WO2024003593A1 - Pièce forgée en acier et son procédé de fabrication - Google Patents
Pièce forgée en acier et son procédé de fabrication Download PDFInfo
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- WO2024003593A1 WO2024003593A1 PCT/IB2022/055992 IB2022055992W WO2024003593A1 WO 2024003593 A1 WO2024003593 A1 WO 2024003593A1 IB 2022055992 W IB2022055992 W IB 2022055992W WO 2024003593 A1 WO2024003593 A1 WO 2024003593A1
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- Prior art keywords
- steel
- steel part
- temperature
- anyone
- martensite
- Prior art date
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- 229910000831 Steel Inorganic materials 0.000 title claims abstract description 131
- 239000010959 steel Substances 0.000 title claims abstract description 131
- 238000004519 manufacturing process Methods 0.000 title claims description 17
- 229910000734 martensite Inorganic materials 0.000 claims abstract description 32
- 229910001563 bainite Inorganic materials 0.000 claims abstract description 30
- 230000005540 biological transmission Effects 0.000 claims abstract description 28
- 239000010955 niobium Substances 0.000 claims abstract description 23
- 239000000203 mixture Substances 0.000 claims abstract description 20
- 229910001566 austenite Inorganic materials 0.000 claims abstract description 16
- 229910052758 niobium Inorganic materials 0.000 claims abstract description 15
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 12
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 12
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims abstract description 12
- 229910000859 α-Fe Inorganic materials 0.000 claims abstract description 12
- 229910052757 nitrogen Inorganic materials 0.000 claims abstract description 11
- 239000002244 precipitate Substances 0.000 claims abstract description 11
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 10
- 229910001567 cementite Inorganic materials 0.000 claims abstract description 7
- KSOKAHYVTMZFBJ-UHFFFAOYSA-N iron;methane Chemical compound C.[Fe].[Fe].[Fe] KSOKAHYVTMZFBJ-UHFFFAOYSA-N 0.000 claims abstract description 7
- 229910052742 iron Inorganic materials 0.000 claims abstract description 6
- 230000001186 cumulative effect Effects 0.000 claims abstract description 5
- 239000012535 impurity Substances 0.000 claims abstract description 5
- 229910001562 pearlite Inorganic materials 0.000 claims abstract description 4
- 238000012545 processing Methods 0.000 claims abstract description 4
- 238000000034 method Methods 0.000 claims description 21
- 238000001816 cooling Methods 0.000 claims description 16
- 229910052799 carbon Inorganic materials 0.000 claims description 14
- 238000005242 forging Methods 0.000 claims description 14
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 13
- 238000010438 heat treatment Methods 0.000 claims description 12
- 229910052710 silicon Inorganic materials 0.000 claims description 11
- 239000011265 semifinished product Substances 0.000 claims description 10
- 239000010703 silicon Substances 0.000 claims description 10
- 229910052750 molybdenum Inorganic materials 0.000 claims description 8
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims description 7
- 238000000137 annealing Methods 0.000 claims description 7
- 239000011733 molybdenum Substances 0.000 claims description 7
- 238000005255 carburizing Methods 0.000 claims description 6
- 238000002791 soaking Methods 0.000 claims description 4
- 238000003303 reheating Methods 0.000 claims description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 18
- 230000015572 biosynthetic process Effects 0.000 description 12
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 10
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 9
- 229910052759 nickel Inorganic materials 0.000 description 9
- 239000010410 layer Substances 0.000 description 8
- 239000011651 chromium Substances 0.000 description 7
- 230000001627 detrimental effect Effects 0.000 description 7
- 239000011572 manganese Substances 0.000 description 7
- 230000009466 transformation Effects 0.000 description 7
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 6
- 229910052804 chromium Inorganic materials 0.000 description 6
- 229910052748 manganese Inorganic materials 0.000 description 6
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 5
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 5
- 150000001247 metal acetylides Chemical class 0.000 description 5
- 238000005096 rolling process Methods 0.000 description 5
- 238000012360 testing method Methods 0.000 description 5
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 4
- 239000005864 Sulphur Substances 0.000 description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 4
- 230000002411 adverse Effects 0.000 description 4
- 230000007423 decrease Effects 0.000 description 4
- 229910052698 phosphorus Inorganic materials 0.000 description 4
- 239000011574 phosphorus Substances 0.000 description 4
- 238000005728 strengthening Methods 0.000 description 4
- 239000010936 titanium Substances 0.000 description 4
- 229910052719 titanium Inorganic materials 0.000 description 4
- -1 Niobium carbides Chemical class 0.000 description 3
- 239000011575 calcium Substances 0.000 description 3
- 238000005266 casting Methods 0.000 description 3
- 239000010949 copper Substances 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000001556 precipitation Methods 0.000 description 3
- 239000006104 solid solution Substances 0.000 description 3
- 238000007711 solidification Methods 0.000 description 3
- 230000008023 solidification Effects 0.000 description 3
- 239000000126 substance Substances 0.000 description 3
- CADICXFYUNYKGD-UHFFFAOYSA-N sulfanylidenemanganese Chemical compound [Mn]=S CADICXFYUNYKGD-UHFFFAOYSA-N 0.000 description 3
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 2
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 2
- 229910052684 Cerium Inorganic materials 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 2
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 2
- 239000004411 aluminium Substances 0.000 description 2
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 2
- 229910052797 bismuth Inorganic materials 0.000 description 2
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth atom Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 description 2
- 229910052796 boron Inorganic materials 0.000 description 2
- 229910052791 calcium Inorganic materials 0.000 description 2
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical compound [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 238000009792 diffusion process Methods 0.000 description 2
- 238000000227 grinding Methods 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 239000011777 magnesium Substances 0.000 description 2
- 229910052749 magnesium Inorganic materials 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- 238000001953 recrystallisation Methods 0.000 description 2
- 238000012827 research and development Methods 0.000 description 2
- 238000005204 segregation Methods 0.000 description 2
- 238000007493 shaping process Methods 0.000 description 2
- 239000002344 surface layer Substances 0.000 description 2
- 238000005496 tempering Methods 0.000 description 2
- 229910052718 tin Inorganic materials 0.000 description 2
- 229910052720 vanadium Inorganic materials 0.000 description 2
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 2
- 229910052726 zirconium Inorganic materials 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- PMHQVHHXPFUNSP-UHFFFAOYSA-M copper(1+);methylsulfanylmethane;bromide Chemical compound Br[Cu].CSC PMHQVHHXPFUNSP-UHFFFAOYSA-M 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000007571 dilatometry Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000005098 hot rolling Methods 0.000 description 1
- BHEPBYXIRTUNPN-UHFFFAOYSA-N hydridophosphorus(.) (triplet) Chemical compound [PH] BHEPBYXIRTUNPN-UHFFFAOYSA-N 0.000 description 1
- 238000011068 loading method Methods 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
- 239000000463 material Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 238000010606 normalization Methods 0.000 description 1
- 238000004881 precipitation hardening Methods 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 230000000979 retarding effect Effects 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 239000011593 sulfur Substances 0.000 description 1
Classifications
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- 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
- 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
- C21D1/06—Surface hardening
-
- 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
- C21D1/26—Methods of annealing
-
- 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
- C21D1/74—Methods of treatment in inert gas, controlled atmosphere, vacuum or pulverulent material
- C21D1/76—Adjusting the composition of the atmosphere
-
- 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
- C21D6/02—Hardening by precipitation
-
- 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
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/28—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for plain shafts
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/32—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for gear wheels, worm wheels, or the like
-
- 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
- C22C38/02—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
- C22C38/40—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
- C22C38/48—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
Definitions
- the present invention relates to steel suitable for forging mechanical parts of steel for automobiles and particularly to the steel suitable for manufacturing of gear, shafts and other transmission parts for the transmission system of an automobile.
- Transmission parts such as gears, shafts, differentials and other parts of a transmission system of an automobile works under the conditions of high rotating speed and high load and continuous alternation of rotating speed and load.
- the transmission parts it is necessary for the transmission parts to have high strength, high hardness and good wear resistance specifically the contact surface of these parts whereas the core of the transmission parts are required to have good durability, and meanwhile, the meshing precision of the transmission parts is required to be high and the working noise is required to be low.
- US20070193658A1 is a steel for mechanical components, wherein the composition thereof is, in percentages by weight: 0.19% ⁇ C ⁇ 0.25%; 1.1% ⁇ Mn ⁇ 1.5%; 0.8% ⁇ Si ⁇ 1.2%; 0.01% ⁇ S ⁇ 0.09%; trace levels ⁇ P ⁇ 0.025%; trace levels ⁇ Ni ⁇ 0.25%; 1% ⁇ Cr ⁇ 1.4%; 0.10% ⁇ Mo ⁇ 0.25%; trace levels ⁇ Cu ⁇ 0.30%; 0.010% ⁇ Al ⁇ 0.045%; 0.010% ⁇ Nb ⁇ 0.045%; 0.0130% ⁇ N ⁇ 0.0300%; optionally trace levels ⁇ Bi ⁇ 0.10% and/or trace levels ⁇ Pb ⁇ 0.12% and/or trace levels ⁇ Te ⁇ 0.015% and/or trace levels ⁇ Se ⁇ 0.030% and/or trace levels ⁇ Ca ⁇ 0.0050%; the balance
- WO2020/178854 provides a steel composition for high temperature carburizing and a steel article made from the steel composition.
- the composition comprises: a) 0.11 to 0.3 wt.% of Carbon, b) 1.1 to 1.4 wt. % of Manganese, c) 0.15 to 0.35wt. % of Silicon, d) 1 to 1.3 wt. % of Chromium, e) ⁇ 0.0006 wt. % of Boron, f) 0.04 to 0.05 wt.
- a steel part for the transmission system of an automobile that simultaneously have: an ultimate tensile strength greater than or equal to 1600 MPa and preferably above 1650 MPa, a yield strength greater than or equal to 1330 MPa, an impact toughness of 53J/cm2 or less and preferably 50J/cm2 or less when measured for a KCU type of sample, a YS/TS ratio equal to 0.80 or more,
- a steel part according to the invention presents a surface hardness of 650HV or more from a surface depth of 0.4mm to 0.6mm.
- such steel is suitable for manufacturing of a forged steel parts for the transmission system of an automobile wherein each part can have a cross section up to 150mm *150 mm and the steel is also suitable for other parts of an automobiles such as chassis members.
- Another object of the present invention is also to make available a method for the manufacturing of these mechanical parts that is compatible with conventional industrial applications while being robust towards manufacturing parameters shifts.
- Carbon is present in the steel of present invention is from 0.2% to 0.35%. Carbon is an element necessary for increasing the strength of the Steel of present invention by producing a lowtemperature transformation phases such as Bainite, But Carbon content less than 0.2% will not be able to impart the tensile strength to the steel of present invention.
- the toughness is adversely impacted due to the excessive formation of proeutectoid cementite during the cooling after hot rolling or forging. Further excessive formation of proeutectoid cementite is also detrimental for mechanical operations on the part of the transmission system such as hobbling, lapping, shaping drilling, honing or grinding.
- the carbon content is advantageously in the range 0.22% to 0.35% and more especially 0.25% to 0.30%.
- Manganese is added in the present steel from 1.0% to 1.6%. This element is gammagenous. Manganese provides solid solution strengthening and suppresses the ferritic transformation temperature and reduces ferritic transformation rate hence assist in the formation of bainite.
- An amount of at least 1.0% is required to impart strength as well as to assist the formation of Bainite. But when Manganese content is present more than 1.6% it cause segregation which results in banded microstructure after annealing and this banded microstructure is deferential to the mechanical properties of the steel of present invention. process.
- the preferred limit for the presence of Manganese is from 1.1% to 1.5% and more preferably from 1.1% to 1.4%.
- Silicon is present in the steel of present invention from 0.2% to 0.7%. Silicon imparts the steel of present invention with strength through solid solution strengthening and also acts as a deoxidizer. Silicon is a constituent that can retard the precipitation of carbides during cooling after mechanical operation, therefore, Silicon promotes formation of Bainite.
- Silicon is also a ferrite former and also increases the Ac3 transformation point which will push the austenitic temperature to higher temperature ranges that is why the content of Silicon is kept at a maximum of 0.7%.Further Silicon higher than 0.7% also enhances segregation.
- the preferred limit for the presence of Silicon is from 0.2% to 0.6% and more preferably from 0.22% to 0.4%.
- the content of the Aluminum is from 0.001% to 0.1%. Aluminum removes Oxygen existing in molten steel to prevent Oxygen from forming a gas phase during solidification process. Aluminum also fixes Nitrogen in the steel to form Aluminum nitride to reduce the size of the grains. But the deoxidizing effect saturates for aluminum content more than 0.1%.
- Aluminum also controls the grain size of the present steel by forming AlN. Higher content of Aluminum above 0.1% lead to the occurrence of coarse aluminum rich oxides that deteriorate machinability and hot forging on steel.
- the preferred limit for the presence of Aluminium is from 0.01% to 0.09% and more preferably from 0.01 to 0.035%
- Molybdenum is an essential element and may be present from 0.01 % to 0.5% in the present invention. Molybdenum is added to impart hardenability and hardness to steel by forming Molybdenum based carbides and also promote the formation of Martensite during the carburization and also retard the formation of coarse Niobium carbides or Niobium Carbonitrides.
- Niobium is an essential element for the Steel of present invention from 0.020% to 0.06% and suitable for forming carbonitrides to impart strength of the Steel of present invention by precipitation hardening. Niobium will also impact the size of microstructural components through its precipitation as carbonitrides and by retarding the recrystallization during heating process. Thus, microstructure formed at the end of the holding temperature and as a consequence after the complete austenitization lead to the hardening of the product.
- Niobium content above 0.06% is not economically interesting as well as forms coarser precipitates which are detrimental for the fatigue properties, impact toughness of the steel and also when the content of niobium is 0.06% or more niobium is also detrimental for steel hot ductility resulting in difficulties during steel casting and rolling.
- the preferred limit for niobium content is from 0.025% to 0.058% and more preferably from 0.025% to 0.055%.
- Chromium is present from 1% to 1.5% in the steel of present invention.
- Chromium is an essential element that provide strength to the steel by solid solution strengthening and a minimum of 1% is required to impart the strength but when used above 1.5% increase the hardenability is beyond an acceptable limit due the formation of coarse cementite after cooling thereby impairing the forgeability as well as the ductility of the steel. Chromium addition also decreases the diffusion coefficient of carbon in the austenite same as nickel hence promote the formation of martensite during carburization
- the preferred limit for the presence of Chromium is from 1.1% to 1.4 % and more preferably from 1.1% to 1.3%.
- Phosphorus is content of the steel of present invention is from 0 % to 0.09%. Phosphorus tends to segregate at the grain boundaries or cosegregate with Manganese.
- phosphorus As less as possible. Specifically, content over 0.05% can cause rupture by intergranular interface decohesion which may be detrimental for the fatigue limit.
- the preferred limit for Phosphorus content is from 0% to 0.05%.
- Sulphur is contained from 0 % to 0.09%. Sulphur forms MnS precipitates which improve the machinability and assists in obtaining a sufficient machinability. During metal forming processes such as rolling and forming, deformable manganese sulfide (MnS) inclusions become elongated.
- Such elongated MnS inclusions can have considerable adverse effects on mechanical properties such as striction and impact toughness if the inclusions are not aligned with the loading direction further higher sulphur content is also detrimental for the forgeability of the steel. Therefore, sulfur content is limited to 0.09%.
- a preferable range the content of Sulphur is 0 % from 0.05% and more preferably from 0% to 0.040%to obtain the best balance between machinability and fatigue limit.
- Nitrogen is in an amount from 0.009% % and 0.09% in steel of present invention. It seems that Nb(C,N) precipitated nucleate on AlN precipitates. To obtain the Nb(C,N) precipitates, a minimum of 0.009% nitrogen is required.
- the preferred limit for nitrogen is from 0.009% to 0.05% and more preferably from 0.009% to 0.04%
- Nickel is added to the present invention from 0% to 1% to increase the strength of the steel present invention and to improve toughness specially after Normalizing and carburizing. Nickel is beneficial in improving its pitting corrosion resistance. A minimum of 0.1% is required to get such effects. Nickel is added into the steel composition to decreases the diffusion coefficient of carbon in the austenite thereby promoting the formation of martensite during the Carburization process as well as low temperature phases such as bainite. But the presence of nickel content above 1% lowers the martensite start temperature hence leading to the excessive stabilization of residual austenite thereby having a detrimental impact on tensile strength and yield strength.
- Nickel is also restricted to 1% due to the economic reasons. It is preferred to have nickel from 0.1% to 0.9% in the steel of present invention. Vanadium is an optional element for the present invention and is content is from 0% to 0.2%. Vanadium is effective in enhancing the strength of steel by precipitation strengthening especially by forming carbides or carbonitrides. Upper limit is kept at 0.2% due to the economic reasons.
- the steel of present invention is always Titanium free due to the reason that Titanium forms coarse is an optional element and present from 0% to 0.1%. Titanium forms titanium nitrides which impart steel with strength, but these nitrides may form during solidification process, therefore have a detrimental effect fatigue limit. Hence the preferred limit for titanium is from 0% to 0.05%.
- Copper is a residual element and may be present up to 1% due to processing of steel. Till 0.5% copper does not impact any of the properties of steel but over 0.5% the hot workability decreases significantly.
- Other elements such as Tin, Cerium, Calcium, Bismuth, Magnesium or Zirconium can be added individually or in combination in the following proportions by weight: Tin ⁇ 0.1%, Cerium ⁇ 0.1%, Magnesium ⁇ 0.10%, Calcium ⁇ 0.0010%, Bismuth ⁇ 0.05%, 0% ⁇ Boron ⁇ 0.008% and Zirconium ⁇ 0.10%. Up to the maximum content levels indicated, these elements make it possible to refine the grain during solidification. The remainder of the composition of the Steel consists of iron and inevitable impurities resulting from processing.
- the rest of the composition is iron and unavoidable impurities, in particular resulting from the elaboration. More particularly, the composition of the steel part consists of the abovementioned elements.
- the steel part for the transmission system of an automobile has a microstructure comprising, in surface fractions or area%, of at least 90% bainite, an optional cumulative presence of Residual Austenite, Pearlite, ferrite and martensite from 0% to 10% and the precipitates of Al and Nb in form of AlN and Nb(C,N).
- Bainite is present in the steel according to the invention as a matrix phase and imparts strength to such steel. Bainite is present in the steel at least 90% by area fraction and preferably from 90% to 100% by area fraction and more preferably from 95% to 100%.
- Such bainite may include CementiteFree LathLike Bainite, granular bainite, Upper bainite and Lower bainite or any other bainite.
- the cementite free LathLike bainite is consisting of bainite in the form of laths and including, between these laths, carbides such that the number N of interlath carbides larger than 0.1 micrometers per unit of surface area is less than or equal to 50000/mm 2 .
- This cementitefree lathlike bainite structure can confer to the steel of present invention high strength as well as impact toughness.
- the lower bainite is consisting of bainite in the form of laths and including, fine iron carbides stick which are precipitated inside the laths.
- the lower bainite structure can provide the steel of present invention with elongation and tensile strength.
- Precipitates of Al and Nb are present in the steel according to the invention as AlN and Niobium Carbonitrides Nb(C,N) respectively. These precipitates preferably have a size from 20nm to 350nm. Precipitate formation takes place during the annealing process as well as the cooling step.
- the precipitates of the present invention are responsible for the pinning of the prior Austenite grains during Carburizing process thereby assisting in the formation of Bainite and Martensite of the martensite enriched layer present invention in targeted amounts.
- the prior austenite grain size is from 3 to 12 measured as per the ASTM grain Index. It is more preferable to have prior austenite grain size from 4 to 11 and more preferably from 4 to 10.
- the cumulative presence of Residual Austenite, Pearlite, ferrite and martensite does not affect adversely to the present invention till 10% but above 10% the mechanical properties may get impacted adversely. Residual Austenite may impart toughness and ductility to the steel of present invention.
- Martensite of the present invention may imparts strength and fatigue endurance to steel.
- the preferred limit for the cumulative presence ferrite and bainite is kept from 0% to 8% and more preferably from 0% to 4%.
- this microstructure in the core of the steel part also includes a martensiticenriched layer on all the surfaces of the steel part of the transmission system of an automobile up to a depth of 1mm or less and preferably up to a depth of 0.8mm or less and more preferably 0.5mm or less and showing a martensite percentage from 85% to 95% in area fraction, preferably from 85% to 92% more preferably from 85% to 90%.
- the martensite enriched layer formed on the surfaces preferably comprises any or all possible martensite kinds and notably fresh martensite, tempered martensite etc.
- This martensite layer imparts the steel of the invention with a surface hardness of 650 Hv or more which provides the final steel part good resistance against the wear and also impart the precision during the meshing of part with each other during rotary operation of transmission system.
- the remaining part of this surface layer comprises of anyone or more from bainite, residual austenite, ferrite and cementite.
- a steel part for the transmission system of an automobile according to the invention can be produced by any suitable manufacturing process, with the stipulated process parameters explained hereinafter. A preferred exemplary method is demonstrated herein but this example does not limit the scope of the disclosure and the aspects upon which the examples are based.
- the steel part considered for demonstrating preferred process according to the present invention is a gear.
- a preferred method consists in providing a semifinished casting of steel with a chemical composition according to the invention.
- the casting can be done in any form such as ingots or blooms or billets which is capable of being manufactured or processed into a steel part that can have a cross section up to 150mm*150 mm.
- the steel having the abovedescribed chemical composition is casted into a billet and then rolled in form of a bar. This bar can act as a semifinished product for further process steps of manufacturing.
- a preferred Semifinished product has a cross section be from ⁇ 20mmto ⁇ 110mm
- the semifinished product after the rolling process can be used directly at a high temperature after the rolling or may be first cooled to room temperature and then reheated for hot forging at a temperature ranging from Ac3 + 30° C to 1300° C.
- the Ac3 for the present steel is calculated by a dilatometry study.
- the temperature of the semifinished which is subjected to hot forging, is preferably at least 1150° C and must be below 1300°C because the temperature of the semifinished product is lower than 1150° C, excessive load is imposed on forging dies and, further, the temperature of the steel may decrease to a Ferrite transformation temperature during finishing forging, whereby the steel will be forged in a state in which transformed Ferrite contained in the structure. Therefore, the temperature of the semifinished product is preferably sufficiently high so that hot forging can be completed in the austenitic temperature range. Reheating at temperatures above 1300°C must be avoided because they are industrially expensive.
- a final finishing forging temperature herein after referred as Tforging, must be kept above 830°C to have a structure that is favorable to recrystallization and forging. It is preferred to have final forging to be performed at a temperature greater than Ac3+100°C and preferably above Ac3+200°C because below this temperature the steel bar exhibits a significant drop in forging.
- the hot forged part is thus obtained in this manner and then this hot forged steel part is cooled to room temperature. The hot forged steel part is then subjected to annealing to reduce the hardness of the steel part for further machining.
- the hot forged steel part is subjected to heating to reach the soaking temperature TA from 600°C to Ac3 +200°C, the preferred TA temperature is from 625°C to Ac3 +100°, more preferably from 640°C to Ac3 +50°C.
- hot forged steel part is heated from room temperature to soaking temperature TA at a heating rate HR1 from 0.1°C/s to 100°C/s. It is preferred to have HR1 rate from 0.1°C/s to 50°C/s and more preferably from 0.1°C/s to 10°C/s.
- the hot forged steel part is held at the annealing soaking temperature TA during 10 to 1000 seconds to ensure adequate transformation to Austenite microstructure of the strongly workhardened initial structure thereby reducing the hardness of the hot forged steel part. It is Then the hot forged steel part is cooled is at a cooling rate CR1 which is more than 1°C/s and preferably more than 2°C/s and more preferably more than 5°C/s to a cooling stop temperature range CS1 from Ms5°C to 15°C and preferably from Ms5°C to 20°C and more preferably from Ms10°C to 20°C.
- a cooling rate CR1 which is more than 1°C/s and preferably more than 2°C/s and more preferably more than 5°C/s to a cooling stop temperature range CS1 from Ms5°C to 15°C and preferably from Ms5°C to 20°C and more preferably from Ms10°C to 20°C.
- Mechanical operation may comprise hobbling, shaping, machining, grinding, honing or any other suitable mechanical operation or manufacturing procedure.
- the mechanical operations can be performed at room temperature or a higher temperature as desired by condition of specific mechanical operation.
- the forged steel part is then subjected to carburization to form the martensite enriched layer on all the surfaces of the steel part and also impart the steel part of present invention with targeted microstructure and mechanical properties
- the forged steel part is subjected to heating to reach the carburization temperature TZ from 800°C to 1100°C,
- the preferred TZ temperature is from 850°C to 1080°C , more preferably from 900°C to 1080°C.
- forged steel part is heated from room temperature to TZ at a heating rate HR2 from 0.1°C/s to 20°C/s. It is preferred to have HR2 rate from 0.1°C/s to 10°C/s and more preferably from 0.1°C/s to 5°C/s. Then the forged steel part is held at the TZ during 10 to 3600 seconds in an Carbon enriched atmosphere having a dew point of from 15°C to +15°C.
- the Carburizing treatment is intended to fuse the carbon from the Carbon enriched atmosphere into the surface of the the forged steel part at high temperature which will transformation the microstructure of the surface of the forged steel part into martensite.
- This enriched martensite layer can be up to a depth of 1mm or less and preferably up to a depth of 0.8 mm or less and more preferably up to a depth of 0.5mm or less.
- the forged steel part is cooled is at a cooling rate CR2 which is more than 1°C/s and preferably more than 2°C/s and more preferably more than 5°C/s to a cooling stop temperature range CS2 from Ms5°C to 15°C and preferably from Ms5°C to 20°C and more preferably from Ms10°C to 20°C to obtain a steel part for the transmission system of an automobile.
- the obtained steel part for the transmission system of an automobile may optionally be reheated to a tempering temperature Ttemper from 150°C to 250°C with a heating rate of at least 1°C/s and preferably of at least 2°C/s and more of at least 10°C/s during 100 s to 600s.
- the preferred temperature range for tempering is from 180°C to 240°C and the preferred duration for holding at Ttemper is from 200 s to 500s.
- Table 1 Forged mechanical part made of steels with different compositions is gathered in Table 1, where the forged mechanical part is produced according to process parameters as stipulated in Table 2, respectively. Thereafter Table 3 gathers the microstructures of the forged mechanical part obtained during the trials and table 4 gathers the result of evaluations of obtained properties.
- Table 1 Table 2
- Table 2 gathers the process parameters implemented on semifinished product made of steels of Table 1.
- the steels 1 and 2 serve for the manufacture of forged mechanical part according to the invention.
- This table also specifies the steels for reference forged mechanical parts which are steels 3 and 4.
- Table 3 gathers the results of test conducted in accordance of standards on different microscopes such as Scanning Electron Microscope for determining microstructural composition of both the inventive steel and reference trials and Xray measurements.
- Table 4 exemplifies the mechanical properties of both the inventive steel parts and reference steel parts.
- tests are conducted in accordance of NF EN ISO 68921 standards.
- Tests to measure the toughness and fatigue are conducted in accordance of EN ISO 1481 standard KCU specimen with U notch at toom temperature.
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Abstract
La présente invention concerne une pièce en acier pour le système de transmission d'une automobile comprenant les éléments suivants, 0,2 % ≦ C ≦ 0,35 % ; 1,0 % ≦ Mn ≦ 1,6 % ; 0,2 % ≦ Si ≦ 0,7 % ; 0,001 % ≦ Al ≦ 0,1 % ; 0,01 % ≦ Mo ≦ 0,5 % ; 0,020 % ≦ Nb ≦ 0,06 % ; 1 % ≦ Cr ≦ 1,5 % ; 0 ≦ P ≦ 0,09 % ; 0 ≦ S ≦ 0,09 % ; 0,009 % ≦ N ≦ 0,09 % ; 0 % ≦ Ni ≦ 1 % ; 0 % ≦ V ≦ 0,2 % ; 0 % ≦ Ti ≦ 0,1 % ; 0 % ≦ Cu ≦ 1 % ; 0 % ≦ B ≦ 0,008 % ; 0 % ≦ Sn ≦ 0,1 % ; 0 % ≦ Ce ≦ 0,1 % ; 0 % ≦ Mg ≦ 0,10 % ; 0 % ≦ Zr ≦ 0,10 % ; la composition restante étant composée de fer et d'impuretés inévitables provoquées par le traitement, la microstructure du noyau de ladite pièce en acier comprenant, par pourcentage de surface, au moins 90 % de baïnite, avec une présence facultative cumulative d'un élément quelconque ou plusieurs parmi l'austénite résiduelle, la perlite, la ferrite ou la martensite à partir de 0 % et 10 % et des précipités d'aluminium et de niobium sous la forme d'AlN et de Nb (C,N), une telle pièce en acier ayant une couche enrichie en martensite jusqu'à une profondeur de 1 mm ou moins sur toutes les surfaces de ladite pièce en acier, une telle couche enrichie en martensite comprenant de 85 % à 95 % de martensite, le reste étant un ou plusieurs éléments quelconques parmi la baïnite, l'austénite résiduelle, la ferrite ou la cémentite.
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JP4050829B2 (ja) * | 1998-07-30 | 2008-02-20 | 新日本製鐵株式会社 | 転動疲労特性に優れた浸炭材 |
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JP2020117789A (ja) * | 2019-01-25 | 2020-08-06 | Jfeスチール株式会社 | 自動車変速機用リングギアおよびその製造方法 |
WO2020178854A2 (fr) | 2019-03-04 | 2020-09-10 | Bharat Forge Limited | Acier pour carburation à haute température et son procédé de préparation |
US20210381088A1 (en) * | 2018-10-31 | 2021-12-09 | Jfe Steel Corporation | Steel for nitrocarburizing and nitrocarburized component, and methods of producing same |
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JPH0953148A (ja) * | 1995-08-11 | 1997-02-25 | Kobe Steel Ltd | 高靭性肌焼き鋼製機械部品およびその製法 |
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