EP1426452B1 - Manufacturing process of a bainitic steel article - Google Patents
Manufacturing process of a bainitic steel article Download PDFInfo
- Publication number
- EP1426452B1 EP1426452B1 EP03292950A EP03292950A EP1426452B1 EP 1426452 B1 EP1426452 B1 EP 1426452B1 EP 03292950 A EP03292950 A EP 03292950A EP 03292950 A EP03292950 A EP 03292950A EP 1426452 B1 EP1426452 B1 EP 1426452B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- steel
- content
- carried out
- precipitation
- trace levels
- 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 abstract description 59
- 239000010959 steel Substances 0.000 title claims abstract description 59
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 10
- 238000001816 cooling Methods 0.000 claims abstract description 26
- 238000001556 precipitation Methods 0.000 claims abstract description 23
- 238000000034 method Methods 0.000 claims abstract description 19
- 239000000203 mixture Substances 0.000 claims abstract description 13
- 238000003754 machining Methods 0.000 claims abstract description 12
- 229910001208 Crucible steel Inorganic materials 0.000 claims abstract description 3
- 238000005496 tempering Methods 0.000 claims abstract 6
- 238000005242 forging Methods 0.000 claims description 21
- 238000005096 rolling process Methods 0.000 claims description 12
- 229910052782 aluminium Inorganic materials 0.000 claims description 11
- 229910052802 copper Inorganic materials 0.000 claims description 11
- 229910052720 vanadium Inorganic materials 0.000 claims description 9
- 229910052796 boron Inorganic materials 0.000 claims description 7
- 229910052719 titanium Inorganic materials 0.000 claims description 7
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 6
- 229910052797 bismuth Inorganic materials 0.000 claims description 3
- 239000012535 impurity Substances 0.000 claims description 3
- 229910052711 selenium Inorganic materials 0.000 claims description 3
- 229910052714 tellurium Inorganic materials 0.000 claims description 3
- 229910052742 iron Inorganic materials 0.000 claims description 2
- 229910052745 lead Inorganic materials 0.000 claims description 2
- 238000005266 casting Methods 0.000 abstract description 5
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 29
- 239000010949 copper Substances 0.000 description 14
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 12
- 229910052759 nickel Inorganic materials 0.000 description 12
- 238000007792 addition Methods 0.000 description 11
- 239000010936 titanium Substances 0.000 description 10
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 9
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 8
- 239000011572 manganese Substances 0.000 description 7
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 6
- 229910000943 NiAl Inorganic materials 0.000 description 6
- NPXOKRUENSOPAO-UHFFFAOYSA-N Raney nickel Chemical compound [Al].[Ni] NPXOKRUENSOPAO-UHFFFAOYSA-N 0.000 description 6
- 239000011651 chromium Substances 0.000 description 6
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 5
- 229910052799 carbon Inorganic materials 0.000 description 5
- 238000010438 heat treatment Methods 0.000 description 5
- 239000000463 material Substances 0.000 description 5
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 4
- 239000010955 niobium Substances 0.000 description 4
- 238000004881 precipitation hardening Methods 0.000 description 4
- 239000000047 product Substances 0.000 description 4
- 229910052710 silicon Inorganic materials 0.000 description 4
- 239000010703 silicon Substances 0.000 description 4
- 238000011282 treatment Methods 0.000 description 4
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 3
- 229910001563 bainite Inorganic materials 0.000 description 3
- 229910052804 chromium Inorganic materials 0.000 description 3
- 239000002244 precipitate Substances 0.000 description 3
- 239000006104 solid solution Substances 0.000 description 3
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 2
- 239000004411 aluminium Substances 0.000 description 2
- 229910001566 austenite Inorganic materials 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 239000011575 calcium Substances 0.000 description 2
- 238000005098 hot rolling Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 229910052748 manganese Inorganic materials 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 229910052758 niobium Inorganic materials 0.000 description 2
- 150000004767 nitrides Chemical class 0.000 description 2
- 229910052757 nitrogen Inorganic materials 0.000 description 2
- 239000011669 selenium Substances 0.000 description 2
- 239000011265 semifinished product Substances 0.000 description 2
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- BUGBHKTXTAQXES-UHFFFAOYSA-N Selenium Chemical compound [Se] BUGBHKTXTAQXES-UHFFFAOYSA-N 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth atom Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 229910052729 chemical element Inorganic materials 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 238000005272 metallurgy Methods 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 230000001376 precipitating effect Effects 0.000 description 1
- 238000010405 reoxidation reaction Methods 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 239000011593 sulfur Substances 0.000 description 1
- PORWMNRCUJJQNO-UHFFFAOYSA-N tellurium atom Chemical compound [Te] PORWMNRCUJJQNO-UHFFFAOYSA-N 0.000 description 1
- -1 titanium nitrides Chemical class 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
- 229910000859 α-Fe Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/42—Ferrous alloys, e.g. steel alloys containing chromium with nickel with copper
-
- 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
- C21D1/02—Hardening articles or materials formed by forging or rolling, with no further heating beyond that required for the formation
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/005—Modifying the physical properties by deformation combined with, or followed by, heat treatment of ferrous alloys
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—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
- C22C38/46—Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
-
- 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
-
- 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
- C21D2211/004—Dispersions; Precipitations
Definitions
- the invention relates to metallurgy, and more specifically the field of steels for the manufacture of parts to withstand significant stresses.
- such parts are made of hardened and tempered steel or, as far as possible, of forged steel with a ferrito-pearlitic structure which is supposed to offer a better technical-economic compromise, but whose mechanical performance is still limited. .
- Ferritic-pearlitic steels often used for this purpose are types XC70, 45Mn5, 30MnSiV6 and 38MnSiV5, and undergo, after rolling or forging, simple cooling in line with still air. Their method of implementation is therefore relatively economical, but their service life in the presence of high demands is limited.
- the object of the invention is to propose an association between a steel grade and a part manufacturing process, having economic advantages over existing associations without the metallurgical performance being altered, or even improving these performances.
- the part thus manufactured will have to withstand heavy fatigue stresses.
- this manufacturing process should, in particular, be adaptable to any forging line.
- the steel contains from 5 to 50 ppm B.
- the steel contains 0.005 to 0.04% Ti.
- the Ti content is preferably at least 3.5 times the N content of the steel.
- the steel contains from 0.005 to 0.06% Nb.
- the steel contains from 0.005 to 0.2% of S.
- the steel contains at least one of the elements Ca up to 0.007%, Te up to 0.03%, Se up to 0.05%, Bi up to 0.05% and Pb up to 0.1%.
- the C content of the steel is between 0.06 and 0.20%.
- the Mn content of the steel is then preferably between 0.5 and 1.5%, and the Cr content is preferably between 0.3 and 1.2%.
- the Ni content of the steel can then be preferably between traces and 1%.
- the Ni content of the steel can then also be between 2 and 4.5%, and the Al content is then between 1 and 2%.
- the precipitation yield is in the general case preferably between 425 and 600 ° C.
- the precipitation yield is preferably between 425 and 500 ° C for 1 to 10h.
- the precipitation is preferably between 500 and 600 ° C for more than 1 hour.
- the precipitation is preferably between 500 and 550 ° C for more than 1 hour.
- Said hot deformation may be a rolling.
- Said hot deformation may be forging.
- the controlled cooling of the blank is carried out at a rate of less than 3 ° C / s between 600 and 300 ° C.
- a steel part obtained by the process according to the invention has a bainitic microstructure, and typically a tensile strength Rm of 750 to 1300 MPa and a yield strength Re greater than or equal to 500 MPa.
- the invention consists of the combination of a steel grade and a post-casting treatment process comprising a hot forming step of the part, a controlled cooling being carried out in calm air or in pulsed air and a precipitation income preceding or following the machining of the room.
- the composition of the selected steel ensures that, regardless of the cooling mode, the fatigue strength results of the parts manufactured from this steel will be sufficient to meet the requirements of the users.
- the hot forming operation may consist of one or more rolling, or rolling followed by forging, or forging alone.
- the bottom line is that the last hot deformation brings the steel between 1100 and 1300 ° C, and the controlled cooling takes place from this temperature.
- the chemical characteristics of the steel and its heat treatments after casting aim at obtaining a bainitic microstructure, and also at obtaining optimized mechanical characteristics.
- This bainitic microstructure must be able to be obtained after cooling in still air, but must also be compatible with forced air cooling.
- the parts of the process of the invention can be produced on any existing installation, that it allows after forging or rolling a forced air cooling, or that it allows only a cooling in the calm air .
- a forging installation initially designed to treat ferritic-pearlitic microstructure steel parts can without difficulty, and without special adaptations, treat bainitic microstructure parts of the process of the invention.
- the bainitic microstructure steels previously used for these purposes required pulsed air cooling, and therefore could not always be processed on standard design facilities.
- the last hot deformation is carried out at 1100-1300 ° C and is followed by air-controlled cooling in hot rolling or forging, in still air or forced air. This gives a rough sketch of the piece.
- blade it should be understood that here is meant a bar, or a half-product in another form, from which the final piece will be obtained by machining, and this regardless of the mode of hot deformation practiced: rolling, forging or their combination.
- a precipitation income is then made. This is either before or after machining the workpiece from said blank.
- the carbon content is between 0.06 and 0.25%. This content makes it possible to govern the type of microstructure obtained. Less than 0.06%, the microstructure obtained would not be interesting for the objectives. Above 0.25%, in combination with the other elements, a sufficiently bainitic microstructure would not be obtained after cooling with still air.
- the manganese content is between 0.5 and 2%. This element added to more than 0.5% gives its quenchability to the material, and allows to obtain a broad bainitic range regardless of the cooling mode. A content greater than 2% would, however, be likely to cause excessive segregation.
- the silicon content is between traces and 3%. This element, which is not obligatory, is advantageous in that it hardens the bainite by passing it in solid solution.
- silicon avoids the problems associated with the presence of copper during hot forming. A content greater than 3% can however pose problems of machinability of the material.
- the nickel content is between traces and 4.5%. This non-obligatory element promotes quenchability and stabilization of austenite. If the aluminum content allows it, it can form very hardening NiAl precipitates, giving the metal high mechanical characteristics. In the case where copper is present in a relatively large quantity, nickel can play the same role as silicon. Above 4.5%, the addition of nickel is unnecessarily expensive in view of metallurgical objectives.
- the aluminum content is between traces and 3%.
- This non-obligatory element is a strong deoxidizer, and even added at a low level, it makes it possible to limit the amount of dissolved oxygen in the liquid steel, thus improving the inclusiveness of the room if it has been possible to avoid reoxidation too much. important during casting. At high levels, as has been said, it is likely to form NiAl precipitates if nickel is present in large quantities. It is not useful for the aluminum content to exceed 3%.
- chromium content a non-mandatory element, is between traces and 1.2%. Like manganese, chromium contributes to the improvement of quenchability. Its addition becomes unnecessarily expensive beyond 1.2%.
- the molybdenum content is between traces and 0.30%. This element, which is not mandatory, prevents the formation of coarse-grained ferrite and makes it possible to obtain the bainitic structure more definitely. Its addition is unnecessarily expensive beyond 0.30%.
- the vanadium content is between traces and 2%. This element, not mandatory, serves to harden the bainite by passing it in solid solution. At high content, it also makes it possible to obtain precipitation hardening of carbides and / or carbonitrides. Its addition is unnecessarily expensive beyond 2%.
- the copper content is between traces and 3.5%.
- This element which is not mandatory, can improve machinability and, by precipitating, cause secondary hardening of the material. But beyond 3.5% it makes hot formatting of the problematic part. As has been said, it is advisable to associate a significant nickel or silicon content to minimize hot forming problems. Beyond 3.5% its addition is in any case unnecessarily expensive.
- the boron content can be between 5 and 50 ppm. It can improve the hardenability, but must be in solid solution to be effective. In other words, it must be avoided that almost all the boron is found in the form of nitrides or carbonitrides of boron.
- the minimum titanium content, for this purpose is 0.005%, for the lowest nitrogen contents usually encountered. However, it is advisable not to exceed a titanium content of 0.04%, otherwise we obtain titanium nitrides too large.
- Titanium also has the function of limiting the magnification of the austenitic grain at high temperature, and can, for this, be added independently of boron, at a content of between 0.005 and 0.04%.
- Niobium may also be added at levels of between 0.005 and 0.06%. He too can precipitate in the form of carbonitrides in the austenite, and can thus bring about a hardening of the material.
- the machinability of the material can be improved by adding sulfur (from 0.005% to 0.2%), to which a calcium addition can also be added (up to 0.007%), and / or or tellurium (up to 0.03%) and / or selenium (up to 0.05%), and / or bismuth (up to 0.05%) and / or lead (up to 0.1%).
- the part blank is forged or not according to the usual methods. It is heated to 1100-1300 ° C, then the deformations giving rise to the piece blank are carried out.
- controlled cooling of the room is carried out, either in still air or in forced air.
- the part is forced to cool at a speed less than or equal to 3 ° C / s between 600 and 300 ° C.
- the precipitation yield is preferably between 425 and 600 ° C.
- the temperature of the income and its duration are optimally adapted to the targeted characteristics.
- the precipitation of copper is preferably obtained by treatment at 425-500 ° C for 1 to 10 hours.
- Precipitation of vanadium is preferably obtained by treatment at 500-600 ° C for more than 1 hour.
- Precipitation of NiAl is preferably obtained by treatment at 500-550 ° C for more than 1h.
- the tensile strength Rm is from 1000 to 1300 MPa and the yield strength Re is of the order of 900 MPa or more.
- the carbon content is limited to 0.06-0.2%, so as to obtain a bainite of hardness limited to 300-330 Hv30.
- the manganese content should be between 0.5 and 1.5%, the chromium content between 0.3 and 1.2%, and the nickel content can be up to 1% if it is not that a good quenchability, or go from 2 to 4% if one seeks a NiAl precipitation as we have seen. In the latter case, the aluminum content is between 1 and 2%.
- the tensile characteristics (yield strength, strength) of the product obtained after rolling or forging and cooling with controlled air are not particularly high: typically the tensile strength Rm is of the order of 750 -1050 MPa and the elasticity limit Re of the order of 500 to 750 MPa. But these steels have good machinability.
- This example is representative of the variant of the invention for which a relatively low carbon content can be used, and precipitation hardening is achieved by the addition of copper.
- composition of the steel is as follows, expressed in 10 -3 % by weight: VS mn Yes S P Or Cu Cr MB al Ti B NOT 80 1500 300 85 10 1500 2500 280 50 25 - - 6
- a bainitic microstructure After hot forging at a temperature of 1250-1200 ° C and cooling with still air (average cooling rate of 1 ° C / s between 700 and 300 ° C) a bainitic microstructure is obtained with a moderate hardness of 265Hv30, providing a resistance of less than 900 MPa. With this level of mechanical characteristics, machinability is not a problem. Then, an income at 450 ° C, with a hold time of one hour, allows to increase the resistance characteristics to reach more than 340Hv30 hardness, providing a resistance of 1100MPa.
- This example is representative of the variant of the invention for which a relatively low carbon content can be used, and precipitation hardening is carried out by the addition of vanadium.
- composition of the steel is as follows, expressed in 10 -3 % by weight: VS mn Yes S P Or Cu Cr MB al Ti V 150 1230 250 80 20 150 200 205 50 30 - 820
- This example is representative of the variant of the invention for which a relatively low carbon content can be used, and precipitation hardening is carried out by means of conjugate additions of nickel and aluminum.
- composition of the steel is as follows, given in 10 -3 % by weight: VS mn Yes S P Or Cu Cr MB al Ti B NOT 95 1150 200 80 10 3000 206 220 60 1500 - 3 3
- a bainitic microstructure After hot forging at a temperature of 1250-1200 ° C and cooling with still air (average cooling rate of 1 ° C / s between 700 and 300 ° C) a bainitic microstructure is obtained with a moderate hardness of 240Hv30, providing a resistance of less than 800 MPa. With this level of mechanical characteristics, machinability is not a problem. Then, an income at 520 ° C, with a holding time of 10 hours, increases the strength characteristics to reach more than 370Hv30 hardness, providing a resistance of the order of 1200MPa.
- composition of the steel is as follows, given in 10 -3 % by weight: VS mn Yes S P Or Cu Cr MB al Ti V B 230 1500 700 80 11 150 150 800 70 20 25 190 3
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Heat Treatment Of Steel (AREA)
- Forging (AREA)
- Heat Treatment Of Sheet Steel (AREA)
Abstract
Description
L'invention concerne la métallurgie, et plus précisément le domaine des aciers destinés à la fabrication des pièces devant résister à d'importantes sollicitations.The invention relates to metallurgy, and more specifically the field of steels for the manufacture of parts to withstand significant stresses.
Souvent, de telles pièces sont réalisées en un acier trempé et revenu ou, dans la mesure du possible, en acier forgé à structure ferrito-perlitique qui est censé offrir un meilleur compromis technico-économique, mais dont les performances mécaniques sont tout de même limitées.Often, such parts are made of hardened and tempered steel or, as far as possible, of forged steel with a ferrito-pearlitic structure which is supposed to offer a better technical-economic compromise, but whose mechanical performance is still limited. .
Des aciers à structure ferrito-perlitique souvent employés à cet effet sont des types XC70, 45Mn5, 30MnSiV6 et 38MnSiV5, et subissent après laminage ou forgeage un simple refroidissement en ligne à l'air calme. Leur méthode de mise en oeuvre est donc relativement économique, mais leur durée de vie en présence de fortes sollicitations est limitée.Ferritic-pearlitic steels often used for this purpose are types XC70, 45Mn5, 30MnSiV6 and 38MnSiV5, and undergo, after rolling or forging, simple cooling in line with still air. Their method of implementation is therefore relatively economical, but their service life in the presence of high demands is limited.
On a déjà proposé de réaliser de telles pièces en acier bainitique à partir d'une nuance de type 25MnSiCrVBS, le refroidissement après forgeage ou laminage ayant lieu à l'air. Les performances de tenue sont sensiblement améliorées par rapport aux exemples précédents, mais restent relativement limitées par rapport à ce qu'il est possible d'atteindre sur un acier trempé et revenu.It has already been proposed to make such bainitic steel pieces from a grade of 25MnSiCrVBS, the cooling after forging or rolling taking place in the air. The withstand performance is significantly improved over the previous examples, but remain relatively limited compared to what can be achieved on a tempered and tempered steel.
Le document
- coulée d'un acier de composition, en pourcentage de poids: C 0,04-0,08%; Mn 1,20-1,70%; Si 0,10-0,30%; Mo 0,100-0,500%; Ti 0,020-0,070; Nb 0.030-0,080%; balance Fe et impuretés;
- chauffage entre 1200 et 1300°C;
- laminage à chaud; et
- bobinage entre 450 et 560°C.
- casting of a composition steel, in percent by weight: C 0.04-0.08%; Mn 1.20-1.70%; If 0.10-0.30%; Mo 0.100-0.500%; Ti 0.020-0.070; Nb 0.030-0.080%; Fe balance and impurities;
- heating between 1200 and 1300 ° C;
- hot rolling; and
- winding between 450 and 560 ° C.
Le but de l'invention est de proposer une association entre une nuance d'acier et un procédé de fabrication d'une pièce, présentant des avantages économiques par rapport aux associations existantes sans que les performances métallurgiques soient altérées, voire en améliorant ces performances. La pièce ainsi fabriquée devra résister à d'importantes sollicitations en fatigue. Dans le cas des pièces forgées, ce procédé de fabrication devrait, en particulier, être adaptable sur toute ligne de forgeage.The object of the invention is to propose an association between a steel grade and a part manufacturing process, having economic advantages over existing associations without the metallurgical performance being altered, or even improving these performances. The part thus manufactured will have to withstand heavy fatigue stresses. In the case of forgings, this manufacturing process should, in particular, be adaptable to any forging line.
A cet effet, l'invention a pour objet un procédé de fabrication d'une pièce en acier, caractérisé en ce que :
- on élabore et on coule un acier de composition, en pourcentages pondéraux, 0,06% ≤ C ≤ 0,25% ; 0,5% ≤ Mn ≤ 2% ; traces ≤ Si ≤ 3% ; traces ≤ Ni ≤ 4,5% ; traces ≤ Al ≤ 3% ; traces ≤ Cr ≤ 1,2% ; traces ≤ Mo ≤ 0,30% ; traces ≤ V ≤ 2% ; traces ≤ Cu ≤ 3,5% ; et respectant l'une au moins des conditions :
- * 0,5% ≤ Cu ≤ 3,5%
- * 0,5% ≤ V ≤ 2%
- * 2% ≤ Ni ≤ 4,5% et 1% ≤ Al ≤ 2%
- on effectue au moins une déformation à chaud de l'acier coulé pour obtenir une ébauche de la pièce à une température de 1100 à 1300°C ;
- on effectue un refroidissement contrôlé de l'ébauche de la pièce à l'air calme ou à l'air pulsé à une vitesse inférieure à 3°C/s entre 600 at 300° C, de manière à lui conférer une microstructure bainitique;
- et on réchauffe l'acier pour effectuer un revenu de précipitation, précédant ou suivant l'usinage de la pièce à partir de ladite ébauche.
- a composition steel is produced and cast in percentages by weight, 0.06% ≤ C ≤ 0.25%; 0.5% ≤ Mn ≤ 2%; traces ≤ If ≤ 3%; traces ≤ Ni ≤ 4.5%; traces ≤ Al ≤ 3%; traces ≤ Cr ≤ 1.2%; traces ≤ Mo ≤ 0.30%; traces ≤ V ≤ 2%; traces ≤ Cu ≤ 3.5%; and respecting at least one of the conditions:
- * 0.5% ≤ Cu ≤ 3.5%
- * 0.5% ≤ V ≤ 2%
- * 2% ≤ Ni ≤ 4.5% and 1% ≤ Al ≤ 2%
- at least one hot deformation of the cast steel is performed to obtain a blank of the workpiece at a temperature of 1100 to 1300 ° C;
- a controlled cooling of the blank of the workpiece is carried out in still air or in pulsed air at a speed of less than 3 ° C./s between 600 and 300 ° C., so as to give it a bainitic microstructure;
- and heating the steel to effect a precipitation of precipitation, preceding or following machining of the workpiece from said blank.
De préférence, l'acier contient de 5 à 50 ppm de B.Preferably, the steel contains from 5 to 50 ppm B.
De préférence, l'acier contient de 0,005 à 0,04% de Ti.Preferably the steel contains 0.005 to 0.04% Ti.
Si du B est présent, la teneur en Ti est de préférence égale à au moins 3,5 fois la teneur en N de l'acier.If B is present, the Ti content is preferably at least 3.5 times the N content of the steel.
De préférence, l'acier contient de 0,005 à 0,06% de Nb.Preferably the steel contains from 0.005 to 0.06% Nb.
De préférence, l'acier contient de 0,005 à 0,2% de S.Preferably the steel contains from 0.005 to 0.2% of S.
Dans ce cas, de préférence, l'acier contient au moins un des éléments Ca jusqu'à 0,007%, Te jusqu'à 0,03%, Se jusqu'à 0,05%, Bi jusqu'à 0,05% et Pb jusqu'à 0,1%.In this case, preferably, the steel contains at least one of the elements Ca up to 0.007%, Te up to 0.03%, Se up to 0.05%, Bi up to 0.05% and Pb up to 0.1%.
Selon une variante de l'invention, la teneur en C de l'acier est comprise entre 0,06 et 0,20%.According to a variant of the invention, the C content of the steel is between 0.06 and 0.20%.
La teneur en Mn de l'acier est alors de préférence comprise entre 0,5 et 1,5%, et la teneur en Cr est de préférence comprise entre 0,3 et 1,2%.The Mn content of the steel is then preferably between 0.5 and 1.5%, and the Cr content is preferably between 0.3 and 1.2%.
La teneur en Ni de l'acier peut être alors de préférence comprise entre des traces et 1%.The Ni content of the steel can then be preferably between traces and 1%.
La teneur en Ni de l'acier peut alors également être comprise entre 2 et 4,5%, et la teneur en Al est alors comprise entre 1 et 2%.The Ni content of the steel can then also be between 2 and 4.5%, and the Al content is then between 1 and 2%.
Le revenu de précipitation est dans le cas général effectué de préférence entre 425 et 600°C.The precipitation yield is in the general case preferably between 425 and 600 ° C.
Lorsque l'acier contient 0,5 à 3,5% de Cu, le revenu de précipitation est de préférence effectué entre 425 et 500°C pendant 1 à 10h.When the steel contains 0.5 to 3.5% Cu, the precipitation yield is preferably between 425 and 500 ° C for 1 to 10h.
Lorsque l'acier contient 0,5 à 2% de V, le revenu de précipitation est effectué de préférence entre 500 et 600°C pendant plus d'1h.When the steel contains 0.5 to 2% of V, the precipitation is preferably between 500 and 600 ° C for more than 1 hour.
Lorsque l'acier contient de 2 à 4,5% de Ni et 1 à 2% d'Al, le revenu de précipitation est effectué de préférence entre 500 et 550°C pendant plus d'1h.When the steel contains 2 to 4.5% Ni and 1 to 2% Al, the precipitation is preferably between 500 and 550 ° C for more than 1 hour.
Ladite déformation à chaud peut être un laminage.Said hot deformation may be a rolling.
Ladite déformation à chaud peut être un forgeage.Said hot deformation may be forging.
De préférence, le refroidissement contrôlé de l'ébauche est effectué à une vitesse inférieure à 3°C/s entre 600 et 300°C.Preferably, the controlled cooling of the blank is carried out at a rate of less than 3 ° C / s between 600 and 300 ° C.
Une pièce en acier obtenue par le procédé selon l'invention a une microstructure bainitique, et typiquement une résistance à la traction Rm de 750 à 1300MPa et une limite d'élasticité Re supérieure ou égale à 500MPa.A steel part obtained by the process according to the invention has a bainitic microstructure, and typically a tensile strength Rm of 750 to 1300 MPa and a yield strength Re greater than or equal to 500 MPa.
Comme on l'aura compris, l'invention consiste en la combinaison d'une nuance d'acier et d'un procédé de traitement suivant la coulée comprenant une étape de mise en forme à chaud de la pièce, un refroidissement contrôlé pouvant être effectué à l'air calme ou à l'air pulsé et un revenu de précipitation précédant ou suivant l'usinage de la pièce. La composition de l'acier choisie garantit que, quel que soit le mode de refroidissement, les résultats de tenue en fatigue des pièces fabriquées à partir de cet acier seront suffisants pour répondre aux exigences des utilisateurs.As will have been understood, the invention consists of the combination of a steel grade and a post-casting treatment process comprising a hot forming step of the part, a controlled cooling being carried out in calm air or in pulsed air and a precipitation income preceding or following the machining of the room. The composition of the selected steel ensures that, regardless of the cooling mode, the fatigue strength results of the parts manufactured from this steel will be sufficient to meet the requirements of the users.
L'opération de mise en forme à chaud peut consister en un ou des laminages, ou en un laminage suivi d'un forgeage, ou en un forgeage seul. L'essentiel est que la dernière déformation à chaud amène l'acier entre 1100 et 1300°C, et que le refroidissement contrôlé ait lieu à partir de cette température.The hot forming operation may consist of one or more rolling, or rolling followed by forging, or forging alone. The bottom line is that the last hot deformation brings the steel between 1100 and 1300 ° C, and the controlled cooling takes place from this temperature.
Les caractéristiques chimiques de l'acier et ses traitements thermiques postérieurs à la coulée visent à l'obtention d'une microstructure bainitique, et également à l'obtention de caractéristiques mécaniques optimisées. Cette microstructure bainitique doit pouvoir être obtenue à la suite d'un refroidissement à l'air calme, mais doit aussi être compatible avec un refroidissement à l'air pulsé. De cette façon, les pièces du procédé de l'invention pourront être produites sur toute installation existante, que celle-ci permette après forgeage ou laminage un refroidissement à air pulsé, ou qu'elle ne permette qu'un refroidissement à l'air calme. Ainsi, une installation de forgeage initialement conçue pour traiter des pièces en acier à microstructure ferrito-perlitique pourra sans difficultés, et sans adaptations particulières, traiter des pièces à microstructure bainitique du procédé de l'invention. Les aciers à microstructure bainitique précédemment employés pour ces usages exigeaient un refroidissement à air pulsé, et ne pouvaient donc pas toujours être traités sur des installations de conception courante.The chemical characteristics of the steel and its heat treatments after casting aim at obtaining a bainitic microstructure, and also at obtaining optimized mechanical characteristics. This bainitic microstructure must be able to be obtained after cooling in still air, but must also be compatible with forced air cooling. In this way, the parts of the process of the invention can be produced on any existing installation, that it allows after forging or rolling a forced air cooling, or that it allows only a cooling in the calm air . Thus, a forging installation initially designed to treat ferritic-pearlitic microstructure steel parts can without difficulty, and without special adaptations, treat bainitic microstructure parts of the process of the invention. The bainitic microstructure steels previously used for these purposes required pulsed air cooling, and therefore could not always be processed on standard design facilities.
Selon l'invention, on commence donc par élaborer un acier dont la composition sera détaillée et justifiée plus loin, puis on le coule, en lingots ou en continu suivant le format de la pièce finale, et le plus généralement on le lamine de manière à obtenir un demi-produit.According to the invention, we therefore start by developing a steel whose composition will be detailed and justified further, then it is cast, in ingots or continuously according to the format of the final part, and more generally it is rolled so as to get a half-product.
On peut ensuite effectuer une opération de forgeage du demi-produit.It is then possible to perform a forging operation of the semi-finished product.
La dernière déformation à chaud est effectuée à 1100-1300°C et est suivie par un refroidissement contrôlé à l'air dans la chaude de laminage ou de forge, à l'air calme ou à l'air pulsé. On obtient ainsi une ébauche de la pièce.The last hot deformation is carried out at 1100-1300 ° C and is followed by air-controlled cooling in hot rolling or forging, in still air or forced air. This gives a rough sketch of the piece.
Par le terme « ébauche », il doit être compris que l'on désigne ici une barre, ou un demi-produit sous une autre forme, à partir duquel la pièce définitive sera obtenue par usinage, et ceci indépendamment du mode de déformation à chaud pratiqué : laminage, forgeage ou leur combinaison.By the term "blank", it should be understood that here is meant a bar, or a half-product in another form, from which the final piece will be obtained by machining, and this regardless of the mode of hot deformation practiced: rolling, forging or their combination.
On effectue ensuite un revenu de précipitation. Celui-ci se situe soit avant, soit après l'usinage de la pièce à partir de ladite ébauche.A precipitation income is then made. This is either before or after machining the workpiece from said blank.
Les fourchettes analytiques exigées sont les suivantes pour les différents éléments chimiques devant ou pouvant être présents (tous les pourcentages sont pondéraux).The analytical ranges required are as follows for the different chemical elements in front of or may be present (all percentages are by weight).
La teneur en carbone est comprise entre 0,06 et 0,25%. Cette teneur permet de gouverner le type de microstructure obtenu. A moins de 0,06%, la microstructure obtenue ne serait pas intéressante pour les objectifs visés. Au-delà de 0,25%, en combinaison avec les autres éléments, on n'obtiendrait pas une microstructure suffisamment bainitique après refroidissement à l'air calme.The carbon content is between 0.06 and 0.25%. This content makes it possible to govern the type of microstructure obtained. Less than 0.06%, the microstructure obtained would not be interesting for the objectives. Above 0.25%, in combination with the other elements, a sufficiently bainitic microstructure would not be obtained after cooling with still air.
La teneur en manganèse est comprise entre 0,5 et 2%. Cet élément ajouté à plus de 0,5% procure sa trempabilité au matériau, et permet d'obtenir un domaine bainitique large quel que soit le mode de refroidissement. Une teneur supérieure à 2% serait cependant susceptible de provoquer des ségrégations trop importantes.The manganese content is between 0.5 and 2%. This element added to more than 0.5% gives its quenchability to the material, and allows to obtain a broad bainitic range regardless of the cooling mode. A content greater than 2% would, however, be likely to cause excessive segregation.
La teneur en silicium est comprise entre des traces et 3%. Cet élément, non obligatoire à proprement parier, est avantageux en ce qu'il durcit la bainite par son passage en solution solide. De plus, au cas où du cuivre serait présent en quantité relativement importante, le silicium permet d'éviter les problèmes associés à cette présence de cuivre lors de la mise en forme à chaud. Une teneur supérieure à 3% peut cependant poser des problèmes d'usinabilité du matériau.The silicon content is between traces and 3%. This element, which is not obligatory, is advantageous in that it hardens the bainite by passing it in solid solution. In addition, in the case where copper is present in a relatively large amount, silicon avoids the problems associated with the presence of copper during hot forming. A content greater than 3% can however pose problems of machinability of the material.
La teneur en nickel est comprise entre des traces et 4,5%. Cet élément non obligatoire favorise la trempabilité et la stabilisation de l'austénite. Si la teneur en aluminium le permet, il peut former des précipités de NiAl très durcissants, procurant au métal des caractéristiques mécaniques élevées. Au cas où du cuivre serait présent en quantité relativement importante, le nickel peut jouer le même rôle que le silicium. Au-delà de 4,5%, l'addition de nickel est inutilement coûteuse au vu des objectifs métallurgiques visés.The nickel content is between traces and 4.5%. This non-obligatory element promotes quenchability and stabilization of austenite. If the aluminum content allows it, it can form very hardening NiAl precipitates, giving the metal high mechanical characteristics. In the case where copper is present in a relatively large quantity, nickel can play the same role as silicon. Above 4.5%, the addition of nickel is unnecessarily expensive in view of metallurgical objectives.
La teneur en aluminium est comprise entre des traces et 3%. Cet élément non obligatoire est un désoxydant fort, et même ajouté à faible teneur, il permet de limiter la quantité d'oxygène dissous dans l'acier liquide, donc d'améliorer la propreté inclusionnaire de la pièce si on a su éviter des réoxydations trop importantes lors de la coulée. A forte teneur, comme on l'a dit, il est susceptible de former des précipités de NiAl si du nickel est présent en grande quantité. Il n'est pas utile que la teneur en aluminium dépasse 3%.The aluminum content is between traces and 3%. This non-obligatory element is a strong deoxidizer, and even added at a low level, it makes it possible to limit the amount of dissolved oxygen in the liquid steel, thus improving the inclusiveness of the room if it has been possible to avoid reoxidation too much. important during casting. At high levels, as has been said, it is likely to form NiAl precipitates if nickel is present in large quantities. It is not useful for the aluminum content to exceed 3%.
La teneur en chrome, élément non obligatoire, est comprise entre des traces et 1,2%. Comme le manganèse, le chrome contribue à l'amélioration de la trempabilité. Son addition devient inutilement coûteuse au-delà de 1,2%.The chromium content, a non-mandatory element, is between traces and 1.2%. Like manganese, chromium contributes to the improvement of quenchability. Its addition becomes unnecessarily expensive beyond 1.2%.
La teneur en molybdène est comprise entre des traces et 0,30%. Cet élément, non obligatoire, empêche la formation de ferrite à gros grains et permet d'obtenir plus assurément la structure bainitique. Son addition est inutilement coûteuse au-delà de 0,30%.The molybdenum content is between traces and 0.30%. This element, which is not mandatory, prevents the formation of coarse-grained ferrite and makes it possible to obtain the bainitic structure more definitely. Its addition is unnecessarily expensive beyond 0.30%.
La teneur en vanadium est comprise entre des traces et 2%. Cet élément, non obligatoire, sert à durcir la bainite par son passage en solution solide. A forte teneur, il permet également d'obtenir un durcissement par précipitation de carbures et/ou de carbonitrures. Son addition est inutilement coûteuse au-delà de 2%.The vanadium content is between traces and 2%. This element, not mandatory, serves to harden the bainite by passing it in solid solution. At high content, it also makes it possible to obtain precipitation hardening of carbides and / or carbonitrides. Its addition is unnecessarily expensive beyond 2%.
La teneur en cuivre est comprise entre des traces et 3,5%. Cet élément, non obligatoire, peut améliorer l'usinabilité et, en précipitant, provoquer un durcissement secondaire du matériau. Mais au-delà de 3,5% il rend la mise en forme à chaud de la pièce problématique. Comme on l'a dit, il est conseillé de lui associer une teneur en nickel ou en silicium significative pour minimiser les problèmes de mise en forme à chaud. Au-delà de 3,5% son addition est de toute façon inutilement coûteuse.The copper content is between traces and 3.5%. This element, which is not mandatory, can improve machinability and, by precipitating, cause secondary hardening of the material. But beyond 3.5% it makes hot formatting of the problematic part. As has been said, it is advisable to associate a significant nickel or silicon content to minimize hot forming problems. Beyond 3.5% its addition is in any case unnecessarily expensive.
Par ailleurs, il faut que l'une au moins des trois conditions suivantes soit respectée :
- une teneur en cuivre comprise entre 0,5 et 3,5%
- une teneur en vanadium comprise entre 0,5 et 2%
- une teneur en nickel comprise entre 2 et 4,5% et une teneur en aluminium comprise entre 1 et 2%.
- a copper content between 0.5 and 3.5%
- a vanadium content between 0.5 and 2%
- a nickel content of between 2 and 4.5% and an aluminum content of between 1 and 2%.
Les éléments que l'on vient de citer sont ceux dont le rôle métallurgique est ou peut être le plus important pour l'invention, mais d'autres éléments que l'on va citer peuvent aussi être optionnellement présents pour améliorer certaines propriétés de l'acier.The elements that have just been mentioned are those whose metallurgical role is or may be the most important for the invention, but other elements that will be mentioned may also be optionally present to improve certain properties of the steel.
La teneur en bore peut être comprise entre 5 et 50ppm. Il peut améliorer la trempabilité, mais doit être en solution solide pour être efficace. Autrement dit, on doit éviter que tout le bore ou presque ne se retrouve sous la forme de nitrures ou carbonitrures de bore. A cet effet, il est conseillé d'associer à l'addition de bore une addition de titane, de préférence dans une proportion telle que 3,5 x N% ≤ Ti%. A cette dernière condition, on peut capter tout l'azote dissous et éviter la formation de nitrures ou de carbonitrures de bore. La teneur minimale en titane, à cet effet, est de 0,005%, pour les teneurs en azote les plus basses usuellement rencontrées. Il est cependant conseillé de ne pas dépasser une teneur en titane de 0,04%, sinon on obtient des nitrures de titane de taille trop élevée.The boron content can be between 5 and 50 ppm. It can improve the hardenability, but must be in solid solution to be effective. In other words, it must be avoided that almost all the boron is found in the form of nitrides or carbonitrides of boron. For this purpose, it is advisable to associate the addition of boron with an addition of titanium, preferably in a proportion such that 3.5 × N% ≤ Ti%. In this latter condition, all the dissolved nitrogen can be captured and the formation of nitrides or carbonitrides of boron can be avoided. The minimum titanium content, for this purpose, is 0.005%, for the lowest nitrogen contents usually encountered. However, it is advisable not to exceed a titanium content of 0.04%, otherwise we obtain titanium nitrides too large.
Le titane a également pour fonction de limiter le grossissement du grain austénitique à haute température, et peut, pour cela, être ajouté indépendamment du bore, à une teneur comprise entre 0,005 et 0,04%.Titanium also has the function of limiting the magnification of the austenitic grain at high temperature, and can, for this, be added independently of boron, at a content of between 0.005 and 0.04%.
Du niobium peut également être ajouté, à des teneurs comprises entre 0,005 et 0,06%. Lui aussi peut précipiter sous forme de carbonitrures dans l'austénite, et peut ainsi apporter un durcissement du matériau.Niobium may also be added at levels of between 0.005 and 0.06%. He too can precipitate in the form of carbonitrides in the austenite, and can thus bring about a hardening of the material.
Enfin, de manière classique, on peut améliorer l'usinabilité du matériau par une addition de soufre (de 0,005% à 0,2%), à laquelle on peut aussi associer une addition de calcium (jusqu'à 0,007%), et/ou de tellure (jusqu'à 0,03%) et/ou de sélénium (jusqu'à 0,05%), et/ou de bismuth (jusqu'à 0,05%) et/ou de plomb (jusqu'à 0,1%).Finally, in a conventional way, the machinability of the material can be improved by adding sulfur (from 0.005% to 0.2%), to which a calcium addition can also be added (up to 0.007%), and / or or tellurium (up to 0.03%) and / or selenium (up to 0.05%), and / or bismuth (up to 0.05%) and / or lead (up to 0.1%).
Une fois obtenu après laminage le demi-produit ayant la composition précédemment citée, on procède ou non à un forgeage de l'ébauche de la pièce selon les procédés habituels. On la chauffe jusqu'à 1100-1300°C, puis on exécute les déformations donnant naissance à l'ébauche de pièce.Once obtained after rolling the semi-finished product having the above-mentioned composition, the part blank is forged or not according to the usual methods. It is heated to 1100-1300 ° C, then the deformations giving rise to the piece blank are carried out.
En l'absence de forgeage, le laminage doit se terminer à une température de 1100-1300°C.In the absence of forging, the rolling must be completed at a temperature of 1100-1300 ° C.
Puis immédiatement après le laminage, ou après le forgeage si cette opération a été effectuée, on effectue un refroidissement contrôlé de la pièce, soit à l'air calme, soit à l'air pulsé. De manière générale, on impose à la pièce un refroidissement à une vitesse inférieure ou égale à 3°C/s entre 600 et 300°C.Then immediately after rolling, or after forging if this operation was carried out, controlled cooling of the room is carried out, either in still air or in forced air. In general, the part is forced to cool at a speed less than or equal to 3 ° C / s between 600 and 300 ° C.
Selon l'invention, et ce avant ou après l'usinage de la pièce qui lui confère ses dimensions définitives, on procède à un durcissement de l'acier par précipitation au moyen d'un revenu, c'est-à-dire d'un traitement thermique faisant suite à un réchauffage à partir d'une température égale ou de peu supérieure à l'ambiante ; pour cela trois options sont possibles, et peuvent d'ailleurs être combinées :
- la précipitation de cuivre, si la teneur en cuivre est comprise entre 0,5 et 3,5% ;
- la précipitation de vanadium si sa teneur est comprise entre 0,5 et 2% ;
- la précipitation de NiAl si la teneur en nickel est comprise entre 2 et 4,5% et la teneur en aluminium comprise entre 1 et 2%.
- the precipitation of copper, if the copper content is between 0.5 and 3.5%;
- the precipitation of vanadium if its content is between 0.5 and 2%;
- the precipitation of NiAl if the nickel content is between 2 and 4.5% and the aluminum content between 1 and 2%.
De manière générale, le revenu de précipitation est effectué de préférence entre 425 et 600°C. Mais la température du revenu et sa durée sont optimalement à adapter aux caractéristiques visées. A titre d'exemple, la précipitation du cuivre est obtenue de préférence par un traitement à 425-500°C pendant 1 à 10h. La précipitation de vanadium est de préférence obtenue par un traitement à 500-600°C pendant plus d'1h. La précipitation de NiAl est de préférence obtenue par un traitement à 500-550°C pendant plus d'1h.In general, the precipitation yield is preferably between 425 and 600 ° C. But the temperature of the income and its duration are optimally adapted to the targeted characteristics. By way of example, the precipitation of copper is preferably obtained by treatment at 425-500 ° C for 1 to 10 hours. Precipitation of vanadium is preferably obtained by treatment at 500-600 ° C for more than 1 hour. Precipitation of NiAl is preferably obtained by treatment at 500-550 ° C for more than 1h.
Ce revenu peut être effectué :
- soit après l'usinage de façon à avoir un métal pas trop dur pendant l'usinage ;
- soit après le refroidissement contrôlé à l'air et avant l'usinage ; on réalise alors l'usinage sur une pièce à hautes caractéristiques mécaniques, ce qui le rend particulièrement précis.
- after machining so as to have a metal not too hard during machining;
- after air-controlled cooling and before machining; machining is then performed on a part with high mechanical characteristics, which makes it particularly precise.
Grâce à ce revenu, on peut obtenir des caractéristiques mécaniques élevées pour le produit obtenu. Typiquement, la résistance à la traction Rm va de 1000 à 1300 MPa et la limite d'élasticité Re est de l'ordre de 900 MPa ou davantage.Thanks to this income, high mechanical characteristics can be obtained for the product obtained. Typically, the tensile strength Rm is from 1000 to 1300 MPa and the yield strength Re is of the order of 900 MPa or more.
Optimalement, on limite la teneur en carbone à 0,06-0,2%, de manière à obtenir une bainite de dureté limitée à 300-330 Hv30. Optimalement, la teneur en manganèse doit être comprise entre 0,5 et 1,5%, la teneur en chrome entre 0,3 et 1,2%, et la teneur en nickel peut soit aller jusqu'à 1% si on ne vise qu'une bonne trempabilité, soit aller de 2 à 4% si on recherche une précipitation de NiAl comme on l'a vu. Dans ce dernier cas, la teneur en aluminium est comprise entre 1 et 2%.Optimally, the carbon content is limited to 0.06-0.2%, so as to obtain a bainite of hardness limited to 300-330 Hv30. Optimally, the manganese content should be between 0.5 and 1.5%, the chromium content between 0.3 and 1.2%, and the nickel content can be up to 1% if it is not that a good quenchability, or go from 2 to 4% if one seeks a NiAl precipitation as we have seen. In the latter case, the aluminum content is between 1 and 2%.
Pour ces aciers, les caractéristiques de traction (limite d'élasticité, résistance) du produit obtenu après laminage ou forgeage et refroidissement à l'air contrôlé ne sont pas particulièrement élevées : typiquement la résistance à la traction Rm est de l'ordre de 750-1050 MPa et la limite d'élasticité Re de l'ordre de 500 à 750MPa. Mais ces aciers présentent une bonne usinabilité.For these steels, the tensile characteristics (yield strength, strength) of the product obtained after rolling or forging and cooling with controlled air are not particularly high: typically the tensile strength Rm is of the order of 750 -1050 MPa and the elasticity limit Re of the order of 500 to 750 MPa. But these steels have good machinability.
A titre d'exemples de mise en oeuvre de l'invention et d'exemple comparatif, on peut citer les essais suivants,By way of examples of implementation of the invention and comparative example, mention may be made of the following tests,
Cet exemple est représentatif de la variante de l'invention pour laquelle on peut utiliser une teneur en carbone relativement basse, et où on réalise le durcissement par précipitation grâce à une addition de cuivre.This example is representative of the variant of the invention for which a relatively low carbon content can be used, and precipitation hardening is achieved by the addition of copper.
La composition de l'acier est la suivante, exprimée en 10-3% pondéraux :
Après forgeage à chaud à une température de 1250-1200°C et refroidissement à l'air calme (vitesse de refroidissement moyenne de 1°C/s entre 700 et 300°C) une microstructure bainitique est obtenue avec une dureté modérée de 265Hv30, procurant une résistance inférieure à 900 MPa. Avec ce niveau de caractéristiques mécaniques, l'usinabilité ne pose pas de problèmes. Ensuite, un revenu à 450°C, avec une durée de maintien d'une heure, permet d'augmenter les caractéristiques de résistance pour atteindre plus de 340Hv30 de dureté, procurant une résistance de 1100MPa.After hot forging at a temperature of 1250-1200 ° C and cooling with still air (average cooling rate of 1 ° C / s between 700 and 300 ° C) a bainitic microstructure is obtained with a moderate hardness of 265Hv30, providing a resistance of less than 900 MPa. With this level of mechanical characteristics, machinability is not a problem. Then, an income at 450 ° C, with a hold time of one hour, allows to increase the resistance characteristics to reach more than 340Hv30 hardness, providing a resistance of 1100MPa.
Cet exemple est représentatif de la variante de l'invention pour laquelle on peut utiliser une teneur en carbone relativement basse, et où on réalise le durcissement par précipitation grâce à une addition de vanadium.This example is representative of the variant of the invention for which a relatively low carbon content can be used, and precipitation hardening is carried out by the addition of vanadium.
La composition de l'acier est la suivante, exprimée en 10-3% pondéraux :
Après forgeage à chaud à une température de 1250-1200°C et refroidissement à l'air calme (en moyenne 1°C/s entre 700 et 300°C) d'une pièce de forge de diamètre équivalent à 15mm, une microstructure majoritairement bainitique est obtenue avec déjà une dureté importante de 300-320Hv30, procurant une résistance de 1000MPa environ, qui est actuellement la limite haute permettant encore une usinabilité correcte sur des moyens d'usinage classiques. Après un revenu de 2h à 580°C, le durcissement par le vanadium permet d'atteindre une dureté de l'ordre de 400Hv30, correspondant à une résistance supérieure à 1200MPa.After hot forging at a temperature of 1250-1200 ° C and cooling in still air (on average 1 ° C / s between 700 and 300 ° C) of a forging piece of diameter equivalent to 15 mm, a microstructure mainly bainitique is obtained with already a significant hardness of 300-320Hv30, providing a resistance of about 1000MPa, which is currently the limit high still allowing good machinability on conventional machining means. After a period of 2 hours at 580 ° C., the hardening with vanadium makes it possible to reach a hardness of the order of 400Hv30, corresponding to a resistance greater than 1200 MPa.
Cet exemple est représentatif de la variante de l'invention pour laquelle on peut utiliser une teneur en carbone relativement basse, et où on réalise le durcissement par précipitation grâce à des additions conjuguées de nickel et d'aluminium.This example is representative of the variant of the invention for which a relatively low carbon content can be used, and precipitation hardening is carried out by means of conjugate additions of nickel and aluminum.
La composition de l'acier est la suivante, donnée en 10-3% pondéraux :
Après forgeage à chaud à une température de 1250-1200°C et refroidissement à l'air calme (vitesse de refroidissement moyenne de 1°C/s entre 700 et 300°C) une microstructure bainitique est obtenue avec une dureté modérée de 240Hv30, procurant une résistance inférieure à 800 MPa. Avec ce niveau de caractéristiques mécaniques, l'usinabilité ne pose pas de problèmes. Ensuite, un revenu à 520°C, avec une durée de maintien de 10 heures, permet d'augmenter les caractéristiques de résistance pour atteindre plus de 370Hv30 de dureté, procurant une résistance de l'ordre de 1200MPa.After hot forging at a temperature of 1250-1200 ° C and cooling with still air (average cooling rate of 1 ° C / s between 700 and 300 ° C) a bainitic microstructure is obtained with a moderate hardness of 240Hv30, providing a resistance of less than 800 MPa. With this level of mechanical characteristics, machinability is not a problem. Then, an income at 520 ° C, with a holding time of 10 hours, increases the strength characteristics to reach more than 370Hv30 hardness, providing a resistance of the order of 1200MPa.
La composition de l'acier est la suivante, donnée en 10-3% pondéraux :
Après forgeage à chaud à 1250 - 1200°C et refroidissement à l'air calme d'une pièce de diamètre équivalent à 25 mm, une microstructure majoritairement bainitique est obtenue avec une dureté voisine de 320 Hv30, procurant une résistance de 1050Mpa environ. Un revenu d'une heure entre 300 et 450°C ne permet pas d'augmenter significativement la résistance.After hot forging at 1250 - 1200 ° C and cooling in a still air of a piece of diameter equivalent to 25 mm, a predominantly bainitic microstructure is obtained with a hardness close to 320 Hv30, providing a resistance of about 1050Mpa. An income of one hour between 300 and 450 ° C does not significantly increase the resistance.
Claims (12)
- Method for producing a steel component, characterised in that:- a steel is produced and cast having a composition, in percentages by weight, 0.06% s C ≤ 0.25%; 0.5% ≤ Mn ≤ 2%; trace levels ≤ Si ≤ 3%; trace levels ≤ Ni ≤ 4.5%; trace levels ≤ Al ≤ 3%; trace levels ≤ Cr ≤ 1.2%; trace levels ≤ Mo ≤ 0.30%; trace levels ≤ V ≤ 2%; trace levels ≤ Cu ≤ 3.5%; and complying with at least one of the conditions:* 0.5% ≤ Cu ≤ 3.5%* 0.5% ≤ V ≤ 2%* 2% ≤ Ni ≤ 4.5% and 1% ≤ Al ≤ 2%optionally from 5 to 50 ppm of B;
optionally from 0.005 to 0.04% of Ti;
optionally from 0.005 to 0.06% of Nb;
optionally from 0.005 to 0.2% of S;
optionally at least one of the elements Ca up to 0.007%, Te up to 0.03%, Se up to 0.05%, Bi up to 0.05% and Pb up to 0.1%; the remainder being iron and impurities resulting from the production operation;- at least one hot-deformation of the cast steel is carried out in order to obtain a blank of the component at a temperature of from 1100 to 1300°C;- a controlled cooling of the blank of the component is carried out at a rate less than or equal to 3°C/s between 600 and 300°C in still air or pulsed air in order to confer a bainitic microstructure thereon;- and the steel is reheated in order to carry out a precipitation tempering operation prior to or following the machining of the component from the blank. - Method according to claim 1, characterised in that the steel contains B and Ti and that the content of Ti is equal to at least 3.5 times the N content of the steel.
- Method according to either claim 1 or claim 2, characterised in that the C content of the steel is between 0.06 and 0.20%.
- Method according to claim 3, characterised in that the Mn content of the steel is between 0.5 and 1.5%, and in that the Cr content is between 0.3 and 1.2%.
- Method according to claim 3 or claim 4, characterised in that the Ni content of the steel is between trace levels and 1%.
- Method according to claim 3 or claim 4, characterised in that the Ni content of the steel is between 2 and 4.5%, and in that the Al content is between 1 and 2%.
- Method according to any one of claims 1 to 6, characterised in that the precipitation tempering operation is carried out between 425 and 600°C.
- Method according to claim 7, characterised in that the steel contains from 0.5 to 3.5% of Cu, and in that the precipitation tempering operation is carried out between 425 and 500°C for from 1 to 10h.
- Method according to claim 7, characterised in that the steel contains from 0.5 to 2% of V, and in that the precipitation tempering operation is carried out between 500 and 600°C for more than 1 hour.
- Method according to claim 7, characterised in that the steel contains from 2 to 4.5% of Ni and from 1 to 2% of Al, and in that the precipitation tempering operation is carried out between 500 and 550°C for more than 1 hour.
- Method according to any one of claims 1 to 10, characterised in that the hot-deformation is a rolling operation.
- Method according to any one of claims 1 to 10, characterised in that the hot-deformation is a forging operation.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0215226 | 2002-12-03 | ||
FR0215226A FR2847908B1 (en) | 2002-12-03 | 2002-12-03 | A BAINITIQUE STEEL COOLED, COOLED AND REINVENTED, AND METHOD OF MANUFACTURING THE SAME. |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1426452A1 EP1426452A1 (en) | 2004-06-09 |
EP1426452B1 true EP1426452B1 (en) | 2009-09-02 |
Family
ID=32309974
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP03292950A Expired - Lifetime EP1426452B1 (en) | 2002-12-03 | 2003-11-27 | Manufacturing process of a bainitic steel article |
Country Status (11)
Country | Link |
---|---|
US (1) | US7354487B2 (en) |
EP (1) | EP1426452B1 (en) |
JP (1) | JP4316361B2 (en) |
CN (1) | CN1288270C (en) |
AT (1) | ATE441730T1 (en) |
CA (1) | CA2452647C (en) |
DE (1) | DE60329064D1 (en) |
ES (1) | ES2331949T3 (en) |
FR (1) | FR2847908B1 (en) |
MX (1) | MXPA03010998A (en) |
PL (1) | PL206237B1 (en) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7381642B2 (en) | 2004-09-23 | 2008-06-03 | Megica Corporation | Top layers of metal for integrated circuits |
JP4582177B2 (en) * | 2008-03-31 | 2010-11-17 | パナソニック電工株式会社 | Electric tool |
CN103074549B (en) * | 2012-12-01 | 2015-02-25 | 滁州恒昌机械制造有限公司 | Low-carbon multi-component alloy steel for excavator bucket tooth, and its production technology |
EP2985362B8 (en) * | 2013-10-02 | 2020-10-21 | Nippon Steel Corporation | Age-hardenable steel |
US10745772B2 (en) * | 2014-03-05 | 2020-08-18 | Daido Steel Co., Ltd. | Age hardening non-heat treated bainitic steel |
CN105543686A (en) * | 2015-12-28 | 2016-05-04 | 常熟市明瑞针纺织有限公司 | Pro/E-based warp knitting machine cam contour curve generation method |
CN105710264A (en) * | 2016-03-20 | 2016-06-29 | 电子科技大学中山学院 | Process for forging forge piece by adopting additional forced cooling conical plate upsetting method |
CN105886919A (en) * | 2016-06-13 | 2016-08-24 | 苏州双金实业有限公司 | Steel with anti-corrosion performance |
CN106011635A (en) * | 2016-08-03 | 2016-10-12 | 苏州市虎丘区浒墅关弹簧厂 | Impact resistant compressive spring material |
FR3064282B1 (en) * | 2017-03-23 | 2021-12-31 | Asco Ind | STEEL, METHOD FOR MANUFACTURING MECHANICAL PARTS FROM THIS STEEL, AND PARTS SO MANUFACTURED |
CN110684928B (en) * | 2019-10-31 | 2020-10-23 | 上海交通大学 | High-strength high-toughness thick plate structural steel for low temperature and heat treatment method thereof |
CN112501518B (en) * | 2020-12-01 | 2022-04-01 | 青岛科技大学 | Bainite steel and preparation method and application thereof |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
USRE28523E (en) * | 1963-11-12 | 1975-08-19 | High strength alloy steel compositions and process of producing high strength steel including hot-cold working | |
FR2741632B1 (en) * | 1995-11-27 | 1997-12-26 | Ascometal Sa | STEEL FOR MANUFACTURING A FORGED PART HAVING A BATH STRUCTURE AND METHOD FOR MANUFACTURING A PART |
JPH10102184A (en) * | 1996-09-26 | 1998-04-21 | Sumitomo Metal Ind Ltd | Hot rolled steel plate for resistance welded tube for high strength line pipe |
FR2774098B1 (en) * | 1998-01-28 | 2001-08-03 | Ascometal Sa | STEEL AND PROCESS FOR THE MANUFACTURE OF SECABLE MECHANICAL PARTS |
JP3900690B2 (en) * | 1998-06-26 | 2007-04-04 | 愛知製鋼株式会社 | Age-hardening high-strength bainitic steel and method for producing the same |
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 |
WO2001020051A1 (en) * | 1999-09-16 | 2001-03-22 | Nkk Corporation | Steel thin plate having high strength and method for production thereof |
EP1143019B1 (en) * | 1999-09-29 | 2014-11-26 | JFE Steel Corporation | Method for manufacturing a coiled steel sheet |
JP3750789B2 (en) * | 1999-11-19 | 2006-03-01 | 株式会社神戸製鋼所 | Hot-dip galvanized steel sheet having excellent ductility and method for producing the same |
JP2001152246A (en) * | 1999-11-22 | 2001-06-05 | Sanyo Special Steel Co Ltd | Method for producing steel for plastic molding die excellent in toughness, mirror finishing property and machinability |
US6558483B2 (en) * | 2000-06-12 | 2003-05-06 | Sumitomo Metal Industries, Ltd. | Cu precipitation strengthened steel |
-
2002
- 2002-12-03 FR FR0215226A patent/FR2847908B1/en not_active Expired - Fee Related
-
2003
- 2003-11-27 ES ES03292950T patent/ES2331949T3/en not_active Expired - Lifetime
- 2003-11-27 EP EP03292950A patent/EP1426452B1/en not_active Expired - Lifetime
- 2003-11-27 DE DE60329064T patent/DE60329064D1/en not_active Expired - Lifetime
- 2003-11-27 AT AT03292950T patent/ATE441730T1/en not_active IP Right Cessation
- 2003-11-28 MX MXPA03010998A patent/MXPA03010998A/en active IP Right Grant
- 2003-12-01 CA CA002452647A patent/CA2452647C/en not_active Expired - Fee Related
- 2003-12-02 CN CNB2003101247747A patent/CN1288270C/en not_active Expired - Fee Related
- 2003-12-02 JP JP2003403104A patent/JP4316361B2/en not_active Expired - Fee Related
- 2003-12-02 US US10/724,641 patent/US7354487B2/en not_active Expired - Fee Related
- 2003-12-03 PL PL363854A patent/PL206237B1/en unknown
Also Published As
Publication number | Publication date |
---|---|
ES2331949T3 (en) | 2010-01-21 |
JP4316361B2 (en) | 2009-08-19 |
CA2452647C (en) | 2009-07-14 |
FR2847908A1 (en) | 2004-06-04 |
EP1426452A1 (en) | 2004-06-09 |
DE60329064D1 (en) | 2009-10-15 |
CN1519386A (en) | 2004-08-11 |
CA2452647A1 (en) | 2004-06-03 |
US7354487B2 (en) | 2008-04-08 |
CN1288270C (en) | 2006-12-06 |
FR2847908B1 (en) | 2006-10-20 |
PL206237B1 (en) | 2010-07-30 |
PL363854A1 (en) | 2004-06-14 |
US20040108020A1 (en) | 2004-06-10 |
MXPA03010998A (en) | 2004-09-10 |
ATE441730T1 (en) | 2009-09-15 |
JP2004190138A (en) | 2004-07-08 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1874973B1 (en) | Tempered martensitic steel, method of producing a part from said steel and part thus obtained | |
EP0851038B2 (en) | Steel and process for forming a steel article by cold plastic working | |
EP0787812B1 (en) | Process for manufacturing steel forging | |
EP1979583B1 (en) | Method for making a combustion engine valve, and valve thus obtained | |
CA2847809A1 (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 | |
EP1426452B1 (en) | Manufacturing process of a bainitic steel article | |
CA3022115A1 (en) | A process for manufacturing a martensitic stainless steel part from a sheet | |
FR2958943A1 (en) | HEAT TREATED THERMALLY HIGH CARBON-HIGH-STRENGTH STEEL RAIL AND MANUFACTURING METHOD THEREOF | |
CA2984131A1 (en) | Steel, product made of said steel, and manufacturing method thereof | |
FR2931166A1 (en) | HOT FORGED STEEL WITH HIGH MECHANICAL CHARACTERISTICS OF THE PARTS PRODUCED | |
EP0051511A1 (en) | Cast roll for cold rolling, and method for its production | |
FR2774098A1 (en) | Steel for a divisible mechanical part, especially for two-piece internal combustion engine crank arm, manufacture by brittle fracture | |
JP4185997B2 (en) | Manufacturing method of bearing parts | |
EP3378957B1 (en) | Steel, method for manufacturning mechanical pieces made of the steel, and parts thus manufactured | |
FR2583778A1 (en) | HIGH STRENGTH STAINLESS STEEL | |
EP2134882B1 (en) | Microalloyed steel with good resistance to hydrogen for the cold-forming of machine parts having high properties | |
JP2009191330A (en) | Electric resistance steel tube | |
EP3274483B1 (en) | Parts with a bainitic structure having high strength properties and manufacturing process | |
EP1563109A1 (en) | Weldable steel building component and method for making same | |
EP2257652B1 (en) | Method of manufacturing sheets of austenitic stainless steel with high mechanical properties | |
FR3001738B1 (en) | METHOD FOR MANUFACTURING A COMPONENT OF THE AXLE OF A MOTOR VEHICLE | |
FR2781813A1 (en) | STEEL FOR MAKING A WORKPIECE FOR BEARING | |
JPH09165643A (en) | Bearing steel excellent in rolling fatigue characteristic | |
EP1725689A2 (en) | Forged or stamped average or small size mechanical part | |
FR2847592A1 (en) | Steel for the fabrication of high performance precision mechanical components by either hot or cold deformation processes, has a bainitic structure |
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 |
|
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 |
|
17P | Request for examination filed |
Effective date: 20041013 |
|
AKX | Designation fees paid |
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 |
|
17Q | First examination report despatched |
Effective date: 20070802 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
RTI1 | Title (correction) |
Free format text: MANUFACTURING PROCESS OF A BAINITIC STEEL ARTICLE |
|
RIN1 | Information on inventor provided before grant (corrected) |
Inventor name: DIERICKX, PIERRE Inventor name: ANDRE, GAELLE |
|
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: CH Ref legal event code: EP |
|
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: 60329064 Country of ref document: DE Date of ref document: 20091015 Kind code of ref document: P |
|
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: 2331949 Country of ref document: ES Kind code of ref document: T3 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20090902 |
|
NLV1 | Nl: lapsed or annulled due to failure to fulfill the requirements of art. 29p and 29m of the patents act | ||
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL 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: 20090902 Ref country code: SI 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: 20090902 |
|
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: 20090902 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FD4D |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: 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: 20090902 Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20100104 Ref country code: CZ 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: 20090902 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: 20090902 Ref country code: RO 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: 20090902 |
|
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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20090902 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT 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: 20090902 |
|
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: 20090902 |
|
26N | No opposition filed |
Effective date: 20100603 |
|
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: 20091203 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20091130 |
|
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: 20100303 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: TR 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: 20090902 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: LU Payment date: 20141024 Year of fee payment: 12 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20141118 Year of fee payment: 12 Ref country code: MC Payment date: 20141021 Year of fee payment: 12 Ref country code: ES Payment date: 20141124 Year of fee payment: 12 Ref country code: DE Payment date: 20141113 Year of fee payment: 12 Ref country code: FR Payment date: 20141016 Year of fee payment: 12 Ref country code: SE Payment date: 20141114 Year of fee payment: 12 Ref country code: CH Payment date: 20141114 Year of fee payment: 12 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: GC Effective date: 20141222 Ref country code: FR Ref legal event code: TP Owner name: ASCO INDUSTRIES, FR Effective date: 20141222 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: IT Payment date: 20141113 Year of fee payment: 12 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: BE Payment date: 20141127 Year of fee payment: 12 |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: 732E Free format text: REGISTERED BETWEEN 20150910 AND 20150916 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R081 Ref document number: 60329064 Country of ref document: DE Owner name: ASCO INDUSTRIES, FR Free format text: FORMER OWNER: ASCOMETAL, COURBEVOIE, FR |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 60329064 Country of ref document: DE |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151127 Ref country code: MC Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151130 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20151127 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151127 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151130 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151130 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST Effective date: 20160729 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151128 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20160601 Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151127 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151130 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FD2A Effective date: 20161227 |
|
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 NON-PAYMENT OF DUE FEES Effective date: 20151128 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151130 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: RG Effective date: 20180606 |