EP1563103B1 - Method for making an abrasion resistant steel plate and steel plate obtained - Google Patents
Method for making an abrasion resistant steel plate and steel plate obtained Download PDFInfo
- Publication number
- EP1563103B1 EP1563103B1 EP03782550A EP03782550A EP1563103B1 EP 1563103 B1 EP1563103 B1 EP 1563103B1 EP 03782550 A EP03782550 A EP 03782550A EP 03782550 A EP03782550 A EP 03782550A EP 1563103 B1 EP1563103 B1 EP 1563103B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- optionally
- plate
- steel
- titanium
- process according
- 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 44
- 239000010959 steel Substances 0.000 title claims description 44
- 238000005299 abrasion Methods 0.000 title claims description 27
- 238000000034 method Methods 0.000 title claims description 13
- 239000010936 titanium Substances 0.000 claims description 54
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 30
- 229910052719 titanium Inorganic materials 0.000 claims description 28
- 229910000734 martensite Inorganic materials 0.000 claims description 18
- 238000001816 cooling Methods 0.000 claims description 17
- 229910052799 carbon Inorganic materials 0.000 claims description 14
- 150000001247 metal acetylides Chemical class 0.000 claims description 14
- 239000000203 mixture Substances 0.000 claims description 14
- 229910001566 austenite Inorganic materials 0.000 claims description 13
- 239000000126 substance Substances 0.000 claims description 10
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 8
- 238000004519 manufacturing process Methods 0.000 claims description 7
- 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
- 238000010438 heat treatment Methods 0.000 claims description 5
- 239000012535 impurity Substances 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
- 239000010949 copper Substances 0.000 claims description 4
- 229910052742 iron Inorganic materials 0.000 claims description 4
- 229910052745 lead Inorganic materials 0.000 claims description 4
- 238000005496 tempering Methods 0.000 claims description 4
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 238000005096 rolling process Methods 0.000 claims description 3
- 239000002893 slag Substances 0.000 claims description 3
- 238000003303 reheating Methods 0.000 claims description 2
- 238000003723 Smelting Methods 0.000 claims 2
- 229910052726 zirconium Inorganic materials 0.000 description 23
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 16
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 14
- -1 zirconium carbides Chemical class 0.000 description 14
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 13
- 239000011651 chromium Substances 0.000 description 11
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 10
- 230000015572 biosynthetic process Effects 0.000 description 9
- 229910052750 molybdenum Inorganic materials 0.000 description 9
- 239000010955 niobium Substances 0.000 description 9
- 230000009466 transformation Effects 0.000 description 9
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 8
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 8
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 7
- 240000008042 Zea mays Species 0.000 description 7
- 229910001563 bainite Inorganic materials 0.000 description 7
- 229910052804 chromium Inorganic materials 0.000 description 7
- 239000011572 manganese Substances 0.000 description 7
- 239000011733 molybdenum Substances 0.000 description 7
- 229910052759 nickel Inorganic materials 0.000 description 7
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 6
- 230000000694 effects Effects 0.000 description 6
- 229910052748 manganese Inorganic materials 0.000 description 5
- 239000011669 selenium Substances 0.000 description 5
- 229910052721 tungsten Inorganic materials 0.000 description 5
- 229910052757 nitrogen Inorganic materials 0.000 description 4
- 238000001556 precipitation Methods 0.000 description 4
- 230000000717 retained effect Effects 0.000 description 4
- 229910052717 sulfur Inorganic materials 0.000 description 4
- 239000011593 sulfur Substances 0.000 description 4
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 4
- 239000010937 tungsten Substances 0.000 description 4
- 241001080024 Telles Species 0.000 description 3
- 230000008901 benefit Effects 0.000 description 3
- 230000002349 favourable effect Effects 0.000 description 3
- 230000001965 increasing effect Effects 0.000 description 3
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 3
- 230000008961 swelling Effects 0.000 description 3
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 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
- 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
- 229910052796 boron Inorganic materials 0.000 description 2
- 229910052791 calcium Inorganic materials 0.000 description 2
- 239000011575 calcium Substances 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 238000005098 hot rolling Methods 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
- 239000011159 matrix material Substances 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 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
- PORWMNRCUJJQNO-UHFFFAOYSA-N tellurium atom Chemical compound [Te] PORWMNRCUJJQNO-UHFFFAOYSA-N 0.000 description 2
- 239000004411 aluminium Substances 0.000 description 1
- 238000004873 anchoring Methods 0.000 description 1
- 230000008859 change 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
- 238000002788 crimping Methods 0.000 description 1
- 230000000254 damaging effect Effects 0.000 description 1
- 230000002542 deteriorative effect Effects 0.000 description 1
- 229940082150 encore Drugs 0.000 description 1
- 239000004333 gold (food color) Substances 0.000 description 1
- 239000008187 granular material Substances 0.000 description 1
- 210000002216 heart Anatomy 0.000 description 1
- 230000006872 improvement 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
- 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
- 230000009467 reduction Effects 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
- 238000003466 welding Methods 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
- C22C38/58—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
- 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
- C22C38/18—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
- C22C38/50—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
- 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.
- quenching may be followed by tempering at a temperature below 350 ° C, and preferably below 250 ° C.
- the hardness is between 280 HB and 450 HB.
- VS * VS - Ti / 4 - Zr / 8 + 7 ⁇ NOT / 8 ⁇ 0 , 095 %
- the chemical composition is chosen so that the quenchability of the steel is sufficient, given the thickness of the sheet that is to be manufactured.
- the steel is made, cast in the form of a 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 in the hot rolling or later, possibly after a cold or mid-heat planing.
- the sheets A to D have a martensite-bainitic self-regenerating structure containing about 10% retained austenite, as well as titanium carbides, while the plates E to G have a completely martensitic structure, the sheets G and H also containing large titanium carbides.
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)
- Heat Treatment Of Articles (AREA)
- Treatment Of Steel In Its Molten State (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 pour abrasion de dureté voisine de 400 Brinell, contenant environ 0,15% de carbone ainsi que du manganèse, du nickel, du chrome et du molybdène, en des teneurs inférieures à quelques % pour avoir une trempabilité suffisante. Ces aciers sont trempés de façon à avoir une structure entièrement martensitique. Ils ont l'avantage d'être relativement faciles à mettre en oeuvre par soudage, découpage ou pliage. Mais ils ont l'inconvénient d'avoir une résistance à l'abrasion limitée. Il est certes connu d'augmenter la résistance à l'abrasion en augmentant la teneur en carbone et donc la dureté. Mais cette façon de procéder a l'inconvénient de détériorer l'aptitude à la mise en oeuvre.Abrasive steels of hardness close to 400 Brinell containing about 0.15% of carbon as well as manganese, nickel, chromium and molybdenum are known at levels of less than a few% in order to have sufficient quenchability. These steels are soaked so as to have a completely martensitic structure. They have the advantage of being relatively easy to implement by welding, cutting or folding. But they have the disadvantage of having a limited resistance to abrasion. It is certainly known to increase the resistance to abrasion by increasing the carbon content and therefore the hardness. But this procedure has the disadvantage of deteriorating the ability to implement.
Le but de la présente invention est de remédier à ces inconvénients, en proposant une tôle en acier résistant à l'abrasion qui, toutes choses égales par ailleurs, présente une résistance à l'abrasion meilleure que celle des aciers connus ayant une dureté de 400 Brinell, tout en ayant une aptitude à la mise en oeuvre comparable à celle de ces aciers.The object of the present invention is to overcome these disadvantages by providing an abrasion-resistant steel sheet which, all things being equal, has a better abrasion resistance than that of known steels having a hardness of 400. Brinell, while having an applicability comparable to that of these steels.
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 :
0,1% ≤ C < 0,23%
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%
0,05% ≤ Mo +W/2 ≤ 1%
0% ≤ Cu ≤ 1,5%
0% ≤ B ≤ 0,02%
0% ≤ Ti ≤ 0,67%
0% ≤ Zr ≤ 1,34%
0,05% < Ti + Zr/2 ≤ 0,67%
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 %,
et :
et :
avec : K = 1 si B ≥ 0,0005% et K = 0 si B < 0,0005%,
l'acier ayant une structure constituée de martensite ou d'un mélange de martensite et de bainite auto-revenue, ladite structure contenant en outre des carbures et de 5% à 20% d'austénite.
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 T = 800 - 270xC* - 90xMn -37xNi - 70XCr - 83x(Mo + W/2), et T-50°C environ, 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.
0.1% ≤ C <0.23%
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%
0.05% ≤ Mo + W / 2 ≤ 1%
0% ≤ Cu ≤ 1.5%
0% ≤ B ≤ 0.02%
0% ≤ Ti ≤ 0.67%
0% ≤ Zr ≤ 1.34%
0.05% <Ti + Zr / 2 ≤ 0.67%
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%,
and
and
with: K = 1 if B ≥ 0.0005% and K = 0 if B <0.0005%,
the steel having a structure consisting of martensite or a mixture of martensite and self-tempering bainite, said structure further containing carbides and 5% to 20% austenite.
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:
- cool the workpiece or sheet at an average cooling rate greater than 0.5 ° C / s between a temperature above AC 3 and a temperature T = 800 - 270xC * - 90xMn -37xNi - 70XCr - 83x (Mo + W / 2), and T-50 ° C approximately, 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 de 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 tôle, selon la revendication 8. La tôle obtenue notamment par ce procédé, présente une planéité caractérisée par une flèche inférieure ou égale à 12mm/m et de préférence inférieure à 5mm/m, l'acier ayant une structure constituée de 5% à 20% d'austénite retenue, le reste de la structure étant martensitique ou martensito-bainitique, et contient des carbures. L'épaisseur de la tôle peut être comprise entre 2 mm et 150 mm.The invention also relates to a part, in particular sheet metal, according to claim 8. The sheet obtained in particular by this method has a flatness characterized by an arrow less than or equal to 12 mm / m and preferably less than 5 mm / m, the steel having a structure consisting of 5% to 20% retained austenite, the remainder of the structure being martensitic or martensite-bainitic, and contains carbides. The thickness of the sheet may be between 2 mm and 150 mm.
De préférence, la dureté est comprise entre 280 HB et 450 HB.Preferably, the hardness is between 280 HB and 450 HB.
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 :
- plus de 0,1% de carbone de façon à avoir une dureté suffisante et afin de permettre la formation de carbures, mais moins de 0,23%, et de préférence moins de 0,22%, pour que l'aptitude au soudage et au découpage soit bonne.
- de 0% à 0,67% de titane et de 0% à 1,34% de zirconium, ces teneurs devant êtres telles que la somme Ti+Zr/2 soit supérieure à 0,05%, de préférence supérieure à 0,1%, et mieux encore, supérieure à 0,2%, pour que l'acier contienne des gros carbures de titane ou de zirconium qui augmentent la résistance à l'abrasion. Mais la somme Ti+Zr/2 doit rester inférieure à 0,67% car, au-delà, l'acier ne contiendrait pas assez de carbone libre pour que sa dureté soit suffisante. Par ailleurs la teneur Ti +Zr/2 sera préférentiellement inférieure à 0,50% ou mieux 0,40% voire 0,30 % si l'on a besoin de privilégier la ténacité du matériau.
- 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% ou mieux, supérieure à 0,8%. 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.
- 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 favorables à la résistance à l'abrasion.
- 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 0,05% et 1%, et de préférence reste inférieure à 0,8%, ou mieux, inférieure à 0,5%. Ces éléments augmentent la trempabilité et, forment dans la martensite ou dans la bainite de fins carbures durcissants, 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 les carbures 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 pas 0,03%, et reste en général inférieure à 0,025%. L'azote 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.
- more than 0.1% carbon so as to have sufficient hardness and to permit the formation of carbides, but less than 0.23%, and preferably less than 0.22%, so that the weldability and the cutting is good.
- from 0% to 0.67% of titanium and from 0% to 1.34% of zirconium, these contents being such that the sum Ti + Zr / 2 is greater than 0.05%, preferably greater than 0.1. %, and more preferably greater than 0.2%, for the steel to contain large titanium or zirconium carbides which increase the abrasion resistance. But the sum Ti + Zr / 2 must remain below 0.67% because, beyond, the steel would not contain enough free carbon for its hardness is sufficient. Moreover, the Ti + Zr / 2 content will preferably be less than 0.50% or better still 0.40% or even 0.30% if it is necessary to favor the toughness of the material.
- 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% or better, greater than 0.8%. These elements, which are deoxidizing agents, also have the effect of favoring the obtaining of a metastable retained austenite highly loaded with carbon, the transformation of which in martensite is accompanied by a large swelling favoring the anchoring of the titanium carbides.
- 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 favorable to abrasion resistance.
- From 0% (or traces) to 1% molybdenum and 0% (or traces) at 2% tungsten, the sum Mo + W / 2 being between 0.05% and 1%, and preferably remains less than 0.8%, or better, less than 0.5%. These elements increase the quenchability and form in martensite or bainite thin carbides hardening, including self-precipitation 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 the carbides 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. It should be noted that when the steel contains Se and / or Te, the manganese content must be sufficient in view of the sulfur content so that selenides or tellurides of manganese can be formed.
- 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 method but does not exceed 0.03%, and remains generally less than 0.025%. Nitrogen can react with titanium or zirconium to form nitrides that should not be too big to 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 sont choisies telles que :
Et de préférence, C* ≥ 0,12% pour avoir une dureté plus élevée et donc une meilleure résistance à l'abrasion. La grandeur 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 supérieure à 0,095% pour avoir une structure martensitique ou martensito-bainitique ayant une dureté suffisante.And preferably C * ≥ 0.12% to have a higher hardness and therefore a better abrasion resistance. The quantity 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% to have a martensitic or martensite-bainitic structure having a sufficient hardness.
Compte tenu de la formation possible de nitrures de titane ou de zirconium, pour que la quantité de carbures de titane ou de zirconium soit suffisante, les teneurs en Ti, Zr et N doivent être telles que :
De plus, la composition chimique est 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:
avec : K = 1 si B ≥ 0,0005% et K = 0 si B < 0,0005%,In addition, the chemical composition is chosen so that the quenchability of the steel is sufficient, given the thickness of the sheet that is to be manufactured. For this, the chemical composition must satisfy the relation:
with: K = 1 if B ≥ 0.0005% and K = 0 if B <0.0005%,
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. En outre, cette structure comprend des gros carbures de titane ou de zirconium formés à haute température, et éventuellement des carbures de niobium, de tantale ou de vanadium. Du fait du procédé de fabrication qui sera décrit plus loin, cette structure est revenue, si bien qu'elle comporte également des carbures de molybdène ou de tungstène et éventuellement des carbures de chrome.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. In addition, this structure comprises large titanium or zirconium carbides formed at high temperature, and optionally carbides of niobium, tantalum or vanadium. Due to the manufacturing process that will be described later, this structure is returned, so that it also includes molybdenum carbides or tungsten and possibly chromium carbides.
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.The inventors have found that the effectiveness of large carbides for the improvement of 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 moyenne à coeur 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), on réduisait les contraintes résiduelles engendrées par les changements de phase. Ce refroidissement ralenti dans le domaine bainito-martensitique a, en outre, l'avantage de provoquer un auto-revenu qui engendre la formation de carbures de molybdène, de tungstène ou de chrome et améliore la tenue à l'usure de la matrice entourant les gros carbures.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 an average cooling rate at core Vr <1150 × ep -1.7 (in this formula, ep is the thickness of the sheet expressed in mm, and the speed of cooling is expressed in ° C / s) below a temperature T = 800 - 270xC * - 90xMn -37xNi - 70XCr - 83x (Mo + W / 2), (expressed in ° C), the residual stresses generated were reduced by phase changes. This cooling slowed in the bainito-martensitic field has, in addition, the advantage of causing a self-income which generates the formation of carbides of molybdenum, tungsten or chromium and improves the wear resistance of the matrix surrounding the big carbides.
Pour fabriquer une tôle bien plane ayant une bonne résistance à l'abrasion et une bonne aptitude à la mise en oeuvre, 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 dans la chaude de laminage ou ultérieurement, éventuellement après un planage à froid ou à mi-chaud.In order to manufacture a flat sheet having good abrasion resistance and good processability, the steel is made, cast in the form of a 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 in the hot rolling or later, possibly after a cold or mid-heat planing.
Dans tous les cas, pour réaliser le traitement thermique :
- on chauffe l'acier au-dessus du point AC3 de façon à lui conférer une structure entièrement austénitique, dans laquelle cependant subsistent des carbures de titane ou de zirconium,
- puis on le refroidit à une vitesse de refroidissement moyenne à coeur supérieure à la vitesse critique de transformation bainitique jusqu'à une température comprise entre T = 800 - 270xC* - 90xMn -37xNi - 70XCr - 83x(Mo + W/2), et T-50°C, environ, de façon à éviter la formation de constituants ferrito-perlitiques, pour cela, il suffit en général de refroidir à une vitesse supérieure à 0,5°C/s,
- puis, entre la température ainsi définie (c'est à dire comprise entre T et T-50°C environ) et 100°C environ, on refroidit la tôle à une vitesse de refroidissement moyenne à coeur Vr inférieure à 1150xep-1,7, et supérieure à 0,1°C/s, 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.
- the steel is heated above the point AC 3 so as to give it a completely austenitic structure, in which, however, titanium or zirconium carbides remain,
- then cooled to an average core cooling rate above the critical bainitic transformation rate to a temperature of between T = 800 - 270xC * - 90xMn -37xNi - 70XCr - 83x (Mo + W / 2), and T-50 ° C, approximately, so as to avoid the formation of ferrito-pearlitic constituents, for this, it is generally sufficient to cool at a speed greater than 0.5 ° C / s,
- then, between the temperature thus defined (that is to say between about T and T-50 ° C) and about 100 ° C, the sheet is cooled to an average cooling rate Vr heart less than 1150xep -1.7 , and greater than 0.1 ° C / s, to obtain the desired structure,
- and the sheet is cooled to room temperature, preferably, but not required, 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 a tempering at a temperature of less than or equal to 350 ° C, and preferably less than 250 ° C, can be carried out.
Par vitesse de refroidissement moyenne, on entend la vitesse de refroidissement égale à la différence entre les températures de début et de fin de refroidissement divisée par le temps de refroidissement entre ces deux températures.By average cooling rate is meant the cooling rate equal to the difference between the start and end temperatures of cooling divided by the cooling time between these two temperatures.
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 3 mm par mètre sans planage ou avec un planage modéré. La tôle a une dureté comprise entre 280HB et 450HB. Cette dureté dépend principalement de la teneur en carbone libre C* = C - Ti/4 - Zr/8 + 7xN/8. Plus la teneur en carbone libre est élevée, plus la dureté est importante. Plus la teneur en carbone libre est faible, plus la mise en oeuvre est facile. A teneur égale en carbone libre, plus la teneur en titane est élevée, plus la résistance à l'abrasion est bonne.This gives a sheet, whose thickness can be between 2 mm and 150 mm, having excellent flatness characterized by an arrow less than 3 mm per meter without planing or with moderate planing. The sheet has a hardness between 280HB and 450HB. This hardness depends mainly on the free carbon content C * = C - Ti / 4 - Zr / 8 + 7xN / 8. The higher the free carbon content, the greater the hardness. The lower the free carbon content, the more work is easy. At equal free carbon content, the higher the titanium content, the better the abrasion resistance.
A titre d'exemple, on considère des tôles de 30mm d'épaisseur en acier, repérées A, B, C et D selon l'invention, E et F selon l'art antérieur et G et H donnés à titre de comparaison. Les compositions chimiques des aciers, exprimées en 10-3 % en poids, ainsi que la dureté et un indice de résistance à l'usure Rus, sont reportées au tableau 1.
La résistance à l'usure des aciers est mesurée par la perte de poids d'une éprouvette prismatique mise en rotation dans un bac contenant des granulats calibrés de quartzite pendant un temps de 5 heures.The wear resistance of the steels is measured by the weight loss of a prismatic specimen rotated in a tank containing calibrated granules of quartzite for a period of 5 hours.
L'indice de résistance à l'usure Rus d'un acier est le rapport de la résistance à l'usure de l'acier F, pris à titre de référence, et la résistance à l'usure de l'acier considéré.The wear resistance index Rus of a steel is the ratio of the wear resistance of the steel F, taken as a reference, to the wear resistance of the steel under consideration.
Les tôles A à H sont austénitisées à 900°C.The sheets A to H are austenitized at 900 ° C.
Après austénitisation :
- la tôle en acier A est refroidie à une vitesse moyenne de 0,7°C/s au dessus de la température T définie plus haut (environ 460°C), et à une vitesse moyenne de 0,13°C/s en dessous, conformément à l'invention;
- les tôles en aciers B, C, D, sont refroidie à une vitesse moyenne de 6°C/s au dessus de la température T définie plus haut (environ 470°C), et à une vitesse moyenne de 1,4°C/s en dessous, conformément à l'invention ;
- les tôles en acier E, F, G et H, données à titre de comparaison, ont été refroidies à une vitesse moyenne de 20°C/s au dessus de la température T définie plus haut, et à une vitesse moyenne de 12°C/s en dessous.
- the steel sheet A is cooled at an average speed of 0.7 ° C / s above the temperature T defined above (about 460 ° C), and at an average speed of 0.13 ° C / s below according to the invention;
- the steel sheets B, C, D are cooled at an average speed of 6 ° C / s above the temperature T defined above (about 470 ° C), and at an average speed of 1.4 ° C / s below, according to the invention;
- the steel sheets E, F, G and H, given by way of comparison, were cooled at an average speed of 20 ° C./s above the temperature T defined above, and at an average speed of 12 ° C. / s below.
Les tôles A à D ont une structure martensito-bainitique auto-revenue contenant environ 10% d'austénite retenue, ainsi que des carbures de titane, alors que les tôles E à G ont une structure entièrement martensitique, les tôles G et H contenant également de gros carbures de titane.The sheets A to D have a martensite-bainitic self-regenerating structure containing about 10% retained austenite, as well as titanium carbides, while the plates E to G have a completely martensitic structure, the sheets G and H also containing large titanium carbides.
On peut constater que, bien qu'ayant des duretés inférieures à celles des tôles E et F, les tôles A, B, C et D ont des résistances à l'abrasion sensiblement meilleures. Les plus faibles duretés qui correspondent, pour l'essentiel à des teneurs en carbone libre plus faibles, conduisent à de meilleures aptitudes à la mise en oeuvre.It can be seen that, although having hardnesses less than those of the E and F sheets, the sheets A, B, C and D have substantially better abrasion resistance. The lower hardnesses, which essentially correspond to lower free carbon contents, lead to better processability.
La comparaison des exemples C, D, F, G et H montrent que l'augmentation de la résistance à l'abrasion ne résulte pas simplement de l'addition de titane, mais de la combinaison de l'addition de titane et de la structure contenant de l'austénite résiduelle. En effet, on peut constater que les aciers F, G et H dont la structure ne comporte pas d'austénite résiduelle ont des tenues à l'abrasion assez comparables, alors que les aciers C et D qui contiennent de l'austénite résiduelle ont des tenues à l'abrasion sensiblement meilleures.Comparison of Examples C, D, F, G and H shows that the increase in abrasion resistance does not result simply from the addition of titanium, but from the combination of titanium addition and structure. containing residual austenite. In fact, it can be seen that the steels F, G and H, the structure of which does not contain residual austenite, have fairly comparable abrasion resistance, whereas the steels C and D which contain residual austenite have significantly better abrasion.
En outre, la comparaison des couples G et H d'une part et C et D d'autre part, montrent que la présence d'austénite résiduelle augmente sensiblement l'efficacité du titane. Pour les exemples C et D, le passage de 0,110% à 0,350% de titane se traduit par une augmentation de la tenue à l'abrasion de 56%, alors que pour les aciers G et H, l'augmentation n'est que de 37%.In addition, the comparison of the pairs G and H on the one hand and C and D on the other hand, show that the presence of residual austenite significantly increases the efficiency of the titanium. For Examples C and D, the change from 0.110% to 0.350% titanium results in an increase in abrasion resistance of 56%, whereas for G and H steels, the increase is only 37%.
Cette observation est attribuable à l'effet de sertissage accru des carbures de titane par la matrice environnante, quand celle-ci contient de l'austénite résiduelle susceptible de se transformer en martensite dure et gonflante en service.This observation is attributable to the increased crimping effect of titanium carbides by the surrounding matrix, when it contains residual austenite that can turn into hard, swelling martensite in service.
Par ailleurs, la déformation après refroidissement, sans planage, pour les tôles en acier A ou B sont de 6 mm/m et de 17 mm/m pour les tôles en acier E et F. Ces résultats montrent la réduction de déformation des produits obtenus grâce à l'invention.In addition, the deformation after cooling, without planing, for steel sheets A or B are 6 mm / m and 17 mm / m for steel sheets E and F. These results show the reduction of deformation of the products obtained. thanks to the invention.
Il en résulte que, en pratique, en fonction du degré d'exigence en planéité des utilisateurs,
- soit, on peut livrer les produits sans planage (gain sur le coût et sur les contraintes résiduelles),
- soit, on peut réaliser un planage pour satisfaire une exigence de planéité plus sévère' (par exemple 5mm/m) mais plus facilement et en introduisant moins de contraintes du fait de la déformation originelle moindre sur les produits selon l'invention.
- either, one can deliver the products without planing (gain on the cost and on the residual stresses),
- either, one can carry out planing to satisfy a requirement of flatness more severe '(for example 5mm / m) but more easily and by introducing less constraints due to the original deformation less on the products according to the invention.
Claims (13)
- Process for manufacturing a part, and especially a plate, made of an abrasion-resistant steel, the chemical composition of which comprises, by weight:
0.1% ≤ C < 0.23%
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%
0.05% ≤ Mo +W/2 ≤ 1%
0% ≤ B ≤ 0.02%
0% ≤ Ti ≤ 0.67%
0% ≤ Zr ≤ 1.34%
0.05% ≤ Ti +Zr/2 ≤ 0.67%
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:
and
and
where K = 1 if B ≥ 0.0005% and K = 0 if B < 0.0005%,
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 - 270xC* - 90xMn - 37xNi - 70xCr - 83x(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 or equal to 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 or Claim 2, further
characterized in that:
C ≤ 0.22%
and
C* ≥ 0.12%.
- Process according to any one of Claims 1 to 3, further characterized in that:
Ti + Zr/2 ≥ 0.10%.
- Process according to any one of Claims 1 to 4, further 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:
0.1% ≤ C < 0.23%
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%
0.05% ≤ Mo +W/2 ≤ 1%
0% ≤ B ≤ 0.02%
0% ≤ Ti ≤ 0.67%
0% ≤ Zr ≤ 1.34%
0.05% ≤ Ti +Zr/2 ≤ 0.67%
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:
and
and
where K = 1 if B ≥ 0.0005% and K = 0 if B < 0.0005%,
the steel having a martensitic or martensitic-bainitic structure, said structure containing carbides and 5% to 20% residual austenite. - Part according to any one of Claims 8 to 10, characterized in that:
Ti + Zr/2 ≥ 0.10%.
- 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 the thickness of the plate is between 2 mm and 150 mm.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SI200331177T SI1563103T1 (en) | 2002-11-19 | 2003-11-13 | Method for making an abrasion resistant steel plate and steel plate obtained |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0214425 | 2002-11-19 | ||
FR0214425A FR2847271B1 (en) | 2002-11-19 | 2002-11-19 | METHOD FOR MANUFACTURING AN ABRASION RESISTANT STEEL SHEET AND OBTAINED SHEET |
PCT/FR2003/003357 WO2004048618A1 (en) | 2002-11-19 | 2003-11-13 | Method for making an abrasion resistant steel plate and steel plate obtained |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1563103A1 EP1563103A1 (en) | 2005-08-17 |
EP1563103B1 true EP1563103B1 (en) | 2008-03-05 |
Family
ID=32187696
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP03782550A Expired - Lifetime EP1563103B1 (en) | 2002-11-19 | 2003-11-13 | Method for making an abrasion resistant steel plate and steel plate obtained |
Country Status (20)
Country | Link |
---|---|
US (2) | US7462251B2 (en) |
EP (1) | EP1563103B1 (en) |
JP (1) | JP4535875B2 (en) |
KR (1) | KR101010593B1 (en) |
CN (1) | CN100348739C (en) |
AR (1) | AR042072A1 (en) |
AT (1) | ATE388247T1 (en) |
AU (1) | AU2009201117B8 (en) |
BR (1) | BR0315694B1 (en) |
CA (1) | CA2506347C (en) |
DE (1) | DE60319567T2 (en) |
ES (1) | ES2300636T3 (en) |
FR (1) | FR2847271B1 (en) |
PE (1) | PE20040486A1 (en) |
PL (1) | PL203154B1 (en) |
PT (1) | PT1563103E (en) |
RU (1) | RU2326180C2 (en) |
UA (1) | UA81134C2 (en) |
WO (1) | WO2004048618A1 (en) |
ZA (1) | ZA200504151B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102199737A (en) * | 2010-03-26 | 2011-09-28 | 宝山钢铁股份有限公司 | 600HB-grade wear resistant steel plate and its manufacturing method |
Families Citing this family (55)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2847272B1 (en) * | 2002-11-19 | 2004-12-24 | Usinor | METHOD FOR MANUFACTURING AN ABRASION RESISTANT STEEL SHEET AND OBTAINED SHEET |
CN100419114C (en) * | 2004-11-14 | 2008-09-17 | 林海 | Antiwear alloy |
EP1990431A1 (en) | 2007-05-11 | 2008-11-12 | ArcelorMittal France | Method of manufacturing annealed, very high-resistance, cold-laminated steel sheets, and sheets produced thereby |
US8444776B1 (en) | 2007-08-01 | 2013-05-21 | Ati Properties, Inc. | High hardness, high toughness iron-base alloys and methods for making same |
KR101873582B1 (en) | 2007-08-01 | 2018-08-02 | 에이티아이 프로퍼티즈 엘엘씨 | High hardness, high toughness iron-base alloys and methods for making same |
TWI341332B (en) * | 2008-01-07 | 2011-05-01 | Nippon Steel Corp | Wear-resistant steel sheet having excellent wear resistnace at high temperatures and excellent bending workability and method for manufacturing the same |
SI2103704T1 (en) * | 2008-03-10 | 2012-11-30 | Swiss Steel Ag | Hot-rolled long product and method for its manufacture |
EP2123787A1 (en) * | 2008-05-06 | 2009-11-25 | Industeel Creusot | High-grade steel for massive parts. |
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 |
CN102127705B (en) * | 2010-01-12 | 2013-07-17 | 宝山钢铁股份有限公司 | High-strength high-hardness wear-resistant steel |
EP2374910A1 (en) * | 2010-04-01 | 2011-10-12 | ThyssenKrupp Steel Europe AG | Steel, flat, steel product, steel component and method for producing a steel component |
FR2958660B1 (en) * | 2010-04-07 | 2013-07-19 | Ascometal Sa | STEEL FOR MECHANICAL PIECES WITH HIGH CHARACTERISTICS AND METHOD FOR MANUFACTURING THE SAME. |
CN101880831B (en) * | 2010-06-13 | 2012-07-04 | 东北大学 | High-strength-and-toughness low alloy wear resistant steel and manufacturing method thereof |
CN102312174B (en) * | 2010-06-29 | 2013-07-31 | 鞍钢股份有限公司 | Non-quenched and tempered high-strength wear-resistant steel and production method thereof |
US9182196B2 (en) | 2011-01-07 | 2015-11-10 | Ati Properties, Inc. | Dual hardness steel article |
RU2466193C1 (en) * | 2011-05-18 | 2012-11-10 | Общество с ограниченной ответственностью "Северсталь-Проект" (ООО "Северсталь-Проект") | Manufacturing method of thick low-alloy rolled plates |
US9657363B2 (en) | 2011-06-15 | 2017-05-23 | Ati Properties Llc | Air hardenable shock-resistant steel alloys, methods of making the alloys, and articles including the alloys |
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 |
KR20150065619A (en) * | 2012-05-25 | 2015-06-15 | 개리 엠 콜라 | Microtreatment and microstructure of carbide containing iron-based alloy |
RU2495142C1 (en) * | 2012-06-26 | 2013-10-10 | Общество с ограниченной ответственностью "Северсталь-Проект" (ООО "Северсталь-Проект") | Manufacturing method of rolled steel plate from low-alloy steel |
CN103898419B (en) * | 2012-12-25 | 2017-05-17 | 隆英(常州)特钢科技有限公司 | Wear-resisting steel plate and manufacturing method thereof |
CN104109817A (en) * | 2013-04-18 | 2014-10-22 | 曹志春 | High-tungsten-titanium wear-resistant alloy steel |
US9738334B2 (en) * | 2013-05-07 | 2017-08-22 | Arcelormittal | Track shoe having increased service life useful in a track drive system |
MX2015016224A (en) * | 2013-06-07 | 2016-03-01 | Nippon Steel & Sumitomo Metal Corp | Heat-treated steel material and method for producing same. |
RU2530078C1 (en) * | 2013-07-23 | 2014-10-10 | Открытое акционерное общество "Северсталь" (ОАО "Северсталь") | Production of thick-sheet rolled stock for ship building |
KR20150061516A (en) * | 2013-11-27 | 2015-06-04 | 두산중공업 주식회사 | Mold Steel and Manufacturing Method Thereof |
KR101828199B1 (en) * | 2014-01-28 | 2018-02-09 | 제이에프이 스틸 가부시키가이샤 | Abrasion-resistant steel plate and method for manufacturing the same |
RU2544216C1 (en) * | 2014-04-08 | 2015-03-10 | Юлия Алексеевна Щепочкина | Steel |
RU2561558C1 (en) * | 2014-09-15 | 2015-08-27 | 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-nickel steel |
RU2556442C1 (en) * | 2014-10-21 | 2015-07-10 | Юлия Алексеевна Щепочкина | Steel |
CN104498831B (en) * | 2014-10-26 | 2017-02-15 | 驻马店市三山耐磨材料有限公司 | Low-carbon medium-chromium alloy steel wear-resistant liner plate special for wet grinding machine |
CN104451453A (en) * | 2014-11-14 | 2015-03-25 | 无锡信大气象传感网科技有限公司 | Wear-resistant alloy steel material for fan blades of wind-driven generator |
CN104846298A (en) * | 2015-04-21 | 2015-08-19 | 苏州劲元油压机械有限公司 | Manufacturing technology of layered overflow valve |
CN104846299A (en) * | 2015-04-22 | 2015-08-19 | 苏州劲元油压机械有限公司 | Manufacturing process of high pressure-resistant overflow valve |
CN104911509A (en) * | 2015-04-23 | 2015-09-16 | 苏州劲元油压机械有限公司 | Making technology of guiding overflow valve |
CN104911508A (en) * | 2015-04-23 | 2015-09-16 | 苏州劲元油压机械有限公司 | Making technology of bearing pedestal for heavy-duty oil hydraulic cylinders |
US10400320B2 (en) | 2015-05-15 | 2019-09-03 | Nucor Corporation | Lead free steel and method of manufacturing |
RU2586949C1 (en) * | 2015-06-08 | 2016-06-10 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Южно-Уральский государственный университет" (национальный исследовательский университет) (ФГБОУ ВПО "ЮУрГУ" (НИУ)) | Martensite-ferrite corrosion-resistant chrome-nickel steel with improved machinability |
CN106591731B (en) * | 2015-10-15 | 2019-02-15 | 无锡欣誉户外用品有限公司 | A kind of large size semi-autogenous mill shell liner alloy material |
CN105568142B (en) * | 2016-03-09 | 2017-07-28 | 桂林电子科技大学 | A kind of high-obdurability low-alloy abrasion-resistant stee excavator bucket teeth and preparation method thereof |
KR102130949B1 (en) | 2016-04-19 | 2020-07-07 | 제이에프이 스틸 가부시키가이샤 | Abrasion-resistant steel plate and method of producing abrasion-resistant steel plate |
CN105861930A (en) * | 2016-05-23 | 2016-08-17 | 安徽鑫宏机械有限公司 | Casting method for valve body of high-temperature-resistant composite check valve |
PL234098B1 (en) * | 2016-06-27 | 2020-01-31 | Arcelormittal Poland Spolka Akcyjna | Multi-phase steel, preferably for the production of standard-gauge rails |
TWI756226B (en) * | 2016-06-30 | 2022-03-01 | 瑞典商伍德赫爾恩股份有限公司 | A steel for a tool holder |
CN106086689B (en) * | 2016-08-30 | 2018-01-02 | 南阳汉冶特钢有限公司 | A kind of high-strength abrasion-proof steel plate and its production method |
RU2635641C1 (en) * | 2017-03-28 | 2017-11-14 | Юлия Алексеевна Щепочкина | Cast steel |
CN107326305A (en) * | 2017-05-27 | 2017-11-07 | 江苏金基特钢有限公司 | A kind of anti-corrosion steel plate and its manufacture method |
RU2651065C1 (en) * | 2017-11-20 | 2018-04-18 | Юлия Алексеевна Щепочкина | Iron-based alloy |
CN107739985A (en) * | 2017-11-25 | 2018-02-27 | 铜陵市明诚铸造有限责任公司 | A kind of middle evanohm abrasion-proof steel ball and preparation method thereof |
RU2697301C1 (en) * | 2018-12-03 | 2019-08-13 | Публичное акционерное общество "Северсталь" (ПАО "Северсталь") | Method for production of tubular rolled products of increased corrosion resistance at a reversing mill |
BE1027395B1 (en) * | 2020-01-16 | 2021-01-29 | Magotteaux Int | FORGED CRUSH BALLS FOR SEMI-AUTOGENIC CRUSHERS |
RU2765972C1 (en) * | 2021-05-07 | 2022-02-07 | Публичное акционерное общество «Северсталь» (ПАО «Северсталь») | Method for the production of thick sheets from low-alloy mild steels on a reversing mill |
CN113355609B (en) * | 2021-05-26 | 2022-08-16 | 西安交通大学 | Modified high-boron iron-based wear-resistant alloy and preparation method thereof |
CN113737097A (en) * | 2021-09-01 | 2021-12-03 | 温州天和汽车部件有限公司 | Carbon steel material for manufacturing automobile shift fork and preparation method thereof |
CN117512279B (en) * | 2023-11-28 | 2024-12-03 | 巢湖学院 | A method for controlling the shape of NiCrMo thin-gauge quenched and tempered plate |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1019030B (en) * | 1989-12-30 | 1992-11-11 | 清华大学 | Bainite/martensite multi-phase steel with air-cooled high hardenability |
JP3273391B2 (en) * | 1993-12-16 | 2002-04-08 | 新日本製鐵株式会社 | Manufacturing method of good workability wear-resistant steel plate |
FR2726287B1 (en) * | 1994-10-31 | 1997-01-03 | Creusot Loire | LOW ALLOY STEEL FOR THE MANUFACTURE OF MOLDS FOR PLASTICS OR FOR RUBBER |
FR2729974B1 (en) * | 1995-01-31 | 1997-02-28 | Creusot Loire | HIGH DUCTILITY STEEL, MANUFACTURING PROCESS AND USE |
FR2733516B1 (en) * | 1995-04-27 | 1997-05-30 | Creusot Loire | STEEL AND PROCESS FOR THE MANUFACTURE OF PARTS WITH HIGH ABRASION RESISTANCE |
GB9608108D0 (en) * | 1996-04-19 | 1996-06-26 | Naco Inc | Steel Castings |
JP3757027B2 (en) * | 1996-06-05 | 2006-03-22 | 株式会社神戸製鋼所 | High strength hot rolled steel with excellent weldability, high strength steel wire and high strength steel bar using the same |
DE19710125A1 (en) * | 1997-03-13 | 1998-09-17 | Krupp Ag Hoesch Krupp | Process for the production of a steel strip with high strength and good formability |
JP3475706B2 (en) * | 1997-03-28 | 2003-12-08 | 住友金属工業株式会社 | High-strength, high-toughness tempered steel with excellent machinability |
DZ2530A1 (en) * | 1997-12-19 | 2003-02-01 | Exxon Production Research Co | Process for the preparation of a steel sheet, this steel sheet and process for strengthening the resistance to the propagation of cracks in a steel sheet. |
JP3433687B2 (en) * | 1998-12-28 | 2003-08-04 | Jfeスチール株式会社 | High-strength hot-rolled steel sheet excellent in workability and method for producing the same |
JP3551064B2 (en) * | 1999-02-24 | 2004-08-04 | Jfeスチール株式会社 | Ultra fine grain hot rolled steel sheet excellent in impact resistance and method for producing the same |
EP1096029B1 (en) * | 1999-04-21 | 2006-01-25 | JFE Steel Corporation | High tensile hot-dip zinc-coated steel plate excellent in ductility and method for production thereof |
FR2796966B1 (en) * | 1999-07-30 | 2001-09-21 | Ugine Sa | PROCESS FOR THE MANUFACTURE OF THIN STRIP OF TRIP-TYPE STEEL AND THIN STRIP THUS OBTAINED |
CN1115423C (en) * | 2000-09-26 | 2003-07-23 | 上海林沪实业有限公司 | High-hardness wear-resisting low-carbon alloy steel plate |
-
2002
- 2002-11-19 FR FR0214425A patent/FR2847271B1/en not_active Expired - Fee Related
-
2003
- 2003-11-13 PT PT03782550T patent/PT1563103E/en unknown
- 2003-11-13 JP JP2004554593A patent/JP4535875B2/en not_active Expired - Lifetime
- 2003-11-13 UA UAA200505982A patent/UA81134C2/en unknown
- 2003-11-13 RU RU2005119211/02A patent/RU2326180C2/en active
- 2003-11-13 EP EP03782550A patent/EP1563103B1/en not_active Expired - Lifetime
- 2003-11-13 ES ES03782550T patent/ES2300636T3/en not_active Expired - Lifetime
- 2003-11-13 CA CA2506347A patent/CA2506347C/en not_active Expired - Lifetime
- 2003-11-13 AT AT03782550T patent/ATE388247T1/en active
- 2003-11-13 PL PL375541A patent/PL203154B1/en unknown
- 2003-11-13 CN CNB2003801036481A patent/CN100348739C/en not_active Expired - Lifetime
- 2003-11-13 KR KR1020057009066A patent/KR101010593B1/en active IP Right Grant
- 2003-11-13 BR BRPI0315694-0A patent/BR0315694B1/en active IP Right Grant
- 2003-11-13 DE DE60319567T patent/DE60319567T2/en not_active Expired - Lifetime
- 2003-11-13 WO PCT/FR2003/003357 patent/WO2004048618A1/en active IP Right Grant
- 2003-11-13 US US10/535,176 patent/US7462251B2/en not_active Expired - Lifetime
- 2003-11-18 PE PE2003001169A patent/PE20040486A1/en not_active Application Discontinuation
- 2003-11-18 AR ARP030104258A patent/AR042072A1/en not_active Application Discontinuation
-
2005
- 2005-05-23 ZA ZA200504151A patent/ZA200504151B/en unknown
-
2008
- 2008-06-18 US US12/141,327 patent/US7998285B2/en not_active Expired - Lifetime
-
2009
- 2009-03-19 AU AU2009201117A patent/AU2009201117B8/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102199737A (en) * | 2010-03-26 | 2011-09-28 | 宝山钢铁股份有限公司 | 600HB-grade wear resistant steel plate and its manufacturing method |
CN102199737B (en) * | 2010-03-26 | 2012-09-19 | 宝山钢铁股份有限公司 | 600HB-grade wear resistant steel plate and its manufacturing method |
Also Published As
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1563103B1 (en) | Method for making an abrasion resistant steel plate and steel plate obtained | |
EP1563105B1 (en) | Method for making an abrasion resistant steel plate and plate obtained | |
EP1563104B1 (en) | Method for making an abrasion resistant steel plate and plate obtained | |
EP1913169B1 (en) | Manufacture of steel sheets having high resistance and excellent ductility, products thereof | |
EP0792944B1 (en) | Steel, suitable for manufacture of injection molds for plastics | |
EP1649069B1 (en) | Method of producing austenitic iron/carbon/manganese steel sheets having a high strength and excellent toughness and being suitable for cold forming, and sheets thus produced | |
EP1751321B1 (en) | Steel with high mechanical strength and wear resistance | |
EP1844173B1 (en) | Method for producing austenitic iron-carbon-manganese metal sheets, and sheets produced thereby | |
EP1896624B1 (en) | Martensitic stainless steel composition, method for making a mechanical part from said steel and resulting part | |
EP2689045B1 (en) | Hot-rolled steel sheet and associated production method | |
EP2753723B1 (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 | |
EP2707515B1 (en) | Producing method for very high yield strength martensitic steel sheet and steel sheet obtained | |
EP2020451A1 (en) | Method of manufacturing sheets of steel with high levels of strength and ductility, and sheets produced using same | |
CA3182750A1 (en) | Method for producing high-strength steel parts with improved ductility, and parts obtained by said method | |
EP1563110B1 (en) | Weldable structural steel component and method for making same | |
EP1563109B1 (en) | Weldable structural steel component and method for making same | |
EP1885900B1 (en) | Steel for submarine hulls with improved weldability | |
EP2103705A1 (en) | Method of manufacturing sheets of austenitic stainless steel with high mechanical properties | |
JP4320764B2 (en) | Gear case hardened steel with excellent impact fatigue strength and anti-pitting strength | |
JP2002348638A (en) | Roll for continuous casting and for hot rolling superior in hot abrasion resistance and thermal cracking resistance |
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: 20050517 |
|
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 |
|
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 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: FRENCH |
|
REF | Corresponds to: |
Ref document number: 60319567 Country of ref document: DE Date of ref document: 20080417 Kind code of ref document: P |
|
REG | Reference to a national code |
Ref country code: PT Ref legal event code: SC4A Free format text: AVAILABILITY OF NATIONAL TRANSLATION Effective date: 20080410 |
|
REG | Reference to a national code |
Ref country code: SE Ref legal event code: TRGR |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2300636 Country of ref document: ES Kind code of ref document: T3 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FD4D |
|
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 |
|
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: 20080305 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: 20080305 |
|
26N | No opposition filed |
Effective date: 20081208 |
|
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: 20080305 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: 20080605 |
|
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: 20080305 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20081130 Ref country code: LI 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: 20080906 |
|
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: 20080606 |
|
REG | Reference to a national code |
Ref country code: PT Ref legal event code: PC4A Owner name: INDUSTEEL FRANCE, FR Effective date: 20150616 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R081 Ref document number: 60319567 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: 388247 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: TE4A Ref document number: E 3310 Country of ref document: SK Owner name: INDUSTEEL CREUSOT, SAINT DENIS, FR Effective date: 20150821 Ref country code: SK Ref legal event code: PC4A Ref document number: E 3310 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 |
|
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: PT Payment date: 20221021 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: FI Payment date: 20221018 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: 60319567 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 3310 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: 388247 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: PT Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20231122 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 |