EP1563104B1 - 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
- EP1563104B1 EP1563104B1 EP03782551A EP03782551A EP1563104B1 EP 1563104 B1 EP1563104 B1 EP 1563104B1 EP 03782551 A EP03782551 A EP 03782551A EP 03782551 A EP03782551 A EP 03782551A EP 1563104 B1 EP1563104 B1 EP 1563104B1
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- EP
- European Patent Office
- Prior art keywords
- plate
- optionally
- process according
- steel
- titanium
- 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 42
- 239000010959 steel Substances 0.000 title claims description 42
- 238000005299 abrasion Methods 0.000 title claims description 19
- 238000000034 method Methods 0.000 title claims description 14
- 239000010936 titanium Substances 0.000 claims description 66
- 229910052719 titanium Inorganic materials 0.000 claims description 31
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 30
- 229910052799 carbon Inorganic materials 0.000 claims description 20
- 229910000734 martensite Inorganic materials 0.000 claims description 19
- 229910001566 austenite Inorganic materials 0.000 claims description 17
- 238000001816 cooling Methods 0.000 claims description 17
- 150000001247 metal acetylides Chemical class 0.000 claims description 13
- 239000000203 mixture Substances 0.000 claims description 12
- 239000000126 substance Substances 0.000 claims description 10
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 8
- 229910052758 niobium Inorganic materials 0.000 claims description 8
- 229910052720 vanadium 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
- 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
- 229910052757 nitrogen Inorganic materials 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
- 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
- 238000005496 tempering 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 19
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 18
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 12
- -1 titanium carbides Chemical class 0.000 description 11
- 239000010955 niobium Substances 0.000 description 10
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 8
- 230000000694 effects Effects 0.000 description 8
- 230000009466 transformation Effects 0.000 description 8
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 7
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 7
- 239000011651 chromium Substances 0.000 description 7
- 229910052759 nickel Inorganic materials 0.000 description 7
- 229910052750 molybdenum Inorganic materials 0.000 description 6
- 230000000717 retained effect Effects 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
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-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
- 239000011572 manganese Substances 0.000 description 5
- 239000011669 selenium Substances 0.000 description 5
- 230000015572 biosynthetic process Effects 0.000 description 4
- 230000001965 increasing effect Effects 0.000 description 4
- 239000011733 molybdenum Substances 0.000 description 4
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 4
- 238000001556 precipitation Methods 0.000 description 4
- 229910052710 silicon Inorganic materials 0.000 description 4
- 239000010703 silicon Substances 0.000 description 4
- 229910052717 sulfur Inorganic materials 0.000 description 4
- 239000011593 sulfur Substances 0.000 description 4
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 4
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 3
- 241001080024 Telles Species 0.000 description 3
- 229910052796 boron Inorganic materials 0.000 description 3
- 229910052748 manganese Inorganic materials 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
- 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
- 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
- 229940082150 encore Drugs 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 238000005098 hot rolling Methods 0.000 description 2
- 230000006872 improvement 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
- 239000011159 matrix material 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
- 238000011282 treatment Methods 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 244000000231 Sesamum indicum Species 0.000 description 1
- 235000003434 Sesamum indicum Nutrition 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
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- QUQFTIVBFKLPCL-UHFFFAOYSA-L copper;2-amino-3-[(2-amino-2-carboxylatoethyl)disulfanyl]propanoate Chemical compound [Cu+2].[O-]C(=O)C(N)CSSCC(N)C([O-])=O QUQFTIVBFKLPCL-UHFFFAOYSA-L 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
- 230000014509 gene expression Effects 0.000 description 1
- 239000008187 granular material Substances 0.000 description 1
- 210000002216 heart Anatomy 0.000 description 1
- WABPQHHGFIMREM-UHFFFAOYSA-N lead(0) Chemical compound [Pb] WABPQHHGFIMREM-UHFFFAOYSA-N 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000009527 percussion Methods 0.000 description 1
- JTJMJGYZQZDUJJ-UHFFFAOYSA-N phencyclidine Chemical class C1CCCCN1C1(C=2C=CC=CC=2)CCCCC1 JTJMJGYZQZDUJJ-UHFFFAOYSA-N 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
- 150000004772 tellurides Chemical class 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 239000010937 tungsten Substances 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
- C22C38/04—Ferrous alloys, e.g. steel alloys containing 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.
- Abrasion resistant steels are well known and are generally steels of high hardness (between 400 and 500 Brinell) having a martensitic structure, and containing from 0.12% to 0.3% carbon. It is generally accepted that in order to increase the wear resistance it is sufficient to increase the hardness, but this is done to the detriment of other properties such as the ability to weld or shape by folding, for example . Also, in order to obtain steels having both very good wear resistance and good processability, other means have been sought besides increasing the hardness.
- the object of the present invention is to overcome these disadvantages by providing an abrasion-resistant steel sheet having a good flatness and which, all things being equal, has an abrasion resistance better than that of steels. known.
- quenching may be followed by tempering at a temperature below 350 ° C, and preferably below 250 ° C.
- the invention also relates to a part, and in particular a sheet obtained in particular by this method, the steel having a structure consisting of 5% to 20% retained austenite, the remainder of the structure being martensitic or martensite-bainitic with carbides .
- the piece is a sheet, its thickness may be between 2 mm and 150 mm and its flatness may be characterized by an arrow less than or equal to 12 mm / m, and preferably less than 5 mm / m.
- the hardness is preferably between 280 HB and 450 HB.
- the hardness is preferably between 380 HB and 550 HB.
- the hardness is preferably between 450 HB and 650 HB.
- the carbon, titanium, zirconium and nitrogen contents must be such that: 0 , 1 % ⁇ VS - Ti / 4 - Zr / 8 + 7 ⁇ NOT / 8 ⁇ 0 , 55 %
- 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 0.1%, and preferably greater than or equal to 0.22%, to have a martensite having a minimum hardness, but beyond 0.55% the toughness and the the processability are too deteriorated.
- the chemical composition must be chosen so that the quenchability of the steel is sufficient, given the thickness of the sheet that is to be manufactured.
- the silicon content is greater than 0.5% so as to promote the formation of retained austenite.
- the contents of Ti, Zr and N should preferably be such that: Ti + Zr / 2 - 7xN / 2 ⁇ 0.05%, and more preferably greater than 0.1%, and more preferably, greater than 0.3% for the carbide content to be sufficient.
- 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 comprising large titanium or zirconium carbides, or even carbides of niobium, tantalum or vanadium, formed at high temperature.
- the inventors have found that the effectiveness of large carbides for the improvement of the abrasion resistance could be obelated by premature loosening thereof and that this loosening could be avoided by the presence of metastable austenite which is transformed in fresh martensite under the effect of abrasion phenomena.
- the conversion of the metastable austenite to fresh martensite is by swelling, this transformation in the abraded underlayer increases the resistance to carburetion and thus improves the 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, possibly after a cold planing or half-hot.
- an expansion treatment can be carried out at a temperature of less than or equal to 350 ° C, and preferably less than or equal to 250 ° C.
- the hardness being a function of the free carbon content C * the same hardness can be obtained with very different titanium or zirconium contents. With equal hardness, the resistance to abrasion is all the higher as the titanium or zirconium content is important. Similarly, titanium content or equal zirconium, the resistance to abrasion is even better than the hardness is high. In addition, the implementation of the steel is all the easier as the free carbon content is low, but with equal free carbon content, ductility is even better than the titanium content is low. All of these considerations make it possible to choose the carbon and titanium or zirconium contents which lead to all of the properties best suited to each field of application.
- steel sheets identified A to G according to the invention and H to J according to the prior art are considered.
- the chemical compositions of the steels, expressed in 10 -3 % by weight, as well as the hardness, the residual austenite content of the structure and a wear resistance index Rus, are reported in Table 1.
- the wear resistance index Rus varies as the logarithm of the inverse of the weight loss of a prismatic specimen rotated in a tank containing calibrated quartzite granules.
- All the sheets have a thickness of 30 mm, and the sheets corresponding to the steels A to G have been quenched according to the invention, after austenitization at 900 ° C.
- the sheets according to the invention have a martensite-bainitic structure containing from 5% to 20% retained austenite, whereas the sheets given for comparison have a completely martensitic structure, that is to say, martensitic and not containing more than 2 or 3% retained austenite. All plates contain carbides.
- the pair of steels F, G (according to the invention) is clearly different from the pair of steels I, J, term of gain of holding brought by the titanium.
- the resistance gain Rus supplied by 0.245% of Ti is 0.46, whereas it is only 0.31 for a difference of 0.265% of Ti in the case of the pair I, J. .
- the deformation after cooling, without planing, for the steel sheets according to the invention is less than 10 mm / m, and is about 15 mm / m for the steel sheet H.
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)
- Soft Magnetic Materials (AREA)
- Heat Treatment Of Strip Materials And Filament Materials (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.
Les aciers résistant à l'abrasion sont bien connus et sont, en général, des aciers de dureté élevée (comprise entre 400 et 500 Brinell) ayant une structure martensitique, et contenant de 0,12% à 0,3% de carbone. Il est en général admis que pour augmenter la résistance à l'usure il suffit d'augmenter la dureté, mais cela se fait au détriment d'autres propriétés telles que l'aptitude au soudage ou à la mise en forme par pliage, par exemple. Aussi, afin d'obtenir des aciers ayant tout à la fois une très bonne résistance à l'usure et une bonne aptitude à la mise en oeuvre, on a recherché d'autres moyens que l'augmentation de dureté.Abrasion resistant steels are well known and are generally steels of high hardness (between 400 and 500 Brinell) having a martensitic structure, and containing from 0.12% to 0.3% carbon. It is generally accepted that in order to increase the wear resistance it is sufficient to increase the hardness, but this is done to the detriment of other properties such as the ability to weld or shape by folding, for example . Also, in order to obtain steels having both very good wear resistance and good processability, other means have been sought besides increasing the hardness.
C'est ainsi qu'on a proposé dans
Le but de la présente invention est de remédier à ces inconvénients, en proposant une tôle en acier résistant à l'abrasion ayant une bonne planéité et qui, toutes choses égales par ailleurs, présente une résistance à l'abrasion, meilleure que celle des aciers connus.The object of the present invention is to overcome these disadvantages by providing an abrasion-resistant steel sheet having a good flatness and which, all things being equal, has an abrasion resistance better than that of steels. known.
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:
- 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%,
- 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 ≥ 0,0005% et K = 0 si B < 0,0005%,
- 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.
- optionally at least one element selected from Nb, Ta and V in such contents as 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%,
- 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 ≥ 0.0005% and K = 0 if B <0.0005%,
- 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 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, et notamment une tôle obtenue notamment par ce procédé, l'acier ayant une structure constituée de 5% à 20% d'austénite retenue, le reste de la structure étant martensitique ou martensito-bainitique avec des carbures. Lorsque la pièce est une tôle, son épaisseur peut être comprise entre 2 mm et 150 mm et sa planéité peut être caractérisée par une flèche inférieure ou égale à 12 mm/m, et de préférence inférieure à 5 mm/m.The invention also relates to a part, and in particular a sheet obtained in particular by this method, the steel having a structure consisting of 5% to 20% retained austenite, the remainder of the structure being martensitic or martensite-bainitic with carbides . When the piece is a sheet, its thickness may be between 2 mm and 150 mm and its flatness may be characterized by an arrow less than or equal to 12 mm / m, and preferably less than 5 mm / m.
Lorsque la teneur en carbone est telle que :
Lorsque la teneur en carbone est telle que :
Lorsque la teneur en carbone est telle que :
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 0,35% à 0,8% de carbone, et de préférence, plus de 0,45%, voire plus de 0,5%, et de 0% à 2% de titane, de 0% à 4% de zirconium, ces teneurs devant êtres telles que: 0,05% ≤ Ti+Zr/2 ≤ 2%. Le carbone est destiné d'une part à obtenir une structure martensitique suffisamment dure, d'autre part à former des carbures de titane et/ou de zirconium. La somme Ti+Zr/2 doit être supérieure à 0,05%, de préférence supérieure 0,10%, et mieux encore, supérieure à 0,3%, ou même supérieure à 0,5% pour qu'il y ait un minimum de carbures formés, mais doit rester inférieure à 2%, et de préférence inférieure ou égale à 0,9%, car au-delà, la ténacité et l'aptitude à la mise en oeuvre sont détériorées.
- 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 0,35% et 2% et de préférence supérieure à 0,5%, et mieux encore, 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.
- 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 0,50% de molybdène. Cet élément augmente la trempabilité et forme 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 0,50% 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 0.35% to 0.8% of carbon, and preferably more than 0.45% or even more than 0.5%, and from 0% to 2% of titanium, from 0% to 4% of zirconium these contents must be such that: 0.05% ≤ Ti + Zr / 2 ≤ 2%. The carbon is intended on the one hand to obtain a sufficiently hard martensitic structure, on the other hand to form titanium carbides and / or zirconium. The sum Ti + Zr / 2 must be greater than 0.05%, preferably greater than 0.10%, and more preferably greater than 0.3%, or even greater than 0.5%, so that there is minimum carbides formed, but must remain less than 2%, and preferably less than or equal to 0.9%, because beyond, the toughness and workability are deteriorated.
- From 0% (or traces) to 2% silicon and 0% (or traces) at 2% aluminum, the sum Si + Al being between 0.35% and 2% and preferably greater than 0 , 5%, and more 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, 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.
- From 0% (or traces) to 0.50% molybdenum. This element increases the quenchability and forms in martensite or bainite thin carbides hardening including self-precipitation precipitation during cooling. It is not necessary to exceed 0.50% 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%, he has no significant effect, it causes difficulties in hot rolling 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. 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 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 :
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 supérieure à 0,1%, et de préférence supérieure ou égale à 0,22%, pour avoir une martensite ayant une dureté minimale, mais au-delà de 0,55% la ténacité et l'aptitude à la mise en oeuvre sont trop détériorées.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 0.1%, and preferably greater than or equal to 0.22%, to have a martensite having a minimum hardness, but beyond 0.55% the toughness and the the processability are too deteriorated.
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:
A noter que, plus particulièrement lorsque Tremp est compris entre 1,8 et 2, il est préférable que la teneur en silicium soit supérieure à 0,5% de façon à favoriser la formation d'austénite retenue.Note that, especially when Tremp is between 1.8 and 2, it is preferable that the silicon content is greater than 0.5% so as to promote the formation of retained austenite.
En outre, les teneurs en Ti, Zr et N doivent, de préférence, être telles que : Ti + Zr/2 - 7xN/2 ≥ 0,05%, et mieux supérieure à 0,1 %, et mieux encore, supérieure à 0,3% pour que la teneur en carbures soit suffisante.In addition, the contents of Ti, Zr and N should preferably be such that: Ti + Zr / 2 - 7xN / 2 ≥ 0.05%, and more preferably greater than 0.1%, and more preferably, greater than 0.3% for the carbide content to be sufficient.
Enfin, 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, voire des carbures de niobium, de tantale ou de vanadium, formés à haute température. 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 en martensite fraîche sous l'effet des phénomènes d'abrasion. La transformation de l'austénite métastable en martensite fraîche 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.Finally, 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 comprising large titanium or zirconium carbides, or even carbides of niobium, tantalum or vanadium, formed at high temperature. The inventors have found that the effectiveness of large carbides for the improvement of the abrasion resistance could be obelated by premature loosening thereof and that this loosening could be avoided by the presence of metastable austenite which is transformed in fresh martensite under the effect of abrasion phenomena. The conversion of the metastable austenite to fresh martensite is by swelling, this transformation in the abraded underlayer increases the resistance to carburetion and thus improves the 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 favorisait l'obtention d'une proportion significative d'austénite résiduelle, et d'autre part, on réduisait les contraintes résiduelles engendrées par les changements de phase.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 it was favored to obtain a significant proportion of residual austenite, and on the other hand, the residual stresses generated by the phase changes were reduced.
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, 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, possibly after a cold planing or half-hot.
Pour réaliser le traitement thermique :
- on chauffe l'acier au-dessus du point AC3 de façon à lui conférer une structure entièrement austénitique,
- puis on le refroidit à une vitesse de refroidissement moyenne supérieure à la vitesse critique de transformation bainitique jusqu'à une température égale ou légèrement inférieure (de moins de 50°C environ) à une température T = 800 - 270xC* - 90xMn -37xNi - 70XCr - 83x(Mo + W/2), (exprimée en °C),
- 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 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.
- the steel is heated above the point AC 3 so as to give it a completely austenitic structure,
- and then cooled to a higher average cooling rate than the critical bainitic transformation rate to a temperature equal to or slightly lower (less than about 50 ° C) at a temperature T = 800 - 270xC * - 90xMn -37xNi - 70XCr - 83x (Mo + W / 2), (expressed in ° C),
- then, between the temperature thus defined (that is to say between T and T - about 50 ° C) and 100 ° C, the sheet is cooled to an average cooling rate at heart Vr between 0.1 ° C / s, to obtain a sufficient hardness, and 1150xep -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 à une température inférieure ou égale à 350°C, et de préférence inférieure ou égale à 250°C.In addition, an expansion treatment can be carried out at a temperature of less than or equal to 350 ° C, and preferably less than or equal to 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 ou avec un planage modéré. La tôle a une dureté comprise entre 280HB et 650HB. 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 moderate planing. The sheet has a hardness between 280HB and 650HB. This hardness depends mainly on the free carbon content C * = C - Ti / 4 - Zr / 8 + 7xN / 8.
En fonction des teneurs en carbone libre C*, on peut définir plusieurs domaine correspondant à des niveaux de dureté croissant, et en particulier :
- a) 0,1% ≤ C* ≤ 0,2%, la dureté est comprise entre 280HB et 450HB environ,
- b) 0,2% < C* ≤ 0,3%, la dureté est comprise entre 380HB et 550HB environ,
- c) 0,3% < C* ≤ 0,5%, la dureté est comprise entre 450HB et 650HB environ.
- a) 0.1% ≤ C * ≤ 0.2%, the hardness is between 280HB and 450HB approximately,
- b) 0.2% <C * ≤ 0.3%, the hardness is between 380HB and 550HB,
- c) 0.3% <C * ≤ 0.5%, the hardness is between 450HB and 650HB approximately.
La dureté étant fonction de la teneur en carbone libre C*, la même dureté peut être obtenue avec des teneurs en titane ou zirconium très différentes. A dureté égale, la résistance à l'abrasion est d'autant plus élevée que la teneur en titane ou zirconium est importante. De même, à teneur en titane ou zirconium égale, la résistance à l'abrasion est d'autant meilleure que la dureté est élevée. De plus, la mise en oeuvre de l'acier est d'autant plus facile que la teneur en carbone libre est faible, mais à teneur en carbone libre égale, la ductilité est d'autant meilleure que la teneur en titane est faible. L'ensemble de ces considérations permet de choisir les teneurs en carbone et titane ou zirconium qui conduisent à l'ensemble des propriétés les mieux adaptées à chaque domaine d'application.The hardness being a function of the free carbon content C *, the same hardness can be obtained with very different titanium or zirconium contents. With equal hardness, the resistance to abrasion is all the higher as the titanium or zirconium content is important. Similarly, titanium content or equal zirconium, the resistance to abrasion is even better than the hardness is high. In addition, the implementation of the steel is all the easier as the free carbon content is low, but with equal free carbon content, ductility is even better than the titanium content is low. All of these considerations make it possible to choose the carbon and titanium or zirconium contents which lead to all of the properties best suited to each field of application.
Selon les niveaux de dureté, les utilisations sont par exemple :
- 280 à 450 HB : godets, bennes de camions et de dumpers, blindages de cyclones, trémies, moules à parpaings,
- 380 à 550 HB : blindages de broyeurs à percussion, lame d'attaque de bulldozer, lames de benne preneuse, grilles de cribles,
- 450 à 650 HB : plaques de blindage de broyeur à cylindres, renforts de godets, renforts sous lame d'attaque, bouclier de lame éperon, bord d'attaque.
- 280 to 450 HB: buckets, trucks and dump trucks, cyclone shields, hoppers, block molds,
- 380 to 550 HB: hammer mill shields, bulldozer blade, clamshell blades, screen grates,
- 450 to 650 HB: roll crusher shield plates, bucket reinforcements, reinforcements under attack blade, spur blade shield, leading edge.
A titre d'exemple, on considère des tôles en aciers repérés A à G selon l'invention et H à J selon l'art antérieur. Les compositions chimiques des aciers, exprimés en 10-3 % en poids, ainsi que la dureté, la teneur en austénite résiduelle de la structure et un indice de résistance à l'usure Rus, sont reportées au tableau 1.
L'indice de résistance à l'usure Rus varie comme le logarithme de l'inverse de la perte de poids d'une éprouvette prismatique mise en rotation dans un bac contenant des granulats calibrés de quartzite.The wear resistance index Rus varies as the logarithm of the inverse of the weight loss of a prismatic specimen rotated in a tank containing calibrated quartzite granules.
Toutes les tôles ont une épaisseur de 30 mm, et les tôles correspondant aux aciers A à G ont été trempées conformément à l'invention, après austénitisation à 900°C.All the sheets have a thickness of 30 mm, and the sheets corresponding to the steels A to G have been quenched according to the invention, after austenitization at 900 ° C.
A près austénitisation, les conditions de refroidissement sont :
- pour les tôles en acier B et D: refroidissement à une vitesse moyenne de 0,7°C/s au-dessus de la température T définie plus haut, et à une vitesse moyenne de 0,13°C/s en dessous, conformément à l'invention;
- pour les tôles en acier A, C, E, F, G : refroidissement à une vitesse moyenne de 6°C/s au-dessus de la température T définie plus haut, et à une vitesse moyenne de 1,4°C/s en dessous, conformément à l'invention ;
- pour les tôles en acier H, I, J, données à titre de comparaison : austénitisation 900°C suivie de refroidissement 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.
- for steel sheets B and D: cooling at an average speed of 0.7 ° C / s above the temperature T defined above, and at an average speed of 0.13 ° C / s below, in accordance with to the invention;
- for steel sheets A, C, E, F, G: cooling at an average speed of 6 ° C / s above the temperature T defined above, and at an average speed of 1.4 ° C / sec below, according to the invention;
- for the steel sheets H, I, J, data for comparison: austenitization 900 ° C followed by cooling 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 selon l'invention ont une structure martensito-bainitique contenant de 5% à 20% d'austénite retenue, alors que les tôles données à titre de comparaison ont une structure entièrement martensitique, c'est à dire, martensitique et ne contenant pas plus de 2 ou 3% d'austénite retenue. Toutes les tôles contiennent des carbures.The sheets according to the invention have a martensite-bainitic structure containing from 5% to 20% retained austenite, whereas the sheets given for comparison have a completely martensitic structure, that is to say, martensitic and not containing more than 2 or 3% retained austenite. All plates contain carbides.
La comparaison des résistances à l'usure, montre que, à dureté et teneur en titane voisines, les tôles conformes à l'invention ont un coefficient Rus en moyenne supérieur de 0,5 à celui des tôles selon l'art antérieur. En particulier, la comparaison des exemples A et H qui diffèrent essentiellement par la structure (teneur en austénite résiduelle de 10% pour A, structure entièrement martensitique pour H) montre l'incidence de la présence d'austénite résiduelle dans la structure. Il est à noter que la différence de teneur en austénite résiduelle résulte à la fois de la différence entre les traitements thermiques et de la différence entre les teneurs en silicium.The comparison of the wear resistances, shows that, with similar hardness and titanium content, the sheets in accordance with the invention have an average coefficient Rus which is greater by 0.5 than that of the sheets according to the prior art. In particular, comparison of Examples A and H which differ essentially in structure (residual austenite content of 10% for A, fully martensitic structure for H) shows the incidence of the presence of residual austenite in the structure. It should be noted that the difference in residual austenite content results both from the difference between the heat treatments and the difference between the silicon contents.
On peut en outre observer que, toutes choses sensiblement égales par ailleurs, la contribution à la résistance à l'usure attribuable aux carbures de titane est significativement plus élevée quand leur présence est combinée avec celle d'austénite résiduelle, conformément à l'invention, que lorsque ces carbures sont précipités au sein d'une matrice essentiellement dépourvue d'austénite résiduelle. Ainsi pour des écarts similaires de teneurs en titane (et donc en TiC, le carbone étant toujours en excès), le couple d'aciers F,G (selon l'invention) se différencie nettement du couple d'aciers I,J, en terme de gain de tenue apporté par le titane. Pour F,G, le gain de résistance Rus apporté par 0,245% de Ti est de 0,46, alors qu'il n'est que de 0,31 pour un écart de 0,265% de Ti dans le cas du couple I,J.It may further be observed that, all else being substantially equal, the contribution to wear resistance attributable to titanium carbides is significantly greater when their presence is combined with that of residual austenite, according to the invention, only when these carbides are precipitated within a matrix essentially devoid of residual austenite. Thus, for similar differences in titanium content (and therefore in TiC, the carbon being always in excess), the pair of steels F, G (according to the invention) is clearly different from the pair of steels I, J, term of gain of holding brought by the titanium. For F, G, the resistance gain Rus supplied by 0.245% of Ti is 0.46, whereas it is only 0.31 for a difference of 0.265% of Ti in the case of the pair I, J. .
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 avec gonflement sous l'effet des sollicitations abrasives.This observation is attributable to the increased crimping effect of the titanium carbides by the surrounding matrix, when it contains residual austenite capable of being transformed into hard martensite with swelling under the effect of abrasive stresses.
Par ailleurs, la déformation après refroidissement, sans planage, pour les tôles en acier selon l'invention est inférieure à 10mm/m, et est d'environ 15mm/m pour la tôle en acier H.Furthermore, the deformation after cooling, without planing, for the steel sheets according to the invention is less than 10 mm / m, and is about 15 mm / m for the steel sheet H.
Il en résulte en pratique, soit la possibilité de livrer les produits sans planage, 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 des produits selon l'invention.This results in practice, either the possibility of delivering the products without planing, or the execution of a planing to satisfy a requirement of more severe flatness (for example 5mm / m) but achieved more easily and by introducing less constraints of the makes the original deformation less of the products according to the invention.
Claims (20)
- Process for manufacturing a part, and for example a plate, made of an abrasion-resistant steel, the chemical composition of which comprises, by weight:- 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%,
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), with C* = C - Ti/4 - Zr/8 + 7×N/8, and T-50°C;- then the part or the plate is cooled at a 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 any one of Claims 1 to 7, 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 8, 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:- 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:
the flatness of which is characterized by a bow of less than 12 mm/m, the steel having a martensitic or martensitic-bainitic structure, said structure also containing 5% to 20% residual austenite and carbides. - Part according to any one of Claims 10 to 16, characterized in that it is a plate with a thickness between 2 mm and 150 mm and the flatness of which is characterized by a bow of less than 12 mm/m.
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SI200331362T SI1563104T1 (en) | 2002-11-19 | 2003-11-13 | Method for making an abrasion resistant steel plate and plate obtained |
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FR0214424A FR2847270B1 (en) | 2002-11-19 | 2002-11-19 | METHOD FOR MANUFACTURING AN ABRASION RESISTANT STEEL SHEET AND OBTAINED SHEET |
FR0214424 | 2002-11-19 | ||
PCT/FR2003/003359 WO2004048620A1 (en) | 2002-11-19 | 2003-11-13 | Method for making an abrasion resistant steel plate and plate obtained |
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EP (1) | EP1563104B1 (en) |
JP (1) | JP4535877B2 (en) |
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CN (1) | CN100350061C (en) |
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AT (1) | ATE400667T1 (en) |
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BR (2) | BR122013002046B8 (en) |
CA (1) | CA2506351C (en) |
DE (1) | DE60322092D1 (en) |
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FR (1) | FR2847270B1 (en) |
PE (1) | PE20040487A1 (en) |
PL (1) | PL204080B1 (en) |
RU (1) | RU2327802C2 (en) |
SI (1) | SI1563104T1 (en) |
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DE102010050499B3 (en) * | 2010-11-08 | 2012-01-19 | Benteler Automobiltechnik Gmbh | Use of a wear-resistant steel component |
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