4
- -1 aluminum nitrides Chemical class 0.000 description 4
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 3
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 3
- 238000002441 X-ray diffraction Methods 0.000 description 3
- 230000002939 deleterious effect Effects 0.000 description 3
- 150000001247 metal acetylides Chemical class 0.000 description 3
- 239000011733 molybdenum Substances 0.000 description 3
- 229910001568 polygonal ferrite Inorganic materials 0.000 description 3
- 230000000087 stabilizing effect Effects 0.000 description 3
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 3
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 2
- 229910052796 boron Inorganic materials 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 229910052746 lanthanum Inorganic materials 0.000 description 2
- 239000002244 precipitate Substances 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 229910052702 rhenium Inorganic materials 0.000 description 2
- 229910052706 scandium Inorganic materials 0.000 description 2
- 238000004626 scanning electron microscopy Methods 0.000 description 2
- 230000001629 suppression Effects 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 238000003723 Smelting Methods 0.000 description 1
- 238000002083 X-ray spectrum Methods 0.000 description 1
- VDSREIHVGSWINN-UHFFFAOYSA-N [V].[Mo].[Ni] Chemical compound [V].[Mo].[Ni] VDSREIHVGSWINN-UHFFFAOYSA-N 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000009172 bursting Effects 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
- 238000011109 contamination Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000001934 delay Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000001493 electron microscopy Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000000411 inducer Substances 0.000 description 1
- 230000003993 interaction Effects 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
- 239000000155 melt Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 235000019362 perlite Nutrition 0.000 description 1
- 239000010451 perlite Substances 0.000 description 1
- 239000004848 polyfunctional curative Substances 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 238000005070 sampling Methods 0.000 description 1
- 239000011265 semifinished product Substances 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 238000005482 strain hardening Methods 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
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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
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/58—Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of 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
- C22C38/18—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
-
- 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
- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
-
- 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
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
-
- 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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/22—Ferrous alloys, e.g. steel alloys containing chromium with molybdenum or tungsten
-
- 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
- C22C38/26—Ferrous alloys, e.g. steel alloys containing chromium with niobium or tantalum
-
- 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
- C22C38/34—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of silicon
-
- 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
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/48—Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum
-
- 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
-
- 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
- C21D2211/002—Bainite
Definitions
- the invention relates to a steel alloy for a low alloy high strength steel which at the same time is tenacious and has excellent wear resistance according to patent claim 1 .
- the invention relates to pipes, strips and sheets made of this alloy, from which for example components for the automobile industry such as vehicle bodies, components of support structures or airbag tubes and cylinder tubes are produced.
- wear plates made of this alloy can for example be used in case of high wear requirements for excavator shovels.
- Such steels are also used for applications where sudden impact energies have to be absorbed, for example as bullet proof armor.
- Pipes produced from this alloy can be configured as welded pipes that are produced from hot or cold strip or in a seamlessly, and which depending on the case can have a cross section which deviates from the circular shape.
- Construction pipes or plates made of this alloy can also be used for welded steel constructions that are exposed to particularly high stress for example in crane construction, bridge construction, hoist construction and heavy-duty vehicle construction.
- Characteristic for these steels is for example a strength of 1000 to about 2000 MPa, an elongation at brake of at least 5% depending on the strength and an extremely fine (nano) structured bainitic microstructure with portions of residual austenite.
- the approach for generating this ultra-fine microstructure is based on the phase transformation at low temperatures in the bainite region while avoiding the precipitation of cementite and formation of martensite. Suppression of carbides that precipitate in the bainite such as cementite is necessary because on one hand, these have a strong embrittling effect as possible fracture inducers thereby preventing achieving the required tenacity, and on the other hand, the proportions of stabilized austenite, which are necessary for achieving the properties according to the invention, cannot be established.
- Carbide-free bainitic steels for rail tracks are for example known from DE 696 31 953 T2. Beside manganese, chromium and further elements such as molybdenum nickel vanadium wolfram titanium and boron, the steel alloy disclosed there has a silicon content between 1 and 3%.
- This steel is configured for the demands on rail tracks that are exposed to strong wear stress, however it cannot be used or is uneconomical for strips, sheets and pipes for the mentioned field of application because in these cases beside the demands on wear resistance, the strength and tenacity requirements also have to be met.
- the cross sectional dimensions of rails significantly differ from those of strips, sheets and pipes which requires adjustment of the alloying concept with regard to the material properties to be achieved after air cooling of the steel.
- a disadvantage of the known steel is also the expensive addition of titanium and other alloy elements such as nickel, molybdenum and wolfram.
- a further problem in the known steels is that no information regarding the nitrogen content are given which adversely affects material properties in particular through formation of aluminum nitrides when aluminum is added.
- Object of the invention is to set forth a steel alloy for a low alloy, high-strength carbide-free bainitic steel which is tenacious and wear resistant for producing strips, sheets and pipes, which on one hand is more cost effective than the known steel alloys and on the other hand ensures uniform material properties which meet the demands such as strength, elongation at break, tenacity etc. In addition, these material properties are also to be achieved when cooling at stationary air by air hardening.
- rare earths and reactive elements such as Ce, Hf, La, Re, Sc and/or Y of a ⁇ overall up to 1 weight % can be added.
- steels according to the invention have already after cooling at air a strength (R m ) of over 1250 MPa, an elongation at break of over 12% and a tenacity (KBZ) at ⁇ 20° C. of at least 15 J (cf. Table 1).
- the microstructure consists of carbide-free bainite and residual austenite with a proportion of at least 75% bainitic ferrite, at least 10% residual austenite and up to maximally 5% martensite (or martensite phase and/or decomposed austenite).
- the steel alloy according to the invention is based on the development of the carbide-free bainitic steel form DE 6906 953 T2 and WO 2009/075494 A1.
- Tests that were carried out in the context of the present invention have surprisingly shown that compared to known steel alloys for achieving the demanded material properties already can be achieved by an air hardening by targeted addition of aluminum in the range of 0.05 to 3.0 weight % and niobium in the range of 0.001 to 0.5 weight % beside an excellent material strength and wear resistance, very good tenacity can be achieved.
- the addition of niobium results in a significant improvement of the tenacity properties through grain refinement, so that this alloy meets the high requirements regarding mechanical properties and wear resistance.
- the kinetic of the ferrite formation can be decisively controlled so that the formation of coarse polygonal ferrite bodies, which can adversely affect the material properties, can be effectively avoided.
- Important in this regard is the interaction between aluminum and chromium. While aluminum accelerates the ferritic and bainitic transformation, addition of chromium delays the ferritic transformation (cf. FIG. 2 ). Targeted combination of these two elements, allows controlling the kinetic of the ferrite and bainite formation.
- FIG. 2 The influence of different alloying elements on the kinetic of the transformation is shown in FIG. 2 .
- the effects of C, Si, Al, Mn, Cr and Mo on the transformation kinetic of ferrite, perlite and bainite and on the martensite start temperature are shown schematically.
- the nitrogen content does not exceed the stated upper limit of 0.025%, better 0.015% or optimally 0.010 weight % in order to minimize the number and size of the deleterious aluminum nitrides as primary precipitations in the steel, wherein in addition the condition Al ⁇ N ⁇ 5 ⁇ 10 ⁇ 3 has to be satisfied. Otherwise, a minimal content of nitrogen of 0.001 weight %, optimally 0.0020 is required in order to enable a required niobium carbonitride formation for increasing tenacity by grain refinement.
- the tested alloy compositions and the determined mechanical characteristics are shown in Table 1. All samples where heated to about 950° C. and then cooled at stationary air or subjected to accelerated cooling. The required cooling speed is selected depending on the sheet thickness and the composition. As the results of the mechanical sampling show, the demanded properties could not be achieved with the sample melt 14 due to the too low Cr content. The test melt 16 satisfied the demands due to the greater sheet thickness of 12 mm only after accelerated cooling. Typical temperature profiles for the cooling at stationary air or with quenching are shown in FIG. 3 .
- FIG. 4 some of the tested test melts and their mechanical characteristics and cooling conditions are shown in comparison to the conventional and high strength steel materials. It can be seen that in the developed steel the region of higher strength materials at improved stretch properties.
- TRIP-effect With corresponding proportions of residual austenite a so called TRIP-effect can then also be advantageously used.
- Steels which usually are referred to by the term TRIP (“Transformation Induced Plasticity”) are steels which at the same time have a very high strength and a high ductility, which makes them especially suited for cold forming. These properties are obtained owing to their special microscopic structure, wherein the deformation-induced martensite formation and the work hardening associated therewith is inhibited and the ductility is increased.
- the effect of the TRIP effect is optimal for a residual austenite proportion of about 1 to 20%.
- the following conditions should be adhered to for achieving the demanded material properties in particular of the mechanical technological properties for the transformation kinetic and the transformation behavior ( FIG. 2 ) the stabilizing of the residual austenite and the martensite start temperature while taking the cooling rate into account wherein in the mentioned empirically determined formulas the contents of C, Mn, Si, Al, Cr and Mo in weight % and T as cooling rate in ° C./s have to be inserted.
- the units of the coefficients that are used in the formula are to be selected according to the variables used in the formula.
- the martensite start temperature has to be determined as follows:
- the microstructure of the steel according to the invention consist of ferrite and residual austenite lamellae. It can have proportions of martensite of up to 5% (or martensite/austenite phase and/or decomposed austenite).
- the two most important characteristics of the microstructure which significantly influence the mechanical properties of the steel are the lamella spacing and the proportion of residual austenite. The smaller the lamellar interspacing and the higher the proportion of residual austenite the higher are the strength and elongation at break of the material.
- the average lamellar interspacing should be smaller than 750 nm, advantageously smaller than 500 nm.
- the average previous austenite grain size should not exceed a value of 100 ⁇ m.
- the microstructure is very fine, the components of the microstructure can hardly be distinguished from each other microscopically so that depending on the case a combination of electron microscopy and x-ray diffraction has to be used.
- the components of the microstructure can be distinguished by means of scanning electron microscopy. In this way, an average lamellar interspacing of about 300 nm was determined.
- the result of an x-ray diffraction measurement is shown in FIG. 7 .
- the crystal structure of the present microstructure components and their phase proportions can be determined.
- Residual austenite proportions between 10% and 20% were determined using the x-ray diffraction method.
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- Mechanical Engineering (AREA)
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- Organic Chemistry (AREA)
- Heat Treatment Of Steel (AREA)
- Heat Treatment Of Sheet Steel (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102012018833.1 | 2012-09-14 | ||
| DE102012018833 | 2012-09-14 | ||
| PCT/DE2013/000519 WO2014040585A1 (de) | 2012-09-14 | 2013-08-28 | Stahllegierung für einen niedrig legierten, hochfesten stahl |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/DE2013/000519 A-371-Of-International WO2014040585A1 (de) | 2012-09-14 | 2013-08-28 | Stahllegierung für einen niedrig legierten, hochfesten stahl |
Related Child Applications (1)
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| US15/898,890 Continuation US20200131608A1 (en) | 2012-09-14 | 2018-02-19 | Method of determining a composition of a steel alloy for use in a low-alloy high-strength steel |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20150267282A1 true US20150267282A1 (en) | 2015-09-24 |
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| US15/898,890 Abandoned US20200131608A1 (en) | 2012-09-14 | 2018-02-19 | Method of determining a composition of a steel alloy for use in a low-alloy high-strength steel |
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Country Status (21)
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| US (2) | US20150267282A1 (enExample) |
| EP (1) | EP2895635B1 (enExample) |
| JP (1) | JP6513568B2 (enExample) |
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| AR (1) | AR092556A1 (enExample) |
| AU (2) | AU2013314787A1 (enExample) |
| BR (1) | BR112015005216A2 (enExample) |
| CA (1) | CA2881686A1 (enExample) |
| CL (1) | CL2015000634A1 (enExample) |
| DK (1) | DK2895635T3 (enExample) |
| ES (1) | ES2729562T3 (enExample) |
| MX (1) | MX376714B (enExample) |
| PE (1) | PE20151042A1 (enExample) |
| PL (1) | PL2895635T3 (enExample) |
| RU (1) | RU2620216C2 (enExample) |
| SI (1) | SI2895635T1 (enExample) |
| TR (1) | TR201903460T4 (enExample) |
| TW (1) | TW201432061A (enExample) |
| UA (1) | UA116111C2 (enExample) |
| WO (1) | WO2014040585A1 (enExample) |
| ZA (1) | ZA201502450B (enExample) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
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| US20170297369A1 (en) * | 2016-04-18 | 2017-10-19 | Benteler Steel/Tube Gmbh | Motor vehicle trailer, chassis axle, in particular for a motor vehicle trailer and use of the chassis axle and of a material |
| WO2018215813A1 (en) * | 2017-05-22 | 2018-11-29 | Arcelormittal | Method for producing a steel part and corresponding steel part |
| EP3460089A4 (en) * | 2016-07-06 | 2019-07-24 | Magang (Group) Holding Co., Ltd. | WHEEL FOR RAILING FROM BAINITIC STEEL WITH COST-EFFECTIVE, SLIM PRODUCTION AND METHOD OF PRODUCTION THEREFOR |
| WO2021144804A1 (en) * | 2020-01-17 | 2021-07-22 | Indian Institute Of Technology Bombay | High strength and toughness low carbon nanostructured bainitic steel and preparation method thereof |
| US20220195550A1 (en) * | 2020-12-23 | 2022-06-23 | Caterpillar Inc. | Air-hardened machine components |
| US11708624B2 (en) | 2018-09-14 | 2023-07-25 | Ausferritic Ab | Method for producing an ausferritic steel, austempered during continuous cooling followed by annealing |
| US12480173B2 (en) | 2018-11-30 | 2025-11-25 | Arcelormittal | Cold rolled annealed steel sheet with high hole expansion ratio and manufacturing process thereof |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
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| JP2018538440A (ja) | 2015-11-16 | 2018-12-27 | ベントラー スティール / チューブ ゲーエムベーハー | 高エネルギー吸収能力を備えた合金鋼及び鋼管製品 |
| DE102015119839A1 (de) * | 2015-11-17 | 2017-05-18 | Benteler Steel/Tube Gmbh | Stahllegierung mit hohem Energieaufnahmevermögen und Stahlrohrprodukt |
| JP6967628B2 (ja) * | 2015-12-29 | 2021-11-17 | アルセロールミタル | 超高強度合金化溶融亜鉛めっき鋼板を製造するための方法、及び得られた合金化溶融亜鉛めっき鋼板 |
| US11035020B2 (en) * | 2015-12-29 | 2021-06-15 | Arcelormittal | Galvannealed steel sheet |
| CN110616366B (zh) * | 2018-06-20 | 2021-07-16 | 宝山钢铁股份有限公司 | 一种125ksi钢级抗硫油井管及其制造方法 |
| CN109536843B (zh) * | 2019-01-04 | 2020-08-25 | 武汉钢铁有限公司 | 一种含氮双相耐腐蚀耐磨热轧钢及生产方法 |
| DE102019122515A1 (de) | 2019-08-21 | 2021-02-25 | Ilsenburger Grobblech Gmbh | Verfahren zur Herstellung von hochfesten Blechen oder Bändern aus einem niedrig legierten, hochfesten bainitischen Stahl sowie ein Stahlband oder Stahlblech hieraus |
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| CN116574978B (zh) * | 2023-04-23 | 2024-01-09 | 鞍钢股份有限公司 | 一种多阶段热处理细晶压力容器钢板及其制造方法 |
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- 2013-08-28 US US14/428,286 patent/US20150267282A1/en not_active Abandoned
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Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20170297369A1 (en) * | 2016-04-18 | 2017-10-19 | Benteler Steel/Tube Gmbh | Motor vehicle trailer, chassis axle, in particular for a motor vehicle trailer and use of the chassis axle and of a material |
| EP3460089A4 (en) * | 2016-07-06 | 2019-07-24 | Magang (Group) Holding Co., Ltd. | WHEEL FOR RAILING FROM BAINITIC STEEL WITH COST-EFFECTIVE, SLIM PRODUCTION AND METHOD OF PRODUCTION THEREFOR |
| WO2018215813A1 (en) * | 2017-05-22 | 2018-11-29 | Arcelormittal | Method for producing a steel part and corresponding steel part |
| WO2018215923A1 (en) * | 2017-05-22 | 2018-11-29 | Arcelormittal | Method for producing a steel part and corresponding steel part |
| US12454744B2 (en) | 2017-05-22 | 2025-10-28 | Arcelormittal | Method for producing a steel part and corresponding steel part |
| US11708624B2 (en) | 2018-09-14 | 2023-07-25 | Ausferritic Ab | Method for producing an ausferritic steel, austempered during continuous cooling followed by annealing |
| US12480173B2 (en) | 2018-11-30 | 2025-11-25 | Arcelormittal | Cold rolled annealed steel sheet with high hole expansion ratio and manufacturing process thereof |
| WO2021144804A1 (en) * | 2020-01-17 | 2021-07-22 | Indian Institute Of Technology Bombay | High strength and toughness low carbon nanostructured bainitic steel and preparation method thereof |
| US20220195550A1 (en) * | 2020-12-23 | 2022-06-23 | Caterpillar Inc. | Air-hardened machine components |
Also Published As
| Publication number | Publication date |
|---|---|
| CL2015000634A1 (es) | 2015-11-20 |
| PE20151042A1 (es) | 2015-07-27 |
| DK2895635T3 (da) | 2019-05-20 |
| BR112015005216A2 (pt) | 2022-07-26 |
| KR20150070150A (ko) | 2015-06-24 |
| JP6513568B2 (ja) | 2019-05-15 |
| PL2895635T3 (pl) | 2019-08-30 |
| AU2018201165B2 (en) | 2019-09-26 |
| WO2014040585A1 (de) | 2014-03-20 |
| ZA201502450B (en) | 2016-09-28 |
| AU2013314787A1 (en) | 2015-04-30 |
| KR102079612B1 (ko) | 2020-02-20 |
| TR201903460T4 (tr) | 2019-04-22 |
| TW201432061A (zh) | 2014-08-16 |
| US20200131608A1 (en) | 2020-04-30 |
| JP2015533942A (ja) | 2015-11-26 |
| SI2895635T1 (sl) | 2019-06-28 |
| EP2895635B1 (de) | 2019-03-06 |
| CA2881686A1 (en) | 2014-03-20 |
| RU2620216C2 (ru) | 2017-05-23 |
| AR092556A1 (es) | 2015-04-22 |
| UA116111C2 (uk) | 2018-02-12 |
| AU2018201165A1 (en) | 2018-03-22 |
| RU2015113522A (ru) | 2016-11-10 |
| ES2729562T3 (es) | 2019-11-04 |
| MX2015003103A (es) | 2015-10-22 |
| EP2895635A1 (de) | 2015-07-22 |
| MX376714B (es) | 2025-03-07 |
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