EP1563105B1 - Method for making an abrasion resistant steel plate and plate obtained - Google Patents
Method for making an abrasion resistant steel plate and plate obtained Download PDFInfo
- Publication number
- EP1563105B1 EP1563105B1 EP03786006A EP03786006A EP1563105B1 EP 1563105 B1 EP1563105 B1 EP 1563105B1 EP 03786006 A EP03786006 A EP 03786006A EP 03786006 A EP03786006 A EP 03786006A EP 1563105 B1 EP1563105 B1 EP 1563105B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- plate
- optionally
- steel
- process according
- temperature
- 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.)
- Expired - Lifetime
Links
- 229910000831 Steel Inorganic materials 0.000 title claims description 39
- 239000010959 steel Substances 0.000 title claims description 39
- 238000005299 abrasion Methods 0.000 title claims description 16
- 238000000034 method Methods 0.000 title claims description 12
- 239000010936 titanium Substances 0.000 claims description 36
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 22
- 229910052719 titanium Inorganic materials 0.000 claims description 17
- 238000001816 cooling Methods 0.000 claims description 15
- 229910052799 carbon Inorganic materials 0.000 claims description 13
- 229910000734 martensite Inorganic materials 0.000 claims description 12
- 150000001247 metal acetylides Chemical class 0.000 claims description 12
- 239000000203 mixture Substances 0.000 claims description 12
- 239000000126 substance Substances 0.000 claims description 10
- 229910001566 austenite Inorganic materials 0.000 claims description 9
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 8
- 229910052758 niobium Inorganic materials 0.000 claims description 7
- 239000007788 liquid Substances 0.000 claims description 6
- 229910052715 tantalum Inorganic materials 0.000 claims description 6
- 229910052714 tellurium Inorganic materials 0.000 claims description 6
- 229910052720 vanadium Inorganic materials 0.000 claims description 6
- 239000010949 copper Substances 0.000 claims description 5
- 238000010438 heat treatment Methods 0.000 claims description 5
- 239000012535 impurity Substances 0.000 claims description 5
- 238000004519 manufacturing process Methods 0.000 claims description 5
- 229910052711 selenium Inorganic materials 0.000 claims description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 4
- 229910052742 iron Inorganic materials 0.000 claims description 4
- 229910052745 lead Inorganic materials 0.000 claims description 4
- 229910052757 nitrogen Inorganic materials 0.000 claims description 4
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 238000003303 reheating Methods 0.000 claims description 3
- 238000005096 rolling process Methods 0.000 claims description 3
- 239000002893 slag Substances 0.000 claims description 3
- 238000005496 tempering Methods 0.000 claims description 3
- 238000003723 Smelting Methods 0.000 claims 2
- 229910052726 zirconium Inorganic materials 0.000 description 20
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 17
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 14
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 10
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 9
- 230000015572 biosynthetic process Effects 0.000 description 9
- 239000010955 niobium Substances 0.000 description 9
- 230000009466 transformation Effects 0.000 description 9
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 8
- 239000011572 manganese Substances 0.000 description 8
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 7
- 239000011651 chromium Substances 0.000 description 7
- 229910052750 molybdenum Inorganic materials 0.000 description 7
- 229910052759 nickel Inorganic materials 0.000 description 7
- -1 titanium carbides Chemical class 0.000 description 6
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 5
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 5
- 240000008042 Zea mays Species 0.000 description 5
- 229910001563 bainite Inorganic materials 0.000 description 5
- 229910052804 chromium Inorganic materials 0.000 description 5
- 230000000694 effects Effects 0.000 description 5
- 229910052748 manganese Inorganic materials 0.000 description 5
- 239000011733 molybdenum Substances 0.000 description 5
- 239000011669 selenium Substances 0.000 description 5
- 230000000717 retained effect Effects 0.000 description 4
- 229910052717 sulfur Inorganic materials 0.000 description 4
- 239000011593 sulfur Substances 0.000 description 4
- 238000003466 welding Methods 0.000 description 4
- 229910052796 boron Inorganic materials 0.000 description 3
- 238000005520 cutting process Methods 0.000 description 3
- 229940082150 encore Drugs 0.000 description 3
- 238000005098 hot rolling Methods 0.000 description 3
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 3
- 238000001556 precipitation Methods 0.000 description 3
- 230000009467 reduction Effects 0.000 description 3
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 3
- 229910052721 tungsten Inorganic materials 0.000 description 3
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 3
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 2
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 2
- BUGBHKTXTAQXES-UHFFFAOYSA-N Selenium Chemical compound [Se] BUGBHKTXTAQXES-UHFFFAOYSA-N 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- 241001080024 Telles Species 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 229910052797 bismuth Inorganic materials 0.000 description 2
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth atom Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 description 2
- 229910052791 calcium Inorganic materials 0.000 description 2
- 239000011575 calcium Substances 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 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 2
- 150000004767 nitrides Chemical class 0.000 description 2
- 238000010791 quenching Methods 0.000 description 2
- 230000000171 quenching effect Effects 0.000 description 2
- 230000002829 reductive effect Effects 0.000 description 2
- 238000006467 substitution reaction Methods 0.000 description 2
- 230000008961 swelling Effects 0.000 description 2
- PORWMNRCUJJQNO-UHFFFAOYSA-N tellurium atom Chemical compound [Te] PORWMNRCUJJQNO-UHFFFAOYSA-N 0.000 description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 2
- 239000010937 tungsten Substances 0.000 description 2
- 238000005275 alloying Methods 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 238000004873 anchoring Methods 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000000254 damaging effect Effects 0.000 description 1
- 230000014509 gene expression Effects 0.000 description 1
- 239000008187 granular material Substances 0.000 description 1
- 230000001965 increasing effect Effects 0.000 description 1
- WABPQHHGFIMREM-UHFFFAOYSA-N lead(0) Chemical compound [Pb] WABPQHHGFIMREM-UHFFFAOYSA-N 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 239000011044 quartzite Substances 0.000 description 1
- 150000004771 selenides Chemical class 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 150000004772 tellurides Chemical class 0.000 description 1
- 238000011282 treatment Methods 0.000 description 1
- 230000004580 weight loss Effects 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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/50—Ferrous alloys, e.g. steel alloys containing chromium with nickel with 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
- 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
- C22C38/14—Ferrous alloys, e.g. steel alloys containing titanium or zirconium
-
- 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
- C22C38/44—Ferrous alloys, e.g. steel alloys containing chromium with nickel 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
- C22C38/40—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
- 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
-
- 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
Definitions
- the present invention relates to an abrasion-resistant steel and its method of manufacture.
- High abrasion resistant steels with a hardness of about 600 Brinell are known. These steels contain from 0.4% to 0.6% of carbon and from 0.5% to 3% of at least one alloying element such as manganese, nickel, chromium and molybdenum and are soaked to have a completely martensitic structure. But these steels are very difficult to weld and cut. To remedy these drawbacks, it has been proposed, particularly in EP 0 739 993 to use for the same purposes, a less hard steel, whose carbon content is about 0.27% and having a quenched structure containing a significant amount of residual austenite. But these steels are still difficult to weld or cut.
- the object of the present invention is to overcome these disadvantages, by proposing an abrasion-resistant steel sheet whose abrasion resistance is comparable to that of known steels but whose weldability and thermal cutting ability is better.
- quenching may be followed by tempering at a temperature below 350 ° C, and preferably below 250 ° C.
- the invention also relates to a part, in particular a sheet, obtained in particular by this method, the steel having a martensitic or martensito-bainitic structure, said structure containing from 5% to 20% retained austenite, as well as carbides.
- the thickness of the sheet may be between 2 mm and 150 mm and its flatness is characterized by an arrow less than or equal to 12 mm / m and preferably less than 5 mm / m.
- the carbon, titanium, zirconium and nitrogen contents must be such that: C - Ti / 4 - Zr / 8 + 7xN / 8> 0.095%
- C * represents the free carbon content after precipitation of the titanium and zirconium carbides, taking into account the formation of titanium and zirconium nitrides.
- This free carbon content C * must be greater than 0.095%, and preferably ⁇ 0.12%, to have a martensite having a minimum hardness. The lower this content, the better the welding and thermal cutting ability.
- the micrographic structure of the steel consists of martensite or bainite or a mixture of these two structures, and from 5% to 20% retained austenite.
- This structure further comprises large titanium or zirconium carbides formed at high temperature, or even carbides of niobium, tantalum or vanadium.
- the inventors have found that the effectiveness of large carbides for improving the abrasion resistance could be obelated by the premature loosening thereof and that this loosening could be avoided by the presence of metastable austenite which is transformed under the effect of abrasion phenomena.
- the transformation of the metastable austenite is by swelling, this transformation in the abraded undercoat increases the resistance to carburetion and thus improves abrasion resistance.
- the steel is made, it flows in the form of slab or ingot.
- the slab or slug is hot-rolled to obtain a sheet which is subjected to a heat treatment which makes it possible at the same time to obtain the desired structure and a good flatness without subsequent planing or with limited planing.
- the heat treatment can be carried out directly in the hot rolling or carried out later, and possibly after a cold planing or half-hot.
- an expansion treatment such as tempering, can be carried out at a temperature of less than or equal to 350 ° C, and preferably less than 250 ° C.
- steel sheets identified A to C according to the invention and D to E according to the prior art were produced.
- the chemical compositions of the steels, expressed in 10 -3 % by weight, as well as the hardness and a wear resistance index Rus, are reported in Table 1.
- the wear resistance is measured by the weight loss of a prismatic specimen rotated in a tank containing calibrated granules of quartzite for 5 hours.
- the Rus index of a steel is equal to 100 times the ratio of the wear resistance of the steel in question and the wear resistance of a reference steel (steel D).
- All sheets are 27 mm thick and are hardened after austenitization at 900 ° C.
- the sheets according to the invention have a martensito-bainitic self-regenerating structure containing from 5% to 20% retained austenite and large titanium carbides, whereas the sheets given for comparison have a completely martensitic structure.
- the comparison of the wear resistances and the hardnesses shows that, although being very substantially less hard than the sheets given for comparison, the sheets according to the invention have a slightly better resistance to wear.
- the comparison of the free carbons shows that the good abrasion resistance of the sheets according to the invention is obtained with very significantly lower free carbons, which leads to significantly better welding or thermal cutting abilities than for the sheets according to the invention. the prior art.
- the deformation after cooling, without planing, for steels according to the invention A to C is about 5 mm / m and 16 mm / m for steels D and E given for comparison.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Heat Treatment Of Steel (AREA)
- Heat Treatment Of Sheet Steel (AREA)
- Treatment Of Steel In Its Molten State (AREA)
- Heat Treatment Of Articles (AREA)
Description
La présente invention est relative à un acier résistant à l'abrasion et à son procédé de fabrication.The present invention relates to an abrasion-resistant steel and its method of manufacture.
On connaît des aciers à haute résistance à l'abrasion dont la dureté est d'environ 600 Brinell. Ces aciers contiennent de 0,4% à 0,6% de carbone et de 0,5% à 3% d'au moins un élément d'alliage tel que le manganèse, le nickel, le chrome et le molybdène et ils sont trempés pour avoir une structure entièrement martensitique. Mais ces aciers sont très difficiles à souder et à découper. Pour remédier à ces inconvénients, on a proposé, notamment dans
Le but de la présente invention est de remédier à ces inconvénients, en proposant une tôle en acier résistant à l'abrasion dont la résistance à l'abrasion est comparable à celle des aciers connus mais dont l'aptitude au soudage et au découpage thermique est meilleure.The object of the present invention is to overcome these disadvantages, by proposing an abrasion-resistant steel sheet whose abrasion resistance is comparable to that of known steels but whose weldability and thermal cutting ability is better.
A cet effet, l'invention a pour objet un procédé pour fabriquer une pièce, et notamment une tôle, en acier pour abrasion dont la composition chimique comprend, en poids :
- 0,24% ≤ C < 0,35%
- 0% ≤ Si ≤ 2%
- 0% ≤ Al ≤ 2%
- 0,5% ≤ Si + Al ≤ 2%
- 0% ≤ Mn ≤ 2,5%
- 0% ≤ Ni ≤ 5%
- 0% ≤ Cr ≤ 5%
- 0% ≤ Mo ≤ 1%
- 0% ≤ W ≤ 2%
- 0,1% ≤ Mo +W/2 ≤ 1%
- 0% ≤ Cu ≤ 1,5%
- 0% ≤ B ≤ 0,02%
- 0% ≤ Ti ≤ 1,1%
- 0% ≤ Zr ≤ 2,2%
- 0,35% < Ti + Zr/2 ≤ 1,1%
- 0% ≤ S ≤ 0,15%
- N < 0,03%
- éventuellement au moins un élément pris parmi Nb, Ta et V en des teneurs telles que Nb/2 + Ta/4 + V ≤ 0,5%,
- éventuellement au moins un élément pris parmi Se, Te, Ca, Bi, Pb en des teneurs inférieures ou égales à 0,1%,
- C* = C - Ti/4 - Zr/8 + 7xN/8 ≥ 0,095% et de préférence ≥ 0,12% et :
- 1,05xMn + 0,54xNi +0,50xCr + 0,3x(Mo + W/2)1/2 + K > 1,8 ou mieux 2
Selon ce procédé, on soumet la pièce ou la tôle à un traitement thermique de trempe, effectué dans la chaude de mise en forme à chaud telle que le laminage ou après austénitisation par réchauffage dans un four, qui consiste à :
- refroidir la pièce ou la tôle à une vitesse de refroidissement moyenne supérieure à 0,5°C/s entre une température supérieure à AC3 et une température comprise entre T = 800 - 270xC* - 90xMn -37xNi - 70XCr - 83x(Mo + W/2) et T-50°C, la température étant exprimée en °C et les teneurs en C*, Mn, Ni, Cr, Mo et W, étant exprimées en % en poids,
- puis refroidir la pièce ou la tôle à une vitesse de refroidissement moyenne à coeur Vr < 1150xep-1,7 (en °C/s) et supérieure à 0,1°C/s entre la température T et 100°C, ep étant l'épaisseur de la pièce ou la tôle exprimée en mm,
- et à refroidir la pièce ou la tôle jusqu'à la température ambiante, éventuellement, on effectue un planage.
- 0.24% ≤ C <0.35%
- 0% ≤ If ≤ 2%
- 0% ≤ Al ≤ 2%
- 0.5% ≤ Si + Al ≤ 2%
- 0% ≤ Mn ≤ 2.5%
- 0% ≤ Ni ≤ 5%
- 0% ≤ Cr ≤ 5%
- 0% ≤ Mo ≤ 1%
- 0% ≤ W ≤ 2%
- 0.1% ≤ Mo + W / 2 ≤ 1%
- 0% ≤ Cu ≤ 1.5%
- 0% ≤ B ≤ 0.02%
- 0% ≤ Ti ≤ 1.1%
- 0% ≤ Zr ≤ 2.2%
- 0.35% <Ti + Zr / 2 ≤ 1.1%
- 0% ≤ S ≤ 0.15%
- N <0.03%
- optionally at least one element selected from Nb, Ta and V in contents such that Nb / 2 + Ta / 4 + V ≤ 0.5%,
- optionally at least one element selected from Se, Te, Ca, Bi, Pb in contents of less than or equal to 0.1%,
- C * = C - Ti / 4 - Zr / 8 + 7xN / 8 ≥ 0.095% and preferably ≥ 0.12% and:
- 1.05xMn + 0.54xNi + 0.50xCr + 0.3x (Mo + W / 2) 1/2 + K> 1.8 or better 2
According to this method, the part or the sheet is subjected to a quenching heat treatment, carried out in hot hot shaping such as rolling or after austenitization by reheating in an oven, which consists in:
- cooling the workpiece or sheet at an average cooling rate greater than 0.5 ° C / s between a temperature above AC 3 and a temperature between T = 800 - 270xC * - 90xMn -37xNi - 70XCr - 83x (Mo + W / 2) and T-50 ° C, the temperature being expressed in ° C and the contents of C *, Mn, Ni, Cr, Mo and W, being expressed in% by weight,
- then cool the workpiece or the sheet at an average cooling rate at core Vr <1150xep -1.7 (in ° C / s) and greater than 0.1 ° C / s between the temperature T and 100 ° C, ep being the thickness of the part or sheet metal expressed in mm,
- and to cool the workpiece or the sheet to room temperature, optionally, planing is carried out.
Eventuellement, la trempe peut être suivie d'un revenu à une température inférieure à 350°C, et préférence inférieure à 250°C.Optionally, quenching may be followed by tempering at a temperature below 350 ° C, and preferably below 250 ° C.
L'invention concerne également une pièce, notamment une tôle, obtenue notamment par ce procédé, l'acier ayant une structure martensitique ou martensito-bainitique, ladite structure contenant de 5% à 20% d'austénite retenue, ainsi que des carbures. L'épaisseur de la tôle peut être comprise entre 2 mm et 150 mm et sa planéité est caractérisée par une flèche inférieure ou égale à 12mm/m et de préférence inférieure à 5mm/m.The invention also relates to a part, in particular a sheet, obtained in particular by this method, the steel having a martensitic or martensito-bainitic structure, said structure containing from 5% to 20% retained austenite, as well as carbides. The thickness of the sheet may be between 2 mm and 150 mm and its flatness is characterized by an arrow less than or equal to 12 mm / m and preferably less than 5 mm / m.
L'invention va maintenant être décrite de façon plus précise mais non limitative et être illustrée par des exemples.The invention will now be described in a more precise but nonlimiting manner and be illustrated by examples.
Pour fabriquer une tôle selon l'invention, on élabore un acier dont la composition chimique comprend, en % en poids :
- de 0,24% à 0,35% de carbone pour permettre la formation d'une quantité importante de carbures et d'obtenir une dureté suffisante, tout en ayant une aptitude au soudage suffisante ; de préférence, la teneur en carbone est inférieure à 0,325%, et mieux inférieure à 0,3%.
- De 0% à 1,1% de titane, de 0% à 2,2% de zirconium. La somme Ti + Zr/2 doit être supérieure à 0,35% et de préférence supérieure à 0,4%, et mieux encore supérieure à 0,5%, de façon à former une quantité importante de gros carbures. Cependant, cette somme doit rester inférieure à 1,1% de façon à conserver suffisamment de carbone en solution dans la matrice après formation des carbures. De préférence cette somme doit rester inférieure à 1%, et mieux à 0,9% et mieux encore, inférieure à 0,7% si l'on a besoin de privilégier la ténacité du matériau. Il en résulte que la teneur en titane doit de préférence rester inférieure à 1%, et mieux inférieure à 0,9%, voire inférieure à 0,7%, et la teneur en zirconium doit de préférence rester inférieure à 2%, et mieux inférieure à 1,8%, voire inférieure à 1,4%.
- De 0% (ou des traces) à 2% de silicium et de 0% (ou des traces) à 2% d'aluminium, la somme Si+Al étant comprise entre 0,5% et 2% et de préférence supérieure à 0,7%. Ces éléments, qui sont des désoxydants, ont en outre pour effet de favoriser l'obtention d'une austénite retenue métastable fortement chargée en carbone dont la transformation en martensite s'accompagne d'un gonflement important favorisant l'ancrage des carbures de titane ou de zirconium.
- De 0% (ou des traces) à 2% ou même 2,5% de manganèse, de 0% (ou des traces) à 4% ou même 5% de nickel et de 0% (ou des traces) à 4% ou même 5% de chrome, pour obtenir une trempabilité suffisante et ajuster les différentes caractéristiques mécaniques ou d'emploi. Le nickel a, en particulier un effet favorable sur la ténacité, mais cet élément est cher. Le chrome forme également de fins carbures dans la martensite ou la bainite.
- De 0% (ou des traces) à 1% de molybdène et de 0% (ou des traces) à 2% de tungstène, la somme Mo+W/2 étant comprise entre 0,1% et 1%, et de préférence reste inférieure à 0,8%, ou mieux, inférieure à 0,6%. Ces éléments augmentent la trempabilité et forment dans la martensite ou dans la bainite de fins carbures durcissant, notamment par précipitation par auto revenu au cours du refroidissement. Il n'est pas nécessaire de dépasser une teneur de 1% en molybdène pour obtenir l'effet désiré en particulier en ce qui concerne la précipitation de carbures durcissants. Le molybdène peut être remplacé, en tout ou partie, par un poids double de tungstène. Néanmoins cette substitution n'est pas recherchée en pratique car elle n'offre pas d'avantage par rapport au molybdène et est plus coûteuse.
- Eventuellement de 0% à 1,5% de cuivre. Cet élément peut apporter un durcissement supplémentaire sans détériorer la soudabilité. Au-delà de 1,5%, il n'a plus d'effet significatif, il engendre des difficultés de laminage à chaud et coûte inutilement cher.
- De 0% à 0,02% de bore. Cet élément peut être ajouté de façon optionnelle afin d'augmenter la trempabilité. Pour que cet effet soit obtenu, la teneur en bore doit, de préférence, être supérieure à 0,0005% ou mieux 0,001%, et n'a pas besoin de dépasser sensiblement 0,01%.
- Jusqu'à 0,15% de soufre. Cet élément est un résiduel en général limité à 0,005% ou moins, mais sa teneur peut être volontairement augmentée pour améliorer l'usinabilité. A noter qu'en présence de soufre, pour éviter des difficultés de transformation à chaud, la teneur en manganèse doit être supérieure à 7 fois la teneur en soufre.
- Eventuellement au moins un élément pris parmi le niobium, le tantale et le vanadium, en des teneurs telles que Nb/2+Ta/4+V reste inférieure à 0,5% afin de former des carbures relativement gros qui améliorent la tenue à l'abrasion. Mais les carbures formés par ces éléments sont moins efficaces que ceux qui sont formés par le titane ou le zirconium, c'est pour cela qu'ils sont optionnels et ajoutés en quantité limitée.
- Eventuellement un ou plusieurs éléments pris parmi le sélénium, le tellure, le calcium, le bismuth et le plomb en des teneurs inférieures à 0,1% chacun. Ces éléments sont destinés à améliorer l'usinabilité. A noter que, lorsque l'acier contient du Se et/ou du Te, la teneur en manganèse doit être suffisante compte tenu de la teneur en soufre pour qu'il puisse se former des séléniures ou des tellurures de manganèse.
- Le reste étant du fer et des impuretés résultant de l'élaboration. Parmi les impuretés, il y a en particulier l'azote dont la teneur dépend du procédé d'élaboration mais ne dépasse en général pas 0,03%. Cet élément peut réagir avec le titane ou le zirconium pour former des nitrures qui ne doivent pas être trop gros pour ne pas détériorer la ténacité. Afin d'éviter la formation de gros nitrures, le titane et le zirconium peuvent être ajoutés dans l'acier liquide de façon très progressive, par exemple en mettant au contact de l'acier liquide oxydé une phase oxydée telle qu'un laitier chargé en oxydes de titane ou de zirconium, puis en désoxydant l'acier liquide, de façon à faire diffuser lentement le titane ou le zirconium depuis la phase oxydée vers l'acier liquide.
- from 0.24% to 0.35% carbon to allow the formation of a significant amount of carbides and to obtain sufficient hardness, while having sufficient welding ability; preferably, the carbon content is less than 0.325%, and more preferably less than 0.3%.
- From 0% to 1.1% titanium, from 0% to 2.2% zirconium. The sum Ti + Zr / 2 must be greater than 0.35% and preferably greater than 0.4%, and more preferably greater than 0.5%, so as to form a large amount of large carbides. However, this sum must remain less than 1.1% so as to keep enough carbon in solution in the matrix after formation of carbides. Preferably this sum must remain less than 1%, and better still 0.9% and better still less than 0.7% if one needs to favor the tenacity of the material. As a result, the titanium content should preferably remain less than 1%, and more preferably less than 0.9%, or even less than 0.7%, and the zirconium content should preferably remain below 2%, and better less than 1.8%, or even less than 1.4%.
- From 0% (or traces) to 2% silicon and 0% (or traces) at 2% aluminum, the sum Si + Al being between 0.5% and 2% and preferably greater than 0 , 7%. These elements, which are deoxidizing agents, also have the effect of favoring the obtaining of a metastable retained austenite highly loaded with carbon whose transformation into martensite is accompanied by a significant swelling favoring the anchoring of the titanium carbides or of zirconium.
- From 0% (or traces) to 2% or even 2.5% manganese, from 0% (or traces) to 4% or even 5% nickel and 0% (or traces) at 4% or even 5% chromium, to obtain a sufficient quenchability and adjust the different mechanical characteristics or use. Nickel has a particularly favorable effect on toughness, but this element is expensive. Chromium also forms fine carbides in martensite or bainite.
- 0% (or traces) at 1% molybdenum and 0% (or traces) at 2% tungsten, the sum Mo + W / 2 being between 0.1% and 1%, and preferably remains less than 0.8%, or better, less than 0.6%. These elements increase the quenchability and form in martensite or bainite of hardening carbides, in particular by self-precipitation during cooling. It is not necessary to exceed a molybdenum content of 1% in order to obtain the desired effect, particularly as regards the precipitation of hardening carbides. Molybdenum can be replaced in whole or in part by a double weight of tungsten. However, this substitution is not sought in practice because it offers no advantage over molybdenum and is more expensive.
- Possibly from 0% to 1.5% copper. This element can provide additional hardening without damaging the weldability. Beyond 1.5%, it has no significant effect, it generates hot rolling difficulties and unnecessarily expensive.
- 0% to 0.02% boron. This element can be added optionally to increase quenchability. For this effect to be obtained, the boron content should preferably be greater than 0.0005% or better 0.001%, and need not exceed substantially 0.01%.
- Up to 0.15% sulfur. This element is a residual usually limited to 0.005% or less, but its content can be voluntarily increased to improve machinability. It should be noted that in the presence of sulfur, in order to avoid difficulties of hot transformation, the manganese content must be greater than 7 times the sulfur content.
- Optionally at least one of niobium, tantalum and vanadium in such quantities that Nb / 2 + Ta / 4 + V remains below 0.5% in order to form relatively large carbides which improve the resistance to corrosion. 'abrasion. But the carbides formed by these elements are less effective than those formed by titanium or zirconium, that is why they are optional and added in limited quantities.
- Possibly one or more elements selected from selenium, tellurium, calcium, bismuth and lead in contents of less than 0.1% each. These elements are intended to improve machinability. Note that when the steel contains Se and / or Te, the manganese content must be sufficient sulfur content to form selenides or tellurides of manganese.
- The rest being iron and impurities resulting from the elaboration. Among the impurities, there is in particular nitrogen, the content of which depends on the production process but generally does not exceed 0.03%. This element can react with titanium or zirconium to form nitrides which must not be too big to not deteriorate toughness. In order to avoid the formation of large nitrides, titanium and zirconium can be added to the liquid steel in a very gradual manner, for example by contacting the oxidized liquid steel with an oxidized phase such as a slag loaded with oxides of titanium or zirconium, then deoxidizing the liquid steel, so as to slowly diffuse titanium or zirconium from the oxidized phase to the liquid steel.
En outre, afin d'obtenir des propriétés satisfaisantes, les teneurs en carbone, titane, zirconium, et azote doivent être telles que :
C - Ti/4 - Zr/8 + 7xN/8 > 0,095%In addition, in order to obtain satisfactory properties, the carbon, titanium, zirconium and nitrogen contents must be such that:
C - Ti / 4 - Zr / 8 + 7xN / 8> 0.095%
L'expression C - Ti/4 - Zr/8 + 7xN/8 = C* représente la teneur en carbone libre après précipitation des carbures de titane et de zirconium, compte tenu de la formation de nitrures de titane et de zirconium. Cette teneur en carbone libre C* doit être supérieur à 0,095%, et de préférence ≥ 0,12%, pour avoir une martensite ayant une dureté minimale. Plus cette teneur est faible, plus l'aptitude au soudage et à la découpe thermique est bonne.The expression C - Ti / 4 - Zr / 8 + 7xN / 8 = C * represents the free carbon content after precipitation of the titanium and zirconium carbides, taking into account the formation of titanium and zirconium nitrides. This free carbon content C * must be greater than 0.095%, and preferably ≥ 0.12%, to have a martensite having a minimum hardness. The lower this content, the better the welding and thermal cutting ability.
De plus, la composition chimique doit être choisie de telle sorte que la trempabilité de l'acier soit suffisante, compte tenu de l'épaisseur de la tôle qu'on souhaite fabriquer. Pour cela, la composition chimique doit satisfaire la relation:
- Tremp =1,05xMn + 0,54xNi +0,50xCr + 0,3x(Mo + W/2)1/2 + K > 1,8 ou mieux 2 avec : K = 0,5 si B > 0,001% et K = 0 si B < 0,001%,
- Tremp = 1.05xMn + 0.54xNi + 0.50xCr + 0.3x (Mo + W / 2) 1/2 + K> 1.8 or better 2 with: K = 0.5 if B> 0.001% and K = 0 if B <0.001%,
En outre, et pour obtenir une bonne tenue à l'abrasion, la structure micrographique de l'acier est constituée de martensite ou de bainite ou d'un mélange de ces deux structures, et de 5% à 20% d'austénite retenue. Cette structure comprenant en outre des gros carbures de titane ou de zirconium formés à haute température, voire des carbures de niobium, de tantale ou de vanadium. Les inventeurs ont constaté que l'efficacité des gros carbures pour l'amélioration de la tenue à l'abrasion pouvait être obérée par le déchaussement prématuré de ceux-ci et que ce déchaussement pouvait être évité par la présence d'austénite métastable qui se transforme sous l'effet des phénomènes d'abrasion. La transformation de l'austénite métastable se faisant par gonflement, cette transformation dans la sous-couche abrasée augmente la résistance au déchaussement des carbures et, ainsi, améliore la résistance à l'abrasion.In addition, and to obtain a good resistance to abrasion, the micrographic structure of the steel consists of martensite or bainite or a mixture of these two structures, and from 5% to 20% retained austenite. This structure further comprises large titanium or zirconium carbides formed at high temperature, or even carbides of niobium, tantalum or vanadium. The inventors have found that the effectiveness of large carbides for improving the abrasion resistance could be obelated by the premature loosening thereof and that this loosening could be avoided by the presence of metastable austenite which is transformed under the effect of abrasion phenomena. The transformation of the metastable austenite is by swelling, this transformation in the abraded undercoat increases the resistance to carburetion and thus improves abrasion resistance.
D'autre part, la dureté élevée de l'acier et la présence de carbures de titane fragilisant imposent de limiter autant que possible les opérations de planage. De ce point de vue, les inventeurs ont constaté qu'en ralentissant de façon suffisante le refroidissement dans le domaine de transformation bainito-martensitique, on réduit les déformations résiduelles des produits, ce qui permet de limiter les opérations de planage. Les inventeurs ont constaté qu'en refroidissant la pièce ou la tôle à une vitesse de refroidissement Vr < 1150xep-1,7, (dans cette formule, ep est l'épaisseur de la tôle exprimée en mm, et la vitesse de refroidissement est exprimée en °C/s) en dessous d'une température T = 800 - 270xC* - 90xMn -37xNi - 70XCr - 83x(Mo + W/2), (exprimée en °C), d'une part, on obtenait une proportion significative d'austénite résiduelle, et d'autre part, on réduisait les contraintes résiduelles engendrées par les changements de phase. Cette réduction de contraintes est souhaitable, à la fois pour limiter le recours au planage ou faciliter celui-ci d'une part, et pour limiter les risques de fissuration lors des opérations ultérieures de soudage et de pliage.On the other hand, the high hardness of the steel and the presence of embrittling titanium carbides make it necessary to limit the leveling operations as much as possible. From this point of view, the inventors have found that by slowing down cooling sufficiently in the bainitomensitic transformation domain, the residual deformations of the products are reduced, which makes it possible to limit the leveling operations. The inventors have found that cooling the workpiece or the sheet at a cooling rate Vr <1150xep -1.7 , (in this formula, ep is the thickness of the sheet expressed in mm, and the cooling rate is expressed in ° C / s) below a temperature T = 800 - 270xC * - 90xMn -37xNi - 70XCr - 83x (Mo + W / 2), (expressed in ° C), on the one hand, a proportion was obtained significant residual austenite, and on the other hand, the residual stresses generated by the phase changes were reduced. This reduction in stresses is desirable, both to limit the use of leveling or facilitate it on the one hand, and to limit the risk of cracking during subsequent welding and folding operations.
Pour fabriquer une tôle ayant une bonne résistance à l'abrasion et bien plane, on élabore l'acier, on le coule sous forme de brame ou de lingot. On lamine à chaud la brame ou le lingot pour obtenir une tôle qu'on soumet à un traitement thermique permettant tout à la fois d'obtenir la structure souhaitée et une bonne planéité sans planage ultérieur ou avec un planage limité. Le traitement thermique peut être effectué directement dans la chaude de laminage ou réalisé ultérieurement, et éventuellement après un planage à froid ou à mi-chaud.To make a sheet having a good resistance to abrasion and well flat, the steel is made, it flows in the form of slab or ingot. The slab or slug is hot-rolled to obtain a sheet which is subjected to a heat treatment which makes it possible at the same time to obtain the desired structure and a good flatness without subsequent planing or with limited planing. The heat treatment can be carried out directly in the hot rolling or carried out later, and possibly after a cold planing or half-hot.
Pour réaliser le traitement thermique :
- Soit directement après laminage à chaud, soit après réchauffage au-dessus du point AC3, on refroidit la tôle à une vitesse de refroidissement moyenne, supérieure à 0,5°C/s, c'est à dire supérieure à la vitesse critique de transformation bainitique jusqu'à une température égale ou légèrement inférieure à une température T = 800 - 270xC* - 90xMn -37xNi - 70XCr - 83x(Mo + W/2), (exprimée en °C), de façon à éviter la formation de constituants ferritiques ou perlitiques. Par légèrement inférieure, on entend une température comprise entre T et T - 50°C, ou mieux entre T et T - 25°C, ou mieux encore, entre T et T - 10°C.
- puis, entre la température précédemment définie et 100°C environ, on refroidit la tôle à une vitesse de refroidissement moyenne à coeur Vr comprise entre 0,1°C/s, pour obtenir une dureté suffisante, et 1150xep-1,7 pour obtenir la structure souhaitée,
- et on refroidit la tôle jusqu à la température ambiante, de préférence, sans que ce soit obligatoire, à une vitesse lente.
- Either directly after hot rolling, or after reheating above point AC 3 , the sheet is cooled to an average cooling rate, greater than 0.5 ° C./s, ie greater than the critical speed of bainitic transformation to a temperature equal to or slightly less than a temperature T = 800 - 270xC * - 90xMn -37xNi - 70XCr - 83x (Mo + W / 2), (expressed in ° C), so as to avoid the formation of ferritic constituents or pearlitic. By slightly lower is meant a temperature between T and T - 50 ° C, or better still between T and T - 25 ° C, or better still, between T and T - 10 ° C.
- then, between the previously defined temperature and approximately 100 ° C., the sheet is cooled to a mean core cooling rate Vr of between 0.1 ° C./s, to obtain a sufficient hardness, and 1150 × th -1.7 to obtain the desired structure,
- and the sheet is cooled to room temperature, preferably, but not necessarily, at a slow rate.
En outre, on peut effectuer un traitement de détente, tel qu'un revenu, à une température inférieure ou égale à 350°C, et de préférence, inférieure à 250°C.In addition, an expansion treatment, such as tempering, can be carried out at a temperature of less than or equal to 350 ° C, and preferably less than 250 ° C.
On obtient ainsi une tôle, dont l'épaisseur peut être comprise entre 2 mm et 150 mm, ayant une excellente planéité caractérisée par une flèche inférieure à 12 mm par mètre sans planage, où avec un planage modéré. La tôle a une dureté comprise entre 280HB et 450HB, environ. Cette dureté dépend principalement de la teneur en carbone libre C* = C - Ti/4 - Zr/8 + 7xN/8.This gives a sheet, whose thickness can be between 2 mm and 150 mm, having excellent flatness characterized by an arrow less than 12 mm per meter without planing, or with a moderate leveling. The sheet has a hardness of between 280HB and 450HB, approximately. This hardness depends mainly on the free carbon content C * = C - Ti / 4 - Zr / 8 + 7xN / 8.
A titre d'exemple, on a réalisé des tôles en acier repérées A à C selon l'invention et D à E selon l'art antérieur. Les compositions chimiques des aciers, exprimés en 10-3 % en poids, ainsi que la dureté et un indice de résistance à l'usure Rus, sont reportées au tableau 1.By way of example, steel sheets identified A to C according to the invention and D to E according to the prior art were produced. The chemical compositions of the steels, expressed in 10 -3 % by weight, as well as the hardness and a wear resistance index Rus, are reported in Table 1.
La résistance à l'usure est mesurée par la perte de poids d'une éprouvette prismatique mise en rotation dans un bac contenant des granulats calibrés de quartzite pendant 5 heures.The wear resistance is measured by the weight loss of a prismatic specimen rotated in a tank containing calibrated granules of quartzite for 5 hours.
L'indice Rus d'un acier est égal à 100 fois le rapport de la résistance à l'usure de l'acier considéré et de la résistance à l'usure d'un acier de référence (l'acier D). Ainsi, un acier dont l'indice Rus = 110 a une résistance à l'usure de 10% supérieure à celle de l'acier de référence.The Rus index of a steel is equal to 100 times the ratio of the wear resistance of the steel in question and the wear resistance of a reference steel (steel D). Thus, a steel whose Rus = 110 index has a wear resistance 10% higher than that of the reference steel.
Toutes les tôles ont une épaisseur de 27 mm, et sont trempées après austénitisation à 900°C.All sheets are 27 mm thick and are hardened after austenitization at 900 ° C.
Après austénitisation :
- pour les tôles en acier A et C, la vitesse moyenne de refroidissement est de 7°C/s au dessus de la température T définie plus haut, et de 1,6°C/s en dessous, conformément à l'invention;
- pour la tôle B, la vitesse moyenne de refroidissement est de 0,8°C/s au dessus de la température T définie plus haut, et de 0,15°C/s en dessous, conformément à l'invention;
- les tôles en acier D et E, données à titre de comparaison, ont été refroidies à une vitesse moyenne de 24°C/s au dessus de la température T définie plus haut, et à une vitesse moyenne de 12°C/s en dessous.
- for steel sheets A and C, the average cooling rate is 7 ° C / s above the temperature T defined above, and 1.6 ° C / s below, according to the invention;
- for sheet B, the average cooling rate is 0.8 ° C / s above the temperature T defined above, and 0.15 ° C / s below, according to the invention;
- the steel sheets D and E, given for comparison, were cooled at an average speed of 24 ° C / s above the temperature T defined above, and at an average speed of 12 ° C / s below .
Les tôles selon l'invention ont une structure martensito-bainitique auto-revenue contenant de 5% à 20% d'austénite retenue et des gros carbures de titane, alors que les tôles données à titre de comparaison ont une structure entièrement martensitique.The sheets according to the invention have a martensito-bainitic self-regenerating structure containing from 5% to 20% retained austenite and large titanium carbides, whereas the sheets given for comparison have a completely martensitic structure.
La comparaison des résistances à l'usure et des duretés montre que, bien qu'étant très sensiblement moins dures que les tôles données à titre de comparaison, les tôles selon l'invention ont une résistance à l'usure légèrement meilleure. La comparaison des carbones libres montre que la bonne tenue à l'usure des tôles selon l'invention est obtenue avec des carbones libres très sensiblement plus faibles, ce qui conduit à des aptitudes au soudage ou au découpage thermique nettement meilleures que pour les tôles selon l'art antérieur. Par ailleurs, la déformation après refroidissement, sans planage, pour les aciers selon l'invention A à C est d'environ 5 mm/m et de 16 mm/m pour les aciers D et E donnés à titre de comparaison. Ces résultats montrent la réduction de déformation des produits obtenus grâce à l'invention.The comparison of the wear resistances and the hardnesses shows that, although being very substantially less hard than the sheets given for comparison, the sheets according to the invention have a slightly better resistance to wear. The comparison of the free carbons shows that the good abrasion resistance of the sheets according to the invention is obtained with very significantly lower free carbons, which leads to significantly better welding or thermal cutting abilities than for the sheets according to the invention. the prior art. Furthermore, the deformation after cooling, without planing, for steels according to the invention A to C is about 5 mm / m and 16 mm / m for steels D and E given for comparison. These results show the reduction of deformation of the products obtained thanks to the invention.
Il en résulte en pratique, en fonction du degré d'exigence en planéité des utilisateurs,
- soit la possibilité de livrer les produits sans planage, ce qui engendre un gain sur le coût et une réduction des contraintes résiduelles,
- soit l'exécution d'un planage pour satisfaire une exigence de planéité plus sévère (par exemple 5mm/m) mais réalisée plus facilement et en introduisant moins de contraintes du fait de la déformation originelle moindre sur les produits selon l'invention.
- the possibility of delivering the products without planing, which generates a cost saving and a reduction of the residual stresses,
- either the execution of a planing to satisfy a requirement of flatness more severe (for example 5mm / m) but achieved more easily and introducing fewer constraints due to the original deformation less on the products according to the invention.
Claims (13)
- Process for manufacturing a part or a plate made of an abrasion-resistant steel, the chemical composition of which comprises, by weight:0.24% ≤ C < 0.35%0% ≤ Si ≤ 2%0% ≤ Al ≤ 2%0.5% ≤ Si + Al ≤ 2%0% ≤ Mn ≤ 2.5%0% ≤ Ni ≤ 5%0% ≤ Cr ≤ 5%0% ≤ Mo ≤ 1%0% ≤ W ≤ 2%0.1% ≤ Mo +W/2 ≤ 1%0% ≤ B ≤ 0.02%0% ≤ Ti ≤ 1.1%0% ≤ Zr ≤ 2.2%0.35% ≤ Ti +Zr/2 ≤ 1.1%0% ≤ S ≤ 0.15%N < 0.03%- optionally, 0% to 1.5% of copper;- optionally, at least one element taken from Nb, Ta and V in contents such that Nb/2 + Ta/4 + V ≤ 0.5%;- optionally, at least one element taken from Se, Te, Ca, Bi and Pb in contents of 0.1% or less, the balance being iron and impurities resulting from the smelting, the chemical composition furthermore satisfying the following relationships:where K = 0.5 if B ≥ 0.0005% and K = 0 if B < 0.0005%,C* = C-Ti/4-Zr/8+7×N/8 ≥ 0.095%and
1.05×Mn+ 0.54×Ni +0.50×Cr+0.3×(Mo+W/2)1/2 +K > 1.8
in which the part or the plate undergoes a hardening heat treatment carried out in the hot-forming heat, for example rolling heat, or after austenitization by reheating in a furnace, in order to carry out the hardening, in which:- the part or the plate is cooled at an average cooling rate of greater than 0.5°C/s between a temperature above AC3 and a temperature between T = 800-270×C*-90×Mn-37×Ni-70×Cr-83×(Mo+W/2) and about T-50°C;- then the part or the plate is cooled at an average core cooling rate Vc < 1150 × th-1.7 and greater than 0.1°C/s between the temperature T and 100°C, th being the thickness of the part or plate expressed in mm; and- the part or the plate is cooled down to ambient temperature and, optionally, undergoes skin pass rolling. - Process according to Claim 1, characterized in that:1.05xMn+0.54xNi+0.50xCr+0.3x(Mo+W/2)1/2+K > 2
- Process according to Claim 1 or Claim 2, characterized in that:Ti + Zr/2 ≥ 0.4%.
- Process according to any one of Claims 1 to 3, characterized in that:C* ≥ 0.12%.
- Process according to any one of Claims 1 to 4, characterized in that:Si + Al ≥ 0.7%.
- Process according to any one of Claims 1 to 5, characterized in that a tempering operation is also carried out at a temperature of 350°C or below.
- Process according to any one of Claims 1 to 6, characterized in that, to add titanium to the steel, a liquid steel is brought into contact with a titanium-containing slag and the titanium is made to diffuse slowly from the slag into the liquid steel.
- Part, and especially a plate, made of an abrasion-resistant steel, the chemical composition of which comprises, by weight:0.24% ≤ C < 0.35%0% ≤ Si ≤ 2%0% ≤ Al ≤ 2%0.5% ≤ Si + Al ≤ 2%0% ≤ Mn ≤ 2.5%0% ≤ Ni ≤ 5%0% ≤ Cr ≤ 5%0% ≤ Mo ≤ 1%0% ≤ W ≤ 2%0.1% ≤ Mo +W/2 ≤ 1%0% ≤ B < 0.02%0% ≤ Ti ≤ 1.1%0% ≤ Zr ≤ 2.2%0.35% ≤ Ti +Zr/2 ≤ 1.1%0% ≤ S ≤ 0.15%N < 0.03%- optionally, 0% to 1.5% of copper;- optionally, at least one element taken from Nb, Ta and V in contents such that Nb/2 + Ta/4 + V ≤ 0.5%;- optionally, at least one element taken from Se, Te, Ca, Bi and Pb in contents of 0.1% or less, the balance being iron and impurities resulting from the smelting, the chemical composition furthermore satisfying the following relationships:where K = 0.5 if B ≥ 0.0005% and K = 0 if B < 0.0005%,C* = C-Ti/4-Zr/8+7×N/8 ≥ 0.095% and1.05×Mn+0.54×Ni+0.50×Cr+0.3×(Mo+W/2)1/2+K > 1.8
the steel having a martensitic or martensitic-bainitic structure, said structure containing 5% to 20% residual austenite and carbides. - Part according to Claim 8, characterized in that:1.05×Mn+0.54×Ni+0.50×Cr+0.3×(Mo+W/2)1/2+K > 2
- Part according to Claim 8 or Claim 9, characterized in that:Ti + Zr/2 ≥ 0.4%.
- Part according to any one of Claims 8 to 10, characterized in that:C* ≥ 0.12%.
- Part according to any one of Claims 8 to 11, characterized in that:Si + Al ≥ 0.7%.
- Part according to any one of Claims 8 to 12, characterized in that it is a plate with a thickness between 2 mm and 150 mm.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SI200331112T SI1563105T1 (en) | 2002-11-19 | 2003-11-13 | Method for making an abrasion resistant steel plate and plate obtained |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0214426 | 2002-11-19 | ||
FR0214426A FR2847272B1 (en) | 2002-11-19 | 2002-11-19 | METHOD FOR MANUFACTURING AN ABRASION RESISTANT STEEL SHEET AND OBTAINED SHEET |
PCT/FR2003/003358 WO2004048619A1 (en) | 2002-11-19 | 2003-11-13 | Method for making an abrasion resistant steel plate and plate obtained |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1563105A1 EP1563105A1 (en) | 2005-08-17 |
EP1563105B1 true EP1563105B1 (en) | 2008-01-02 |
Family
ID=32187697
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP03786006A Expired - Lifetime EP1563105B1 (en) | 2002-11-19 | 2003-11-13 | Method for making an abrasion resistant steel plate and plate obtained |
Country Status (19)
Country | Link |
---|---|
US (1) | US7713362B2 (en) |
EP (1) | EP1563105B1 (en) |
JP (1) | JP4535876B2 (en) |
KR (1) | KR101010571B1 (en) |
CN (1) | CN100348738C (en) |
AR (1) | AR042073A1 (en) |
AT (1) | ATE382716T1 (en) |
AU (1) | AU2003295014B2 (en) |
BR (1) | BR0315693B1 (en) |
CA (1) | CA2506349C (en) |
DE (1) | DE60318478T2 (en) |
ES (1) | ES2298605T3 (en) |
FR (1) | FR2847272B1 (en) |
PE (1) | PE20040484A1 (en) |
PL (1) | PL202086B1 (en) |
RU (1) | RU2326179C2 (en) |
UA (1) | UA78624C2 (en) |
WO (1) | WO2004048619A1 (en) |
ZA (1) | ZA200504150B (en) |
Families Citing this family (59)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2847270B1 (en) * | 2002-11-19 | 2004-12-24 | Usinor | METHOD FOR MANUFACTURING AN ABRASION RESISTANT STEEL SHEET AND OBTAINED SHEET |
JP4894296B2 (en) * | 2006-02-28 | 2012-03-14 | Jfeスチール株式会社 | Wear-resistant steel plate |
JP4894297B2 (en) * | 2006-02-28 | 2012-03-14 | Jfeスチール株式会社 | Wear-resistant steel plate |
JP5176954B2 (en) * | 2006-05-10 | 2013-04-03 | 新日鐵住金株式会社 | Steel sheet for hot pressed steel sheet member and method for producing hot pressed steel sheet |
JP4899874B2 (en) * | 2007-01-12 | 2012-03-21 | Jfeスチール株式会社 | Wear-resistant steel plate with excellent workability and method for producing the same |
JP5380892B2 (en) * | 2007-05-29 | 2014-01-08 | Jfeスチール株式会社 | Wear-resistant steel plate with excellent workability and method for producing the same |
FR2919593B1 (en) * | 2007-07-30 | 2009-11-20 | Sidel Participations | DEVICE FOR FORMING LOTS OF SUBSTANTIALLY PARALLELEPIPEDIC OBJECTS CIRCULATING ON A CONVEYOR BELT |
CN101240399B (en) * | 2008-03-05 | 2010-06-02 | 钢铁研究总院 | Low-chromium low-cost hot working die steel |
US8137483B2 (en) * | 2008-05-20 | 2012-03-20 | Fedchun Vladimir A | Method of making a low cost, high strength, high toughness, martensitic steel |
JP2010085716A (en) | 2008-09-30 | 2010-04-15 | Fujinon Corp | Lens assembly and image capturing apparatus |
CN101775545B (en) * | 2009-01-14 | 2011-10-12 | 宝山钢铁股份有限公司 | Low-alloy high-strength high-toughness wear-resistant steel plate and manufacturing method thereof |
US8689667B2 (en) | 2010-04-22 | 2014-04-08 | Milwaukee Electric Tool Corporation | Saw blade |
US10189099B2 (en) | 2010-04-22 | 2019-01-29 | Milwaukee Electric Tool Corporation | Saw Blade |
JP5866820B2 (en) * | 2010-06-30 | 2016-02-24 | Jfeスチール株式会社 | Wear-resistant steel plate with excellent weld toughness and delayed fracture resistance |
JP2012031511A (en) * | 2010-06-30 | 2012-02-16 | Jfe Steel Corp | Wear-resistant steel sheet having excellent toughness of multi-layer-welded part and lagging destruction resistance properties |
RU2458177C1 (en) * | 2010-12-03 | 2012-08-10 | Открытое акционерное общество "Магнитогорский металлургический комбинат" | Strip rolled products from boron-containing manganese steel |
RU2460823C1 (en) * | 2011-02-08 | 2012-09-10 | Российская Федерация, от имени которой выступает Министерство промышленности и торговли (Минпромторг России) | Dynamically resistant steel, and manufacturing method of plates from it |
USD841417S1 (en) | 2011-04-22 | 2019-02-26 | Milwaukee Electric Tool Corporation | Saw blade |
CN102367558B (en) * | 2011-10-24 | 2016-05-04 | 山东双轮股份有限公司 | A kind of pump boric low alloy wear resistant steel |
CN102560272B (en) * | 2011-11-25 | 2014-01-22 | 宝山钢铁股份有限公司 | Ultrahigh-strength abrasion-resistant steel plate and manufacturing method thereof |
CN103898420A (en) * | 2012-12-25 | 2014-07-02 | 隆英(金坛)特钢科技有限公司 | Wear-resisting steel plate and manufacturing method thereof |
CN103060715B (en) * | 2013-01-22 | 2015-08-26 | 宝山钢铁股份有限公司 | A kind of ultra-high strength and toughness steel plate and manufacture method thereof with low yielding ratio |
US9738334B2 (en) * | 2013-05-07 | 2017-08-22 | Arcelormittal | Track shoe having increased service life useful in a track drive system |
RU2532768C1 (en) * | 2013-07-23 | 2014-11-10 | Открытое акционерное общество "Северсталь" (ОАО "Северсталь") | Manufacturing method of rolled stock from low-alloy plate steel |
SI2789699T1 (en) | 2013-08-30 | 2017-06-30 | Rautaruukki Oyj | A high-hardness hot-rolled steel product, and a method of manufacturing the same |
CN103614645A (en) * | 2013-10-24 | 2014-03-05 | 铜陵市经纬流体科技有限公司 | Cold-brittleness resistant alloy steel material used for pump trucks and preparation method of the material |
CN103627967A (en) * | 2013-11-12 | 2014-03-12 | 铜陵市肆得科技有限责任公司 | Wear-resistant alloy steel material for pump casing and preparation method thereof |
CN103628001A (en) * | 2013-11-12 | 2014-03-12 | 铜陵市肆得科技有限责任公司 | Alloy steel material for corrosion-resistant pump valve and preparation method thereof |
CN103898421B (en) * | 2013-11-15 | 2016-04-06 | 东南大学 | A kind of manufacture method of grinder hammerhead |
AT515157B1 (en) * | 2013-11-21 | 2016-12-15 | Böhler Edelstahl GmbH & Co KG | Process for producing plastic molds from martensitic chromium steel and plastic mold |
CN103757552B (en) * | 2013-12-17 | 2016-01-20 | 界首市华盛塑料机械有限公司 | A kind of cutting tool alloy steel material and preparation method thereof |
RU2546262C1 (en) * | 2014-01-09 | 2015-04-10 | Публичное акционерное общество "Северсталь" (ПАО "Северсталь") | Wear-resistant steel and item made from it |
RU2544981C1 (en) * | 2014-03-06 | 2015-03-20 | Закрытое акционерное общество "Омутнинский металлургический завод" | Medium-carbon screw steel |
CN104073741A (en) * | 2014-05-09 | 2014-10-01 | 铜陵市明诚铸造有限责任公司 | High-temperature and deformation resistant alloy steel material and preparation method thereof |
RU2557860C1 (en) * | 2014-09-15 | 2015-07-27 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Южно-Уральский государственный университет" (национальный исследовательский университет) (ФГБОУ ВПО "ЮУрГУ" (НИУ)) | Easy-to-machine structural chromium-manganese-molybdenum steel |
CN104313506A (en) * | 2014-10-20 | 2015-01-28 | 熊荣鑫 | Non-spark iron alloy |
CN104451436A (en) * | 2014-12-08 | 2015-03-25 | 钢铁研究总院 | Bainite-martensite-austenite multi-phase wear-resistant steel plate and manufacturing method thereof |
CN104357758B (en) * | 2014-12-08 | 2016-03-30 | 钢铁研究总院 | A kind of ultra-hard particles enhancement type martensite wear-resistant steel plate and manufacture method thereof |
CN104561834A (en) * | 2014-12-26 | 2015-04-29 | 济源市金诚科技有限公司 | Hard alloy steel and preparation method thereof |
RU2593810C1 (en) * | 2015-03-04 | 2016-08-10 | Открытое акционерное общество "Магнитогорский металлургический комбинат" | Method for production of high-strength steel sheet |
CN104651735B (en) * | 2015-03-06 | 2017-01-18 | 武汉钢铁(集团)公司 | Low-alloy wear-resistant steel with toughness being more than 50J/cm2 and production method thereof |
EP3366801A4 (en) | 2015-10-19 | 2019-05-01 | Nippon Steel & Sumitomo Metal Corporation | HOT ROLLED STEEL AND STEEL PIECE |
CN105220075B (en) * | 2015-11-02 | 2017-05-24 | 大冶有色机电设备修造有限公司 | Method for producing lining plate of ball mill by adopting rolling technology |
CN105648310B (en) * | 2016-03-30 | 2017-09-29 | 河北钢铁股份有限公司承德分公司 | A kind of shellproof coil of strip of hot rolling containing vanadium and its production method |
AU2016403221B2 (en) | 2016-04-19 | 2019-09-19 | Jfe Steel Corporation | Abrasion-Resistant Steel Plate and Method of Producing Abrasion-Resistant Steel Plate |
KR102126661B1 (en) * | 2016-04-19 | 2020-06-25 | 제이에프이 스틸 가부시키가이샤 | Abrasion-resistant steel plate and method of producing abrasion-resistant steel plate |
CN105903764A (en) * | 2016-04-22 | 2016-08-31 | 柳州凯通新材料科技有限公司 | Composite wear-resisting steel plate rolling technology |
RU2625861C1 (en) * | 2016-05-23 | 2017-07-19 | Открытое акционерное общество "Магнитогорский металлургический комбинат" | Production of steel sheets of higher wear resistance |
KR102250916B1 (en) * | 2017-03-13 | 2021-05-11 | 제이에프이 스틸 가부시키가이샤 | Abrasion-resistant steel plate and method of manufacturing same |
US11413693B2 (en) | 2017-05-16 | 2022-08-16 | Milwaukee Electric Tool Corporation | Saw blade |
CN107385354B (en) * | 2017-08-02 | 2019-02-12 | 合肥安力电力工程有限公司 | A kind of high-hardness wear-resistant and oxidation-resistant steel for electrician pliers |
CN107916360A (en) * | 2017-11-14 | 2018-04-17 | 郑媛媛 | A kind of production technology of high-strength abrasion-proof safety valve |
CN107829033B (en) * | 2017-11-23 | 2019-10-11 | 攀钢集团攀枝花钢铁研究院有限公司 | High abrasion containing V brake rim hot continuous rolling alloy-steel plate and its production method |
RU2674797C1 (en) * | 2018-06-07 | 2018-12-13 | Публичное акционерное общество "Магнитогорский металлургический комбинат" | Method of producing high-strength cold-resistant sheet from low-alloy steel |
CN108893680A (en) * | 2018-06-26 | 2018-11-27 | 澳洋集团有限公司 | A kind of low-alloy wear-resistant steel and preparation method thereof |
CN113122771B (en) * | 2019-12-31 | 2022-01-14 | 中内凯思汽车新动力系统有限公司 | High-performance friction welding steel piston and preparation method thereof |
CN115141985B (en) * | 2021-03-31 | 2023-05-09 | 宝山钢铁股份有限公司 | Medium-carbon high-titanium boron-containing steel with high hardenability and slab continuous casting production method thereof |
CN113458175A (en) * | 2021-06-21 | 2021-10-01 | 周传盛 | Spring steel processing method |
CN114107823A (en) * | 2021-11-30 | 2022-03-01 | 宝武集团马钢轨交材料科技有限公司 | Steel for high-speed wheel, heat treatment method of steel and method for preparing high-speed wheel by using steel |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3883347A (en) * | 1971-02-16 | 1975-05-13 | Aikoh Co | Slag-forming agent for steelmaking |
US4170497A (en) * | 1977-08-24 | 1979-10-09 | The Regents Of The University Of California | High strength, tough alloy steel |
JPH0441616A (en) * | 1990-06-06 | 1992-02-12 | Nkk Corp | Production of low-hardness water-resistant steel excellent in wear resistance and bendability |
US5595614A (en) * | 1995-01-24 | 1997-01-21 | Caterpillar Inc. | Deep hardening boron steel article having improved fracture toughness and wear characteristics |
FR2733516B1 (en) * | 1995-04-27 | 1997-05-30 | Creusot Loire | STEEL AND PROCESS FOR THE MANUFACTURE OF PARTS WITH HIGH ABRASION RESISTANCE |
JPH09249935A (en) * | 1996-03-13 | 1997-09-22 | Sumitomo Metal Ind Ltd | High-strength steel with excellent resistance to sulfide stress cracking and its manufacturing method |
CN1182142A (en) * | 1996-11-07 | 1998-05-20 | 鞍山钢铁集团公司 | Abrasion-resisting cast steel |
JP3975852B2 (en) | 2001-10-25 | 2007-09-12 | Jfeスチール株式会社 | Steel pipe excellent in workability and manufacturing method thereof |
FR2847271B1 (en) * | 2002-11-19 | 2004-12-24 | Usinor | METHOD FOR MANUFACTURING AN ABRASION RESISTANT STEEL SHEET AND OBTAINED SHEET |
FR2847270B1 (en) * | 2002-11-19 | 2004-12-24 | Usinor | METHOD FOR MANUFACTURING AN ABRASION RESISTANT STEEL SHEET AND OBTAINED SHEET |
-
2002
- 2002-11-19 FR FR0214426A patent/FR2847272B1/en not_active Expired - Lifetime
-
2003
- 2003-11-13 AU AU2003295014A patent/AU2003295014B2/en not_active Expired
- 2003-11-13 CA CA2506349A patent/CA2506349C/en not_active Expired - Lifetime
- 2003-11-13 UA UAA200505980A patent/UA78624C2/en unknown
- 2003-11-13 EP EP03786006A patent/EP1563105B1/en not_active Expired - Lifetime
- 2003-11-13 DE DE60318478T patent/DE60318478T2/en not_active Expired - Lifetime
- 2003-11-13 ES ES03786006T patent/ES2298605T3/en not_active Expired - Lifetime
- 2003-11-13 PL PL375543A patent/PL202086B1/en unknown
- 2003-11-13 BR BRPI0315693-1A patent/BR0315693B1/en active IP Right Grant
- 2003-11-13 KR KR1020057009055A patent/KR101010571B1/en active IP Right Grant
- 2003-11-13 US US10/535,305 patent/US7713362B2/en active Active
- 2003-11-13 AT AT03786006T patent/ATE382716T1/en active
- 2003-11-13 CN CNB2003801036284A patent/CN100348738C/en not_active Expired - Lifetime
- 2003-11-13 JP JP2004554594A patent/JP4535876B2/en not_active Expired - Lifetime
- 2003-11-13 WO PCT/FR2003/003358 patent/WO2004048619A1/en active IP Right Grant
- 2003-11-13 RU RU2005119205/02A patent/RU2326179C2/en active
- 2003-11-18 AR ARP030104259A patent/AR042073A1/en unknown
- 2003-11-18 PE PE2003001167A patent/PE20040484A1/en not_active Application Discontinuation
-
2005
- 2005-05-23 ZA ZA200504150A patent/ZA200504150B/en unknown
Also Published As
Publication number | Publication date |
---|---|
FR2847272A1 (en) | 2004-05-21 |
WO2004048619A8 (en) | 2005-05-26 |
JP2006506527A (en) | 2006-02-23 |
CN100348738C (en) | 2007-11-14 |
DE60318478T2 (en) | 2008-12-11 |
UA78624C2 (en) | 2007-04-10 |
WO2004048619A1 (en) | 2004-06-10 |
US7713362B2 (en) | 2010-05-11 |
ZA200504150B (en) | 2006-09-27 |
BR0315693B1 (en) | 2011-06-28 |
RU2005119205A (en) | 2006-05-10 |
PL202086B1 (en) | 2009-05-29 |
RU2326179C2 (en) | 2008-06-10 |
FR2847272B1 (en) | 2004-12-24 |
KR101010571B1 (en) | 2011-01-25 |
EP1563105A1 (en) | 2005-08-17 |
US20060162826A1 (en) | 2006-07-27 |
CN1714159A (en) | 2005-12-28 |
CA2506349A1 (en) | 2004-06-10 |
DE60318478D1 (en) | 2008-02-14 |
AR042073A1 (en) | 2005-06-08 |
AU2003295014B2 (en) | 2009-03-12 |
PL375543A1 (en) | 2005-11-28 |
PE20040484A1 (en) | 2004-08-18 |
KR20050083903A (en) | 2005-08-26 |
ATE382716T1 (en) | 2008-01-15 |
JP4535876B2 (en) | 2010-09-01 |
CA2506349C (en) | 2012-04-24 |
AU2003295014A1 (en) | 2004-06-18 |
BR0315693A (en) | 2005-09-20 |
ES2298605T3 (en) | 2008-05-16 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1563105B1 (en) | Method for making an abrasion resistant steel plate and plate obtained | |
EP1563103B1 (en) | Method for making an abrasion resistant steel plate and steel plate obtained | |
EP1563104B1 (en) | Method for making an abrasion resistant steel plate and plate obtained | |
EP2171112B1 (en) | Method for producing steel sheets having high resistance and ductility characteristics, and sheets thus obtained | |
EP1913169B1 (en) | Manufacture of steel sheets having high resistance and excellent ductility, products thereof | |
EP3783116B1 (en) | Pre-coated sheets allowing the production of press-hardened and coated steel parts | |
CA2680623C (en) | Steel for tool-less hot forming or quenching with improved ductility | |
EP1751321B1 (en) | Steel with high mechanical strength and wear resistance | |
JP5024051B2 (en) | Centrifugal cast composite roll | |
CA2847809C (en) | Rolled steel that hardens by means of precipitation after hot-forming and/or quenching with a tool having very high strength and ductility, and method for manufacturing same | |
KR100386134B1 (en) | High strength low alloy heat resistant steel | |
CA3065036C (en) | Method for producing high-strength steel parts with improved ductility, and parts obtained by said method | |
EP2707515B1 (en) | Producing method for very high yield strength martensitic steel sheet and steel sheet obtained | |
TWI741145B (en) | Composite roll for rolling and manufacturing method thereof | |
BE1008531A6 (en) | Hot rolled steel affine no heat and method for the preparation thereof. | |
CA2980878C (en) | Parts with a bainitic structure having high strength properties and manufacturing process | |
FR2847273A1 (en) | Weldable steel components for construction applications requiring an elevated hardness and a martensite or martensite-bainite structure | |
EP1885900B1 (en) | Steel for submarine hulls with improved weldability | |
JP4823441B2 (en) | Continuous casting and hot rolling rolls with excellent hot wear resistance and thermal crack resistance | |
JP4320764B2 (en) | Gear case hardened steel with excellent impact fatigue strength and anti-pitting strength |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 20050513 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR |
|
AX | Request for extension of the european patent |
Extension state: AL LT LV MK |
|
DAX | Request for extension of the european patent (deleted) | ||
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
RIN1 | Information on inventor provided before grant (corrected) |
Inventor name: BEGUINOT, JEAN Inventor name: BRISSON, JEAN-GEORGES |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: FRENCH |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: RO Ref legal event code: EPE |
|
REF | Corresponds to: |
Ref document number: 60318478 Country of ref document: DE Date of ref document: 20080214 Kind code of ref document: P |
|
REG | Reference to a national code |
Ref country code: SE Ref legal event code: TRGR |
|
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 20080405 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2298605 Country of ref document: ES Kind code of ref document: T3 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20080102 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20080402 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20080602 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FD4D |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20080102 Ref country code: IE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20080102 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed |
Effective date: 20081003 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20080102 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20081130 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20080102 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20081130 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20081130 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20080703 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20080403 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R081 Ref document number: 60318478 Country of ref document: DE Owner name: INDUSTEEL FRANCE, FR Free format text: FORMER OWNER: INDUSTEEL CREUSOT, PUTEAUX, FR |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: PC Ref document number: 382716 Country of ref document: AT Kind code of ref document: T Owner name: INDUSTEEL FRANCE, FR Effective date: 20150608 Ref country code: NL Ref legal event code: SD Effective date: 20150706 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: PC2A Owner name: INDUSTEEL FRANCE Effective date: 20150716 Ref country code: GB Ref legal event code: 732E Free format text: REGISTERED BETWEEN 20150625 AND 20150701 |
|
REG | Reference to a national code |
Ref country code: SI Ref legal event code: SP73 Owner name: INDUSTEEL FRANCE; FR Effective date: 20150701 |
|
REG | Reference to a national code |
Ref country code: SK Ref legal event code: PC4A Ref document number: E 3186 Country of ref document: SK Owner name: INDUSTEEL FRANCE, SAINT DENIS, FR Free format text: FORMER OWNER: INDUSTEEL CREUSOT, SAINT DENIS, FR Effective date: 20150821 Ref country code: SK Ref legal event code: TE4A Ref document number: E 3186 Country of ref document: SK Owner name: INDUSTEEL CREUSOT, SAINT DENIS, FR Effective date: 20150821 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: TP Owner name: INDUSTEEL FRANCE, FR Effective date: 20150910 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 13 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 14 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 15 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 16 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: NL Payment date: 20221020 Year of fee payment: 20 Ref country code: FR Payment date: 20221021 Year of fee payment: 20 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: TR Payment date: 20221031 Year of fee payment: 20 Ref country code: SK Payment date: 20221026 Year of fee payment: 20 Ref country code: SE Payment date: 20221024 Year of fee payment: 20 Ref country code: RO Payment date: 20221107 Year of fee payment: 20 Ref country code: LU Payment date: 20221020 Year of fee payment: 20 Ref country code: IT Payment date: 20221020 Year of fee payment: 20 Ref country code: GB Payment date: 20221021 Year of fee payment: 20 Ref country code: ES Payment date: 20221201 Year of fee payment: 20 Ref country code: DE Payment date: 20220616 Year of fee payment: 20 Ref country code: CZ Payment date: 20221025 Year of fee payment: 20 Ref country code: AT Payment date: 20221024 Year of fee payment: 20 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: SI Payment date: 20221026 Year of fee payment: 20 Ref country code: BE Payment date: 20221020 Year of fee payment: 20 |
|
P01 | Opt-out of the competence of the unified patent court (upc) registered |
Effective date: 20230522 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R071 Ref document number: 60318478 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: MK Effective date: 20231112 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FD2A Effective date: 20231124 |
|
REG | Reference to a national code |
Ref country code: BE Ref legal event code: MK Effective date: 20231113 |
|
REG | Reference to a national code |
Ref country code: SK Ref legal event code: MK4A Ref document number: E 3186 Country of ref document: SK Expiry date: 20231113 Ref country code: GB Ref legal event code: PE20 Expiry date: 20231112 |
|
REG | Reference to a national code |
Ref country code: SE Ref legal event code: EUG |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MK07 Ref document number: 382716 Country of ref document: AT Kind code of ref document: T Effective date: 20231113 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SK Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20231113 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20231112 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: ES Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20231114 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SK Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20231113 Ref country code: SI Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20231114 Ref country code: GB Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20231112 Ref country code: ES Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20231114 Ref country code: CZ Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20231113 |