EP3445878B1 - Procédé de fabrication d'une pièce en acier inoxydable martensitique à partir d'une tôle - Google Patents
Procédé de fabrication d'une pièce en acier inoxydable martensitique à partir d'une tôle Download PDFInfo
- Publication number
- EP3445878B1 EP3445878B1 EP17713465.7A EP17713465A EP3445878B1 EP 3445878 B1 EP3445878 B1 EP 3445878B1 EP 17713465 A EP17713465 A EP 17713465A EP 3445878 B1 EP3445878 B1 EP 3445878B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- sheet
- traces
- shaping
- temperature
- volume
- 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.)
- Active
Links
- 238000000034 method Methods 0.000 title claims description 37
- 238000004519 manufacturing process Methods 0.000 title claims description 23
- 229910001105 martensitic stainless steel Inorganic materials 0.000 title claims description 5
- 230000008569 process Effects 0.000 title description 21
- 238000007493 shaping process Methods 0.000 claims description 73
- 229910000734 martensite Inorganic materials 0.000 claims description 47
- 229910000859 α-Fe Inorganic materials 0.000 claims description 43
- 238000005520 cutting process Methods 0.000 claims description 39
- 150000001247 metal acetylides Chemical class 0.000 claims description 32
- 238000012546 transfer Methods 0.000 claims description 30
- 239000000203 mixture Substances 0.000 claims description 29
- 230000009466 transformation Effects 0.000 claims description 26
- 229910001566 austenite Inorganic materials 0.000 claims description 16
- 229910001220 stainless steel Inorganic materials 0.000 claims description 7
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 6
- 239000012535 impurity Substances 0.000 claims description 5
- 238000003303 reheating Methods 0.000 claims description 5
- 239000010935 stainless steel Substances 0.000 claims description 5
- 229910052751 metal Inorganic materials 0.000 claims description 4
- 239000002184 metal Substances 0.000 claims description 4
- 238000000844 transformation Methods 0.000 claims description 4
- 230000008859 change Effects 0.000 claims description 3
- 229910052742 iron Inorganic materials 0.000 claims description 3
- 238000004381 surface treatment Methods 0.000 claims description 3
- 238000009628 steelmaking Methods 0.000 claims 1
- 229910000831 Steel Inorganic materials 0.000 description 54
- 239000010959 steel Substances 0.000 description 54
- 238000001816 cooling Methods 0.000 description 17
- 238000011282 treatment Methods 0.000 description 14
- 238000010438 heat treatment Methods 0.000 description 13
- 230000006698 induction Effects 0.000 description 12
- 230000007423 decrease Effects 0.000 description 10
- 238000005553 drilling Methods 0.000 description 7
- 230000015572 biosynthetic process Effects 0.000 description 6
- 238000005261 decarburization Methods 0.000 description 6
- 239000007788 liquid Substances 0.000 description 6
- 230000003647 oxidation Effects 0.000 description 6
- 238000007254 oxidation reaction Methods 0.000 description 6
- 238000000576 coating method Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 5
- 238000010791 quenching Methods 0.000 description 5
- 230000000171 quenching effect Effects 0.000 description 5
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 4
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 4
- 239000011248 coating agent Substances 0.000 description 4
- 150000004767 nitrides Chemical class 0.000 description 4
- 229910052757 nitrogen Inorganic materials 0.000 description 4
- 239000000047 product Substances 0.000 description 4
- 229910000975 Carbon steel Inorganic materials 0.000 description 3
- 238000005452 bending Methods 0.000 description 3
- 239000012467 final product Substances 0.000 description 3
- 238000012423 maintenance Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 230000007935 neutral effect Effects 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- 238000005480 shot peening Methods 0.000 description 3
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 2
- 229910052786 argon Inorganic materials 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 239000011247 coating layer Substances 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000000593 degrading effect Effects 0.000 description 2
- 238000004090 dissolution Methods 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 229910052750 molybdenum Inorganic materials 0.000 description 2
- 229910052758 niobium Inorganic materials 0.000 description 2
- 238000010301 surface-oxidation reaction Methods 0.000 description 2
- 229910052715 tantalum Inorganic materials 0.000 description 2
- 230000000930 thermomechanical effect Effects 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 229910052720 vanadium Inorganic materials 0.000 description 2
- 229910052726 zirconium Inorganic materials 0.000 description 2
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 101150087698 alpha gene Proteins 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000005422 blasting Methods 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 125000004432 carbon atom Chemical group C* 0.000 description 1
- 239000010962 carbon steel Substances 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000007872 degassing Methods 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 101150034785 gamma gene Proteins 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 238000003698 laser cutting Methods 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 238000005121 nitriding Methods 0.000 description 1
- 238000011017 operating method Methods 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 239000003973 paint Substances 0.000 description 1
- 235000019362 perlite Nutrition 0.000 description 1
- 239000010451 perlite Substances 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 229910052761 rare earth metal Inorganic materials 0.000 description 1
- 150000002910 rare earth metals Chemical class 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000005488 sandblasting Methods 0.000 description 1
- 239000011265 semifinished product Substances 0.000 description 1
- 239000002893 slag Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000005496 tempering Methods 0.000 description 1
- 230000002747 voluntary effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
Images
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
- C22C38/52—Ferrous alloys, e.g. steel alloys containing chromium with nickel with cobalt
-
- 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
- C21D1/62—Quenching devices
- C21D1/673—Quenching devices for die quenching
-
- 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
- C21D6/00—Heat treatment of ferrous alloys
-
- 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
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/002—Heat treatment of ferrous alloys containing Cr
-
- 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
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/004—Heat treatment of ferrous alloys containing Cr and Ni
-
- 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
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/005—Heat treatment of ferrous alloys containing Mn
-
- 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
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/007—Heat treatment of ferrous alloys containing Co
-
- 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
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/008—Heat treatment of ferrous alloys containing Si
-
- 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
- C21D7/00—Modifying the physical properties of iron or steel by deformation
- C21D7/13—Modifying the physical properties of iron or steel by deformation by hot working
-
- 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
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/002—Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
-
- 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
- C22C38/004—Very low carbon steels, i.e. having a carbon content of less than 0,01%
-
- 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
- C22C38/005—Ferrous alloys, e.g. steel alloys containing rare earths, i.e. Sc, Y, Lanthanides
-
- 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
- C22C38/008—Ferrous alloys, e.g. steel alloys containing tin
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/26—Ferrous alloys, e.g. steel alloys containing chromium with niobium or tantalum
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/28—Ferrous alloys, e.g. steel alloys containing chromium with titanium or zirconium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/30—Ferrous alloys, e.g. steel alloys containing chromium with cobalt
-
- 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
- C22C38/32—Ferrous alloys, e.g. steel alloys containing chromium with boron
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/38—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of manganese
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
-
- 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
- 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
- C22C38/48—Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—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
- 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
- C22C38/54—Ferrous alloys, e.g. steel alloys containing chromium with nickel with boron
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/58—Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/004—Dispersions; Precipitations
-
- 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
- C21D2211/005—Ferrite
-
- 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
Definitions
- the invention relates to the hot forming of stainless steels from a sheet to give them a complex shape and remarkable mechanical properties, these steels being intended, for example, for the automotive industry.
- Martensitic steels (or, more generally, with martensitic structure for more than 50%) have such mechanical characteristics, but their cold forming capacity is limited. We therefore have to either form them cold in the ferritic state, then heat treat the part to obtain the martensitic structure, or put them into hot form in the austenitic state by terminating the treatment by quenching. in order to obtain the martensitic structure.
- the object of the invention is to propose a method for producing a hot-transformed martensitic steel part, making it possible to manufacture parts of complex shape from a sheet, this final part also having high mechanical properties. making it suitable, in particular, for use in the automotive industry.
- Said sheet may have a martensitic transformation start temperature (Ms) ⁇ 400 ° C.
- the martensitic transformation start temperature (Ms) of the sheet can be between 390 and 220 ° C.
- the thickness of the sheet can be between 0.1 and 10 mm.
- the austenitization temperature can be at least 850 ° C.
- the austenitization temperature can be between 925 and 1200 ° C.
- the sheet can be reheated, during at least one of the steps of transferring and / or changing the configuration of the tool or the steps of shaping or cutting the sheet.
- a surface treatment can be carried out on the final part, intended to increase its roughness or its fatigue properties.
- the final part can be left between 90 and 500 ° C for 10 s to 1 h, then let it cool naturally in air.
- This process begins with an austenitization of the sheet, that is to say by an elevation of its temperature above the temperature Ac1 of the steel so as to form austenite in place of ferrite and carbides constituting the starting microstructure, and under conditions which limit as much as possible the surface decarburization and oxidation of the sheet.
- shaping step includes operations as diverse as deformation or removal of material as, in particular, deep drawing, hot stamping, stamping, cutting , drilling, these steps can take place in any order chosen by the manufacturer.
- the part obtained is cooled without any particular constraints on cooling.
- This cooling can be preceded by a cutting or final shaping step carried out between Ms and Mf (end temperature of martensitic transformation), under conditions where the microstructure consists of at least 10% austenite, at most 20% ferrite, the rest being martensite.
- composition of the martensitic stainless steel used in the process according to the invention is as follows. All percentages are weight percentages.
- Its C content is between 0.005% and 0.3%.
- the minimum content of 0.005% is justified by the need to obtain an austenitization of the microstructure during the first stage of the hot forming process, so that the final mechanical properties targeted are obtained. Above 0.3%, the weldability and, above all, the resilience of the sheet become insufficient, in particular for an application in the automotive industry.
- Mn content is between 0.2 and 2.0%.
- Si content is between traces (that is to say simple impurities resulting from the production, without Si having been added) and 1.0%.
- Si can be used as a deoxidizer during production, just like Al, to which it can be added or substituted. Above 1.0%, it is considered that it excessively promotes the formation of ferrite and therefore makes austenitization more difficult, and that it weakens the sheet too much for the shaping of a complex part to be assured. perform satisfactorily.
- Its Cr content is between 10.5 and 17.0%, preferably between 10.5% and 14.0% to have faster dissolution of the carbides during austenitization.
- the minimum content of 10.5% is justified to ensure the oxidability of the sheet.
- a content higher than 17% would make austenitization difficult and unnecessarily increase the cost of steel.
- Ni content is between traces and 4.0%.
- Ni is not essential to the invention.
- the presence of Ni within the prescribed limit of 4.0% maximum may, however, be advantageous for promoting austenitization. Exceeding the 4.0% limit would however lead to an excessive presence of residual austenite and an insufficient presence of martensite in the microstructure after cooling.
- Mo is not essential. However, it is favorable to good resistance to corrosion. Above 2.0%, austenitization would be hindered and the cost of steel unnecessarily increased.
- Cu content is between traces and 3.0%, preferably between traces and 0.5%.
- Cu requirements are classic for this type of steel. In practice, this means that adding Cu is not useful and that the presence of this element is only due to the raw materials used. A content greater than 0.5%, which would correspond to a voluntary addition, is not desired for automotive applications, because it would degrade the weldability. Cu can however aid in austenitization, and if the steel of the invention is applied to a field which does not require welding, the Cu content can range up to 3.0%.
- Ti is a deoxidizer, like Al and Si, but its cost and its lower efficiency than that of Al makes its use in general not very interesting from this point of view. It may be advantageous in that the formation of nitrides and carbonitrides of Ti can limit the growth of the grains and favorably influence certain mechanical properties and the weldability. However, this formation can be a drawback in the case of the process according to the invention, since Ti tends to hinder austenitization due to the formation of carbides, and TiNs degrade the resilience. A maximum content of 0.5% should therefore not be exceeded.
- V and Zr are also elements capable of forming nitrides degrading the resilience, and in general, the sum Ti + V + Zr must not exceed 0.5%.
- Al is used as a deoxidizer during production. After deoxidation, there should not remain in the steel an amount exceeding 0.2%, because there would be a risk of forming an excessive amount of AlN degrading the mechanical properties, and also of having difficulties in obtain the martensitic microstructure.
- the requirements on the O content are those which are conventional on martensitic stainless steels, depending on the ability to shape them without cracks starting from the inclusions and the quality of the mechanical properties sought after. the final part, and which the excessive presence of oxidized inclusions is likely to alter. Conversely, if a minimum machinability of the sheet is sought, it may be advantageous to have oxidized inclusions in significant number, if their composition makes them sufficiently malleable so that they serve as a lubricant for the cutting tool. This technique for controlling the number and composition of oxidized inclusions is classic in the steel industry. Control of the composition of the oxides can be advantageously obtained by controlled addition of Ca and / or adjustment of the composition of the slag with which the liquid steel is in contact and in chemical equilibrium during the production.
- Nb content is between 0.05% and 1.0%
- Nb + Ta content is between 0.05% and 1.0%.
- Nb and Ta are important elements for obtaining good resilience, and Ta improves the resistance to pitting corrosion. But as they can interfere with austenitization, they must not be present in quantities exceeding what has just been prescribed. Also, Nb and Ta capture C and N by forming carbonitrides which prevent too strong growth of the austenite grains during austenitization. This is favorable for obtaining a very good resilience when cold, between -100 ° C. and 0 ° C. On the other hand, if the content of Nb and / or Ta is too high, C and N will be entirely trapped in the carbonitrides and there will no longer be enough in dissolved form for the targeted mechanical properties to be achieved, in particular the resilience and the mechanical resistance.
- V content is between traces and 0.3%.
- V an embrittling element which is capable of forming nitrides, and must not be present in too large an amount.
- Ti + V + Zr must not exceed 0.5%.
- the total contents of Cu, Ni and Co must be between traces and 5.0%, so as not to leave too much residual austenite after the martensitic transformation and not to degrade the weldability in the applications which require it.
- Sn content is between traces and 0.05% (500 ppm). This element is not desired because it is detrimental to the weldability and the ability of the steel to be hot processed.
- the 0.05% limit is a tolerance.
- Zr content is between traces and 0.5%, because it reduces the resilience and hinders austenitization. It is also recalled that the total content of Ti + V + Zr must not exceed 0.5%.
- H content is between traces and 5 ppm, preferably not more than 1 ppm. Excessive H content tends to weaken martensite. It will therefore be necessary to choose a method of production of steel in the liquid state which can ensure this low presence of H. Typically, treatments ensuring a thorough degassing of the liquid steel (by massive injection of argon in the liquid steel, well-known process known as “AOD”, or by a vacuum passage during which the steel is decarbonized by release of CO, process known as “VOD”) are indicated.
- N content is between traces and 0.2% (2000 ppm). N is an impurity of which the same treatments which make it possible to reduce the H content help to limit the presence, or even to reduce it substantially. It is not always necessary to have a particularly low N content, but for the reasons that have been said it is necessary that its content, considered jointly with those of elements with which it can combine to form nitrides or carbonitrides obeys the relation 8 ⁇ (Nb + Ta) / (C + N) ⁇ 0.25.
- the rest of the steel is made up of iron and impurities resulting from the production.
- composition of the steel relate to the temperatures at the start of martensitic transformation Ms and at the end of martensitic transformation Mf.
- Ms should preferably be at most 400 ° C. If Ms is higher, there is a risk that the different transfer and shaping operations for the part will not follow each other quickly enough and that there will not be time to carry out all of the shaping at a temperature higher than Ms. However, this risk can be limited or avoided by providing that the part undergoes reheating or temperature maintenance between the shapings, and / or during these if using heating tools of known types integrating , for example, electrical resistors. This condition Ms ⁇ 400 ° C is therefore not always imperative, but only recommended for economical and easy application of the process according to the invention under industrial conditions.
- Ms must be greater than or equal to 200 ° C. to avoid subsistence in the final part of too high a content of residual austenite, which, in particular, would degrade Rp0.2 by bringing it below 800 MPa.
- Ms is between 390 and 320 ° C.
- Mf must be greater than or equal to -50 ° C to guarantee that there will not be too much residual austenite in the final part.
- Ms and Mf are preferably determined experimentally, for example by dilatometric measurements as is well known, see for example the article "Uncertainties in dilatometric determination of martensite start temperature", Yang and Badeshia, Materials Science and Technology, 2007/5, pp 556-560 .
- thermomechanical treatments which will be described can be carried out either on a bare sheet which may possibly be coated subsequently, or on a sheet already coated, for example with an Al-based alloy and / or Zn.
- This coating typically 1 to 200 ⁇ m thick and present on one or two faces of the sheet, may have been deposited by any technique conventionally used for this purpose, it is simply necessary that, if it has been deposited before austenitization, it does not evaporate during the stay of the sheet at austenitization and deformation temperatures, and is not deteriorated during deformations.
- the process according to the invention is as follows, applied to the manufacture and shaping of a sheet.
- an initial stainless steel sheet bare or coated, having the composition just described and a thickness which is typically from 0.1 to 10 mm, is conventionally prepared.
- This preparation can include operations of hot and / or cold transformation and cutting of the semi-finished product resulting from the casting and the solidification of the liquid steel.
- This initial sheet must have a microstructure consisting of ferrite and / or returned martensite and from 0.5% to 5% by volume of carbides.
- the size of the ferritic grains measured according to standard NF EN ISO 643, is between 1 and 80 ⁇ m, preferably between 5 and 40 ⁇ m. A ferritic grain size of 40 ⁇ m at most is recommended to promote the austenitization which will follow and thus obtain at least the 80% of austenite desired. A ferritic grain size of at least 5 ⁇ m is recommended to obtain good cold forming capacity.
- the sheet is first austenitized by passing through an oven which brings it to a range of temperatures greater than Ac1 (temperature at the start of the appearance of austenite), therefore typically greater than approximately 850 ° C. for the compositions concerned). It should be understood that this austenitization temperature must relate to the entire volume of the sheet, and that the treatment must be long enough so that, taking into account the thickness of the sheet and the kinetics of the transformation, the austenitization is complete throughout this volume.
- the maximum temperature of this austenitization is not a characteristic specific to the invention. It must simply be such that the sheet remains in an entirely solid state (the temperature must therefore be lower, in any case, than the solidus temperature of the steel) and is not too soft to support without transfer the transfer between the oven and the shaping tool which will follow the austenitization. Also, the temperature should not be raised to the point of causing significant surface oxidation and / or decarburization of the sheet in the heating atmosphere. A surface oxidation would lead to the need to descaling the sheet mechanically or chemically before it is shaped to avoid encrustation of scale in the surface of the sheet, and would cause a loss of material.
- the austenitization takes place at a temperature between 925 and 1200 ° C. for a duration tm of 10 s to 1 h (this duration being that which the sheet passes over Ac1), preferably between 2 min and 10 min for heating in a conventional oven and between 30 s and 1 min for an induction oven.
- An induction furnace has the advantage, known in itself, of providing rapid reheating to the nominal austenitization temperature. It therefore allows a shorter treatment than a conventional oven to achieve the desired result. These temperatures and durations make it possible to ensure that the continuation of the treatments will lead to a sufficient formation of martensite, and this for a reasonable duration allowing good productivity of the process.
- This austenitization is to pass the metal from the initial ferrite + carbides structure to an austenitic structure containing at most 0.5% carbides by volume fraction, and at most 20% residual ferrite by volume fraction.
- An object of this austenitization is, in particular, to lead to a dissolution of at least the majority of the carbides initially present, so as to release C atoms to form the austenitic structure then the martensitic structure during the following stages of the process.
- the maximum residual ferrite content of 20%, which must remain until the final product, is justified by the resilience and the conventional elastic limit which it is desired to obtain.
- the austenitized sheet is then transferred to a suitable forming tool (such as a stamping or stamping tool) or a cutting tool.
- a suitable forming tool such as a stamping or stamping tool
- This transfer has a duration t0 as short as possible, and during this transfer the sheet must remain at a temperature higher than Ms and keep an austenitic microstructure at 0.5% maximum of carbides and 20% maximum of residual ferrite.
- the sheet is at a temperature TP0, which is as close as possible to the nominal austenitization temperature for obvious reasons of energy saving.
- a first shaping or cutting step is then carried out, of duration t1 typically between 0.1 and 10 s.
- duration t1 typically between 0.1 and 10 s.
- the precise duration of this stage is not in itself a fundamental characteristic of the invention. It must be sufficiently brief so that the temperature of the sheet does not drop below Ms, that there is no decarburization and / or significant oxidation of the sheet surface, and that an austenitic microstructure with 0.5% maximum of carbides and 20% maximum of residual ferrite is always present at the end of the operation. If necessary, one can use a shaping tool provided with sheet heating means so that these temperature and microstructure conditions are met, since the contact of a non-heating shaping tool with the sheet causes sheet cooling which is often greater than 100 ° C / s.
- the sheet thus formed is then transferred to another tool for a second shaping step in the broad sense of the term.
- the same tool is used in the two stages but by modifying its configuration in the meantime (for example by replacing the punch in the case where a drawing is made in each of the two stages).
- the duration t2 of this transfer is typically from 1 to 10 s, the aim being that it is fast enough for the temperature of the sheet to remain above Ms during the transfer and for the microstructure to remain austenitic, at 0.5% maximum. of carbides and 20% maximum of residual ferrite.
- the second shaping step is then carried out, of duration t3 typically between 0.1 and 10 s.
- duration t3 typically between 0.1 and 10 s.
- the temperature of the sheet remains above Ms and the microstructure remains austenitic, at 0.5% maximum of carbides and 20% maximum of residual ferrite.
- the average cooling rate between TP0 and TPn defined by the quantity (TP0-TPn) / ⁇ ti, ⁇ ti constituting the sum of the durations of transfers and shaping, must be at least 0.5 ° C / s.
- composition of the steel is precisely chosen so that, compared to the carbon steels which it is the most common to use in the automotive industry for the production of sheets capable of being welded, this nose is shifted towards the durations higher, thus making possible on usual shaping tools the avoidance of the bainitic domain, a fortiori of the ferritic and perlitic domains, and therefore a execution as complete as possible of the transformation of austenite into martensite.
- each step taken individually must make it possible to maintain an austenitic microstructure with a maximum of 0.5% of carbides and a maximum of 20% of residual ferrite.
- the duration / cooling rate of each stage must therefore be chosen accordingly, and, if necessary, reheating of the sheet between and / or during shaping or cutting is carried out so that this microstructure can be maintained during all the steps.
- At least one additional shaping step in the broad sense at a temperature between Ms and Mf, in a field where the microstructure comprises at least 5% by volume of austenite. If this additional step is a cut, the final shape of the part can be reached with less wear of the tools, and if this additional step is a deformation, at least 5% of austenite will provide sufficient ductility for this deformation to be still possible despite the sometimes already significant presence of martensite.
- the sheet is allowed to cool, for example in the open air, to room temperature, thereby obtaining the final part according to the method of the invention. It is not necessary to impose a minimum speed during this cooling, because the composition of the steel ensures that the sheet will remain anyway in the area where the martensitic transformation can also take place during this cooling down to the ambient, at least if no means are used which significantly slow down cooling compared to natural cooling in the open air, such as a covering of the sheet. Of course, it is not excluded to accelerate this cooling, by means of forced air or a spray of water or another fluid.
- a surface treatment can be applied to the final part such as shot blasting or sandblasting, with the aim of increasing the roughness of its surface to improve the adhesion of a coating which would be subsequently applied, such as a paint, or to create residual stresses improving the fatigue resistance of the sheet.
- This type of operation is known in itself.
- a final heat treatment can be carried out on the final part, therefore after cooling to the ambient, to improve its elongation at break and bring it to a value of more than 8% according to ISO standards, which corresponds substantially more than 10% according to JIS standards.
- This treatment consists in making the final part stay between 90 and 500 ° C for 10 s to 1 h, then in performing a natural air cooling.
- the part thus obtained by the process according to the invention has high mechanical properties at room temperature, in particular because of its high martensite content of at least 80%.
- Rm is at least 1000 MPa
- Re is at least 800 MPa
- the elongation at break A measured according to ISO 6892 standard is at least 8%
- the bending angle capacity for a 1.5 mm thickness is at least 60 °, measured according to VDA 238-100.
- Table 2 shows the intermediate metallurgical structures (during the processing stages where the steel temperature is above Ms) and final structures of these same examples, with the mechanical properties of the final part: tensile strength Rm, elastic limit Rp0,2, elongation A, resilience KCU, bending angle capacity.
- MC designates the proportion of carbides.
- the invention also includes the cases where a sheet having the composition required by the invention is joined to a sheet having another composition, and where the assembly thus obtained is deformed by the process which has just been described.
- the structures and properties according to the invention will normally only be obtained on the part of the assembly having the composition of the invention.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Crystallography & Structural Chemistry (AREA)
- Thermal Sciences (AREA)
- Physics & Mathematics (AREA)
- Heat Treatment Of Articles (AREA)
- Heat Treatment Of Sheet Steel (AREA)
- Heat Treatment Of Steel (AREA)
- Shearing Machines (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SI201730319T SI3445878T1 (sl) | 2016-04-22 | 2017-03-21 | Postopek za proizvodnjo martenzitnih nerjavnih jeklenih delov iz pločevine |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IB2016052302 | 2016-04-22 | ||
PCT/IB2017/051636 WO2017182896A1 (fr) | 2016-04-22 | 2017-03-21 | Procédé de fabrication d'une pièce en acier inoxydable martensitique à partir d'une tôle |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3445878A1 EP3445878A1 (fr) | 2019-02-27 |
EP3445878B1 true EP3445878B1 (fr) | 2020-04-08 |
Family
ID=55911018
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP17713465.7A Active EP3445878B1 (fr) | 2016-04-22 | 2017-03-21 | Procédé de fabrication d'une pièce en acier inoxydable martensitique à partir d'une tôle |
Country Status (14)
Country | Link |
---|---|
US (1) | US11001916B2 (zh) |
EP (1) | EP3445878B1 (zh) |
JP (1) | JP6840771B2 (zh) |
KR (1) | KR102395730B1 (zh) |
CN (1) | CN109415776B (zh) |
AU (1) | AU2017252037A1 (zh) |
BR (1) | BR112018071587B1 (zh) |
CA (1) | CA3022115A1 (zh) |
ES (1) | ES2805067T3 (zh) |
HU (1) | HUE051293T2 (zh) |
MX (1) | MX2018012841A (zh) |
RU (1) | RU2724767C2 (zh) |
SI (1) | SI3445878T1 (zh) |
WO (1) | WO2017182896A1 (zh) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
HUE051293T2 (hu) * | 2016-04-22 | 2021-03-01 | Aperam | Eljárás martenzites rozsdamentes acél alkatrész gyártására lemezbõl |
US10619223B2 (en) | 2016-04-28 | 2020-04-14 | GM Global Technology Operations LLC | Zinc-coated hot formed steel component with tailored property |
US20180216205A1 (en) * | 2017-01-27 | 2018-08-02 | GM Global Technology Operations LLC | Two-step hot forming of steels |
EP3645764B1 (fr) * | 2017-06-30 | 2022-01-19 | Aperam | Procédé de soudage par points de tôles d'acier inoxydable martensitique |
WO2019086934A1 (fr) * | 2017-11-03 | 2019-05-09 | Aperam | Acier inoxydable martensitique, et son procédé de fabrication |
WO2019222950A1 (en) | 2018-05-24 | 2019-11-28 | GM Global Technology Operations LLC | A method for improving both strength and ductility of a press-hardening steel |
CN112534078A (zh) | 2018-06-19 | 2021-03-19 | 通用汽车环球科技运作有限责任公司 | 具有增强的机械性质的低密度压制硬化钢 |
JP6532990B1 (ja) * | 2018-07-18 | 2019-06-19 | 株式会社ソディック | 積層造形物の製造方法 |
CN110076246B (zh) * | 2019-04-25 | 2020-11-20 | 北京航星机器制造有限公司 | 一种可热处理强化铝合金高效热成形装备及方法 |
US11530469B2 (en) | 2019-07-02 | 2022-12-20 | GM Global Technology Operations LLC | Press hardened steel with surface layered homogenous oxide after hot forming |
CN113637924A (zh) * | 2020-04-27 | 2021-11-12 | 靖江市中信特种机械泵阀厂 | 一种醪液泵新型材料 |
CN111471940B (zh) * | 2020-04-29 | 2021-09-10 | 钢铁研究总院 | 一种高强度不锈钢转子及其制备方法 |
CN112251681B (zh) * | 2020-09-29 | 2022-03-18 | 中国科学院金属研究所 | 一种超高强度纳米晶40Cr16Co4W2Mo不锈钢及其制备方法 |
CN116867919A (zh) * | 2021-02-18 | 2023-10-10 | 日铁不锈钢株式会社 | 制动盘转子用马氏体系不锈钢板、制动盘转子及制动盘转子用马氏体系不锈钢板的制造方法 |
CN117286419A (zh) * | 2022-06-16 | 2023-12-26 | 通用电气公司 | 具有改善的韧度和强度的微合金化403Cb级马氏体不锈钢 |
WO2024057705A1 (ja) * | 2022-09-12 | 2024-03-21 | 株式会社プロテリアル | ステンレス鋼およびその製造方法、ならびに、ステンレス鋼製品およびその製造方法 |
DE102023003636A1 (de) | 2023-09-07 | 2024-07-04 | Mercedes-Benz Group AG | Verfahren und Vorrichtung zum Herstellen eines Formteils |
Family Cites Families (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS58123822A (ja) * | 1982-01-18 | 1983-07-23 | Daido Steel Co Ltd | 直接焼入方法 |
FR2567151B1 (fr) * | 1984-07-04 | 1986-11-21 | Ugine Aciers | Procede de fabrication de barres ou de fil machine en acier inoxydable martensitique et produits correspondants |
JPS6439323A (en) * | 1987-08-06 | 1989-02-09 | Sumitomo Metal Ind | Working method for high-temperature high-cr ferrite steel |
US7235212B2 (en) * | 2001-02-09 | 2007-06-26 | Ques Tek Innovations, Llc | Nanocarbide precipitation strengthened ultrahigh strength, corrosion resistant, structural steels and method of making said steels |
DE19546204C1 (de) * | 1995-12-11 | 1997-03-20 | Max Planck Inst Eisenforschung | Verfahren zur Herstellung von hochfesten Gegenständen aus einem Vergütungsstahl und Anwendung dieses Verfahrens zur Erzeugung von Federn |
FR2823226B1 (fr) * | 2001-04-04 | 2004-02-20 | V & M France | Acier et tube en acier pour usage a haute temperature |
JP4144283B2 (ja) * | 2001-10-18 | 2008-09-03 | 住友金属工業株式会社 | マルテンサイト系ステンレス鋼 |
FR2870546B1 (fr) * | 2004-05-21 | 2006-09-01 | Industeel Creusot | Acier a haute resistance mecanique et a l'usure |
RU2417272C2 (ru) * | 2006-10-05 | 2011-04-27 | ДжФЕ СТИЛ КОРПОРЕЙШН | Дисковый тормоз, обладающий отличным сопротивлением смягчающему отпуску и ударной вязкостью |
RU72697U1 (ru) * | 2007-08-22 | 2008-04-27 | Общество с ограниченной ответственностью "Каури" | Пруток из нержавеющей высокопрочной стали |
FR2920784B1 (fr) * | 2007-09-10 | 2010-12-10 | Aubert & Duval Sa | Acier inoxydable martensitique, procede de fabrication de pieces realisees en cet acier et pieces ainsi realisees |
AR073884A1 (es) * | 2008-10-30 | 2010-12-09 | Sumitomo Metal Ind | Tubo de acero inoxidable de alta resistencia excelente en resistencia a la fisuracion bajo tension por sulfuros y a la corrosion de gas de acido carbonico en alta temperatura. |
US8480817B2 (en) * | 2009-07-10 | 2013-07-09 | Rolls-Royce Corporation | Thermal mechanical processing of stainless steel |
WO2012169638A1 (ja) * | 2011-06-10 | 2012-12-13 | 株式会社神戸製鋼所 | 熱間プレス成形品、その製造方法および熱間プレス成形用薄鋼板 |
JP5768663B2 (ja) * | 2011-11-01 | 2015-08-26 | 新日鐵住金株式会社 | 熱間剪断加工方法 |
CA3014626A1 (en) * | 2013-09-10 | 2015-03-19 | Kabushiki Kaisha Kobe Seiko Sho (Kobe Steel, Ltd.) | Hot-pressing steel plate, press-molded article, and method for manufacturing press-molded article |
JP6002114B2 (ja) * | 2013-11-13 | 2016-10-05 | 日本精工株式会社 | マルテンサイト系ステンレス鋼による機構部品の製造方法および転がり軸受の製造方法 |
AT515157B1 (de) | 2013-11-21 | 2016-12-15 | Böhler Edelstahl GmbH & Co KG | Verfahren zur Herstellung von Kunststoffformen aus martensitischem Chromstahl und Kunststoffform |
CN105916608B (zh) * | 2014-01-30 | 2018-11-13 | 新日铁住金株式会社 | 钢板加热方法和钢板加热装置 |
WO2016174500A1 (fr) * | 2015-04-30 | 2016-11-03 | Aperam | Acier inoxydable martensitique, procédé de fabrication d'un demi-produit en cet acier et outil de coupe réalisé à partir de ce demi-produit |
US20190040506A1 (en) * | 2016-03-04 | 2019-02-07 | Hitachi Metals, Ltd. | Martensitic stainless steel member and method for manufacturing same, and martensitic stainless steel component and method for manufacturing same |
HUE051293T2 (hu) * | 2016-04-22 | 2021-03-01 | Aperam | Eljárás martenzites rozsdamentes acél alkatrész gyártására lemezbõl |
CN108315650A (zh) * | 2018-03-30 | 2018-07-24 | 宝钢不锈钢有限公司 | 一种马氏体不锈钢及其制造方法 |
-
2017
- 2017-03-21 HU HUE17713465A patent/HUE051293T2/hu unknown
- 2017-03-21 AU AU2017252037A patent/AU2017252037A1/en not_active Abandoned
- 2017-03-21 MX MX2018012841A patent/MX2018012841A/es unknown
- 2017-03-21 JP JP2018555193A patent/JP6840771B2/ja active Active
- 2017-03-21 BR BR112018071587-5A patent/BR112018071587B1/pt active IP Right Grant
- 2017-03-21 RU RU2018136969A patent/RU2724767C2/ru active
- 2017-03-21 KR KR1020187030500A patent/KR102395730B1/ko active IP Right Grant
- 2017-03-21 SI SI201730319T patent/SI3445878T1/sl unknown
- 2017-03-21 EP EP17713465.7A patent/EP3445878B1/fr active Active
- 2017-03-21 ES ES17713465T patent/ES2805067T3/es active Active
- 2017-03-21 CA CA3022115A patent/CA3022115A1/fr not_active Abandoned
- 2017-03-21 CN CN201780039084.1A patent/CN109415776B/zh active Active
- 2017-03-21 US US16/095,650 patent/US11001916B2/en active Active
- 2017-03-21 WO PCT/IB2017/051636 patent/WO2017182896A1/fr active Application Filing
Non-Patent Citations (1)
Title |
---|
None * |
Also Published As
Publication number | Publication date |
---|---|
MX2018012841A (es) | 2019-03-28 |
HUE051293T2 (hu) | 2021-03-01 |
CA3022115A1 (fr) | 2017-10-26 |
WO2017182896A1 (fr) | 2017-10-26 |
EP3445878A1 (fr) | 2019-02-27 |
CN109415776B (zh) | 2020-09-08 |
CN109415776A (zh) | 2019-03-01 |
KR102395730B1 (ko) | 2022-05-09 |
RU2018136969A (ru) | 2020-04-22 |
BR112018071587B1 (pt) | 2022-03-29 |
AU2017252037A1 (en) | 2018-11-22 |
RU2018136969A3 (zh) | 2020-05-15 |
ES2805067T3 (es) | 2021-02-10 |
BR112018071587A2 (pt) | 2019-02-12 |
KR20180136455A (ko) | 2018-12-24 |
US20190127829A1 (en) | 2019-05-02 |
JP6840771B2 (ja) | 2021-03-10 |
SI3445878T1 (sl) | 2020-08-31 |
JP2019518609A (ja) | 2019-07-04 |
US11001916B2 (en) | 2021-05-11 |
RU2724767C2 (ru) | 2020-06-25 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP3445878B1 (fr) | Procédé de fabrication d'une pièce en acier inoxydable martensitique à partir d'une tôle | |
EP3175006B1 (fr) | Procédé de fabrication de tôles d'acier pour durcissement sous presse, et pièces obtenues par ce procédé | |
EP0971044B1 (fr) | Tole d'acier laminée à chaud et à froid revêtue et présentant une très haute résistance après traitement thermique | |
EP2137327B1 (fr) | Acier pour formage a chaud ou trempe sous outil, a ductilite amelioree | |
CA2847809C (fr) | Acier lamine durcissant par precipitation apres formage a chaud et/ou trempe sous outil a tres haute resistance et ductilite et son procede de fabrication | |
EP3783116B1 (fr) | Tôles prerevêtues permettant la fabrication de pieces d'acier revêtues et durcies a la presse | |
EP3146083B1 (fr) | Tôle d'acier doublement recuite a hautes caracteristiques mecaniques de resistance et de ductilite, procede de fabrication et utilisation de telles tôles | |
EP1979583B1 (fr) | Procédé de fabrication d'une soupape de moteur à explosion, et soupape ainsi obtenue | |
EP3704280B1 (fr) | Acier inoxydable martensitique, et son procédé de fabrication | |
EP2957643A1 (fr) | Acier pour pièces mécaniques à hautes caractéristiques traitées superficiellement, et pièces mécaniques en cet acier et leur procédé de fabrication | |
FR2778672A1 (fr) | Procede de fabrication de pieces trempees en acier | |
EP3645764B1 (fr) | Procédé de soudage par points de tôles d'acier inoxydable martensitique | |
CA2559562C (fr) | Acier pour pieces mecaniques, procede de fabrication de pieces mecaniques l'utilisant et pieces mecaniques ainsi realisees | |
EP0922777A1 (fr) | Produit plat, tel que tÔle, d'un acier à haute limite d'élasticité montrant une bonne ductilité et procédé de fabrication de ce produit | |
WO2000003041A1 (fr) | Produit plat, tel que tole, d'un acier a haute limite d'elasticite montrant une bonne ductilite et procede de fabrication de ce produit |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: UNKNOWN |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE |
|
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 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE |
|
17P | Request for examination filed |
Effective date: 20181022 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
AX | Request for extension of the european patent |
Extension state: BA ME |
|
DAV | Request for validation of the european patent (deleted) | ||
DAX | Request for extension of the european patent (deleted) | ||
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: GRANT OF PATENT IS INTENDED |
|
INTG | Intention to grant announced |
Effective date: 20191113 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE PATENT HAS BEEN GRANTED |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP Ref country code: AT Ref legal event code: REF Ref document number: 1254459 Country of ref document: AT Kind code of ref document: T Effective date: 20200415 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 602017014425 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: FRENCH |
|
REG | Reference to a national code |
Ref country code: FI Ref legal event code: FGE |
|
REG | Reference to a national code |
Ref country code: SE Ref legal event code: TRGR |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: MP Effective date: 20200408 |
|
REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG4D |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IS 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: 20200808 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: 20200408 Ref country code: LT 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: 20200408 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: 20200709 Ref country code: NO 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: 20200708 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: 20200817 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MK05 Ref document number: 1254459 Country of ref document: AT Kind code of ref document: T Effective date: 20200408 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: RS 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: 20200408 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: 20200708 Ref country code: LV 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: 20200408 Ref country code: HR 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: 20200408 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AL 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: 20200408 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 602017014425 Country of ref document: DE |
|
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: 20200408 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: 20200408 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: 20200408 Ref country code: SM 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: 20200408 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: 20200408 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: 20200408 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2805067 Country of ref document: ES Kind code of ref document: T3 Effective date: 20210210 |
|
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: PL 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: 20200408 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: 20200408 |
|
REG | Reference to a national code |
Ref country code: HU Ref legal event code: AG4A Ref document number: E051293 Country of ref document: HU |
|
26N | No opposition filed |
Effective date: 20210112 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20200408 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210331 Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210321 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210331 Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20210321 |
|
P01 | Opt-out of the competence of the unified patent court (upc) registered |
Effective date: 20230524 |
|
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: 20200408 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MK 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: 20200408 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: HU Payment date: 20240226 Year of fee payment: 8 Ref country code: FI Payment date: 20240222 Year of fee payment: 8 Ref country code: DE Payment date: 20240307 Year of fee payment: 8 Ref country code: GB Payment date: 20240325 Year of fee payment: 8 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: SI Payment date: 20240221 Year of fee payment: 8 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: TR Payment date: 20240308 Year of fee payment: 8 Ref country code: SE Payment date: 20240319 Year of fee payment: 8 Ref country code: IT Payment date: 20240312 Year of fee payment: 8 Ref country code: FR Payment date: 20240221 Year of fee payment: 8 Ref country code: BE Payment date: 20240326 Year of fee payment: 8 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: ES Payment date: 20240405 Year of fee payment: 8 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MT 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: 20200408 |