US20220177993A1 - Ferritic stainless steel sheet for automobile brake disk rotors, automobile brake disk rotor, and hot-stamped article for automobile brake disk rotors - Google Patents
Ferritic stainless steel sheet for automobile brake disk rotors, automobile brake disk rotor, and hot-stamped article for automobile brake disk rotors Download PDFInfo
- Publication number
- US20220177993A1 US20220177993A1 US17/598,613 US202017598613A US2022177993A1 US 20220177993 A1 US20220177993 A1 US 20220177993A1 US 202017598613 A US202017598613 A US 202017598613A US 2022177993 A1 US2022177993 A1 US 2022177993A1
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- United States
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- steel sheet
- stainless steel
- automobile brake
- disc rotor
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- 229910001220 stainless steel Inorganic materials 0.000 title claims abstract description 64
- 239000002244 precipitate Substances 0.000 claims abstract description 71
- 239000013078 crystal Substances 0.000 claims abstract description 55
- 239000012535 impurity Substances 0.000 claims abstract description 9
- 229910052742 iron Inorganic materials 0.000 claims abstract description 9
- 229910000831 Steel Inorganic materials 0.000 claims description 79
- 239000010959 steel Substances 0.000 claims description 79
- 238000010438 heat treatment Methods 0.000 claims description 38
- 239000010935 stainless steel Substances 0.000 claims description 23
- 239000000047 product Substances 0.000 claims description 18
- 230000000717 retained effect Effects 0.000 claims description 2
- 230000007797 corrosion Effects 0.000 description 24
- 238000005260 corrosion Methods 0.000 description 24
- 230000000694 effects Effects 0.000 description 21
- 238000001556 precipitation Methods 0.000 description 21
- 238000005728 strengthening Methods 0.000 description 18
- 230000003647 oxidation Effects 0.000 description 16
- 238000007254 oxidation reaction Methods 0.000 description 16
- 230000000052 comparative effect Effects 0.000 description 15
- 238000005336 cracking Methods 0.000 description 15
- 239000000463 material Substances 0.000 description 14
- 238000005098 hot rolling Methods 0.000 description 12
- 238000007670 refining Methods 0.000 description 12
- 229910052799 carbon Inorganic materials 0.000 description 10
- 229910052761 rare earth metal Inorganic materials 0.000 description 9
- 229910001018 Cast iron Inorganic materials 0.000 description 8
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 8
- 229910052757 nitrogen Inorganic materials 0.000 description 8
- 239000006104 solid solution Substances 0.000 description 8
- 238000004804 winding Methods 0.000 description 7
- 230000014759 maintenance of location Effects 0.000 description 6
- 238000004519 manufacturing process Methods 0.000 description 6
- 229910052750 molybdenum Inorganic materials 0.000 description 6
- 229910052758 niobium Inorganic materials 0.000 description 6
- 238000001816 cooling Methods 0.000 description 5
- 229910052735 hafnium Inorganic materials 0.000 description 5
- 229910052715 tantalum Inorganic materials 0.000 description 5
- 229910052726 zirconium Inorganic materials 0.000 description 5
- 238000005266 casting Methods 0.000 description 4
- 229910001068 laves phase Inorganic materials 0.000 description 4
- 238000003754 machining Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 238000005096 rolling process Methods 0.000 description 4
- 238000009864 tensile test Methods 0.000 description 4
- 229910052719 titanium Inorganic materials 0.000 description 4
- 238000000137 annealing Methods 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 3
- 230000001747 exhibiting effect Effects 0.000 description 3
- JEIPFZHSYJVQDO-UHFFFAOYSA-N iron(III) oxide Inorganic materials O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 description 3
- 229910000734 martensite Inorganic materials 0.000 description 3
- 229910001105 martensitic stainless steel Inorganic materials 0.000 description 3
- 238000003825 pressing Methods 0.000 description 3
- 238000009628 steelmaking Methods 0.000 description 3
- 229910052721 tungsten Inorganic materials 0.000 description 3
- 230000002159 abnormal effect Effects 0.000 description 2
- 230000002542 deteriorative effect Effects 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 238000003384 imaging method Methods 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 229910052717 sulfur Inorganic materials 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 229910052765 Lutetium Inorganic materials 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052787 antimony Inorganic materials 0.000 description 1
- 229910052785 arsenic Inorganic materials 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000000339 bright-field microscopy Methods 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 238000009749 continuous casting Methods 0.000 description 1
- 238000006477 desulfuration reaction Methods 0.000 description 1
- 230000023556 desulfurization Effects 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 150000004678 hydrides Chemical class 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 238000009863 impact test Methods 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 229910052747 lanthanoid Inorganic materials 0.000 description 1
- 150000002602 lanthanoids Chemical class 0.000 description 1
- 229910052746 lanthanum Inorganic materials 0.000 description 1
- FZLIPJUXYLNCLC-UHFFFAOYSA-N lanthanum atom Chemical compound [La] FZLIPJUXYLNCLC-UHFFFAOYSA-N 0.000 description 1
- 229910052745 lead Inorganic materials 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- OHSVLFRHMCKCQY-UHFFFAOYSA-N lutetium atom Chemical compound [Lu] OHSVLFRHMCKCQY-UHFFFAOYSA-N 0.000 description 1
- 238000001000 micrograph Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- 238000005554 pickling Methods 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 238000001953 recrystallisation Methods 0.000 description 1
- 230000001172 regenerating effect Effects 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 229910052706 scandium Inorganic materials 0.000 description 1
- SIXSYDAISGFNSX-UHFFFAOYSA-N scandium atom Chemical compound [Sc] SIXSYDAISGFNSX-UHFFFAOYSA-N 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
- 150000003568 thioethers Chemical class 0.000 description 1
- 229910052718 tin Inorganic materials 0.000 description 1
- 229910052727 yttrium Inorganic materials 0.000 description 1
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 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
- C22C38/004—Very low carbon steels, i.e. having a carbon content of less than 0,01%
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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
- C22C38/34—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of silicon
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D22/00—Shaping without cutting, by stamping, spinning, or deep-drawing
- B21D22/02—Stamping using rigid devices or tools
- B21D22/022—Stamping using rigid devices or tools by heating the blank or stamping associated with heat treatment
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D53/00—Making other particular articles
- B21D53/88—Making other particular articles other parts for vehicles, e.g. cowlings, mudguards
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/18—Hardening; Quenching with or without subsequent tempering
- C21D1/19—Hardening; Quenching with or without subsequent tempering by interrupted quenching
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- 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
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- C21D6/00—Heat treatment of ferrous alloys
- C21D6/004—Heat treatment of ferrous alloys containing Cr and Ni
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- C—CHEMISTRY; METALLURGY
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- C21D6/00—Heat treatment of ferrous alloys
- C21D6/005—Heat treatment of ferrous alloys containing Mn
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- C—CHEMISTRY; METALLURGY
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- 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
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- C—CHEMISTRY; METALLURGY
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- C21D6/00—Heat treatment of ferrous alloys
- C21D6/008—Heat treatment of ferrous alloys containing Si
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- C21D6/00—Heat treatment of ferrous alloys
- C21D6/02—Hardening by precipitation
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- 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
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- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0205—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips of ferrous alloys
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- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0226—Hot rolling
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- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
- C21D8/0273—Final recrystallisation annealing
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- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
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- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
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- 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
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- 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
Definitions
- the present invention relates to a ferritic stainless steel sheet for an automobile brake disc rotor, an automobile brake disc rotor and a hot-stamped product for an automobile brake disc rotor, which have excellent heat resistance and formability, and specifically to a ferritic stainless steel sheet suitably used for an automobile brake disc rotor and the like that are required to have high-temperature strength.
- a disc brake is widely used as one of automobile brake systems.
- This disc brake reduces a speed of an automobile by pressing a disc-like structure connected to a tire, called a disc rotor, between brake pads to cause friction, thereby converting kinetic energy to thermal energy.
- a disc rotor As a material for this disc rotor, flake graphite cast iron (hereinafter referred to as cast iron) is used in light of thermal conductivity, a cost and the like.
- Cast iron to which an element improving corrosion resistance is not added, is inferior in corrosion resistance and thus gathers red rust upon being left.
- This red rust conventionally is not so noticeable due to a position of the disc that is lower than a line of sight and a shape of a wheel.
- aluminum is used for a material for the wheel and a spoke is made thinner in order to respond to a request for improvement in fuel efficiency, the rust of the disc cannot be left ignored, thereby generating a need for improving corrosion resistance.
- a material having excellent corrosion resistance is exemplified by stainless steel.
- a martensitic material i.e., SUS410
- SUS410 a martensitic material
- the disc rotor for the two-wheeled vehicle is exposed to be easily noticeable and thus corrosion resistance is considered as important.
- stainless steel is inferior in thermal conductivity to cast iron.
- a brake system being exposed to have excellent cooling performance allows use of even stainless steel with no problem.
- the disc rotor is less likely to be cooled and has low thermal conductivity, whereby stainless steel has not been applied thereto.
- the disc rotor for the two-wheeled vehicle is in a form of a ring-shaped disc, and is produced, without requiring large machining, by punching plate-shaped stainless steel.
- the current disc rotor for the automobile is in a form of a disc whose center is squeezed, called a hat shape, and is produced by casting. Machining stainless steel to be formed into this shape requires deep drawing.
- stainless steel used for the two-wheeled vehicle is martensitic stainless steel, which has extremely high hardness and entails machining difficulty.
- hot stamping involving pressing at a high temperature recently has been increasingly used. The hot stamping also allows forming stainless steel into a hat shape with a high precision.
- the disc rotor in order to meet the request for improvement in fuel efficiency, the disc rotor needs to be made thinner and lighter.
- cast iron is low in strength and the disc rotor is typically produced by casting, there is a limit to thinning thereof.
- a temperature to be reached at braking of the automobile is said to be near 700 degrees C. at a maximum, it may be difficult to apply martensitic stainless steel having a heat resistance temperature of near 500 degrees C.
- a temperature to be reached under driving conditions of frequent braking on a mountain road or the like may be 300 degrees C.
- Patent Literature 1 relates to a stainless steel disc rotor for the automobile but mainly focuses on formability not on high-temperature strength. Furthermore, Patent Literature 2 improves strength by martensitic phases including highly saturated solid solution C and N but does not describe strength near 700 degrees C. Both Patent Literatures 1 and 2 adopt a martensitic structure but are not found to reliably provide heat resistance near 700 degrees C.
- the invention relates to a ferritic stainless steel sheet for an automobile brake disc rotor having excellent heat resistance and formability.
- a target component which is an intended use of the invention whose problem is to be solved, is a braking system component for an automobile, particularly a disc rotor.
- the disc rotor for the automobile having a hat shape requires formability.
- a temperature to be reached is usually about 100 degrees C. in driving on a city road and about 300 degrees C. in driving on a mountain road while being near 700 degrees C. at a maximum
- thinning thereof requires strength in an intermediate to high temperature range.
- cast iron is molded by casting, thinning of the disc rotor deteriorates metal flow, which may result in a failure of molding.
- cast iron is low in strength, the thinning of the disc rotor cannot reliably secure sufficient strength as a disc rotor.
- Ferritic stainless steel can be formed into a hat shape through hot stamping with a high precision. However, stainless steel having low strength cannot be thinned.
- Martensitic stainless steel is excellent in formability in hot stamping but has a heat resistance temperature of about 500 degrees C., thus failing to achieve both formability and heat resistance.
- the invention provides a ferritic stainless steel sheet for an automobile brake disc rotor, an automobile brake disc rotor and a hot-stamped product for an automobile brake disc rotor, which have excellent heat resistance and formability.
- the precipitates may be formed in the steel in a temperature range in which the component according to the invention is formed through hot stamping.
- the finely dispersed precipitates can improve strength of a material.
- presence of the precipitates before the forming results in excessively high strength to reduce elongation of the steel, making it likely for cracking to occur during the forming. Accordingly, it has been believed that finely forming the precipitates during the hot stamping can reliably secure formability and strength after the hot stamping.
- a crystal grain size is increased during heating in the hot stamping to form the precipitates during the hot stamping.
- Setting the finishing temperature at more than 950 degrees C. effectively increases the crystal grain size to improve strength also in an intermediate temperature range. Since the precipitates are finely formed in crystal grains of the steel, excellent high-temperature strength during use as a disc rotor can be attained. The precipitates formed at grain boundaries are likely to grow and coarsen. In this regard, it has been found that the precipitates are formed mainly in the crystal grains by appropriately controlling the crystal grain size during heating in the hot stamping.
- the precipitates in the crystal grains are less likely to grow than the precipitates at the grain boundaries and thus are less likely to coarsen during use.
- the precipitates are finely formed in the grains during the hot stamping, thereby effectively exhibiting precipitation strengthening. Accordingly, a heat-resistant ferritic stainless steel sheet applicable to a disc rotor has been successfully provided.
- a ferritic stainless steel sheet for an automobile brake disc rotor includes: 0.001 to 0.05 mass % of C; 0.001 to 0.05 mass % of N; 0.3 to 4.0 mass % of Si; 0.01 to 2.0 mass % of Mn; 0.01 to 0.05 mass % of P; 0.0001 to 0.02 mass % of S; 10 to 20 mass % of Cr; one or both of 0.001 to 0.5 mass % of Ti and 0.01 to 0.8 mass % of Nb; and a balance consisting of Fe and impurities,
- a heat treatment (hereinafter referred to as a “hot stamping pseudo heat treatment”) in which the steel sheet is heated to 1000 degrees C. and subsequently cooled by being retained in a range from 890 to 700 degrees C. for one to ten minutes, a crystal grain size is in a range from 100 to 200 ⁇ m, and precipitates each having a grain size of 500 nm or less are at a density of 0.01 to 20 pieces per square micrometer, and the ferritic stainless steel sheet is a ferritic stainless steel for hot stamping.
- a heat treatment hereinafter referred to as a “hot stamping pseudo heat treatment”
- the steel sheet is heated to 1000 degrees C. and subsequently cooled by being retained in a range from 890 to 700 degrees C. for one to ten minutes
- a crystal grain size is in a range from 100 to 200 ⁇ m
- precipitates each having a grain size of 500 nm or less are at a density of 0.01 to 20 pieces per square micrometer
- the ferritic stainless steel sheet is
- a ferritic stainless steel sheet for an automobile brake disc rotor includes: 0.001 to 0.05 mass % of C; 0.001 to 0.05 mass % of N; 0.3 to 4.0 mass % of Si; 0.01 to 2.0 mass % of Mn; 0.01 to 0.05 mass % of P; 0.0001 to 0.02 mass % of S; 10 to 20 mass % of Cr; one or both of 0.001 to 0.5 mass % of Ti and 0.01 to 0.8 mass % of Nb; and a balance consisting of Fe and impurities,
- the ferritic stainless steel sheet in which a crystal grain size is in a range from 100 to 200 ⁇ m and precipitates each having a grain size of 500 nm or less are present at a density of 0.01 to 20 pieces per square micrometer is in a form of a hot-stamped product.
- a ferritic stainless steel sheet for an automobile brake disc rotor includes: 0.001 to 0.05 mass % of C; 0.001 to 0.05 mass % of N; 0.3 to 4.0 mass % of Si; 0.01 to 2.0 mass % of Mn; 0.01 to 0.05 mass % of P; 0.0001 to 0.02 mass % of S; 10 to 20 mass % of Cr; one or both of 0.001 to 0.5 mass % of Ti and 0.01 to 0.8 mass % of Nb; and a balance consisting of Fe and impurities.
- the ferritic stainless steel sheet is a ferritic stainless steel sheet for hot stamping.
- the ferritic stainless steel sheet for an automobile brake disc rotor with the above arrangement further includes, in place of a part of Fe, at least one of 0.0001 to 0.0030 mass % of B, 0.001 to 4.0 mass % of Al, 0.01 to 3.0 mass % of Cu, 0.01 to 3.0 mass % of Mo, 0.001 to 2.0 mass % of W, 0.001 to 1.0 mass % of V, 0.01 to 0.5 mass % of Sn, 0.01 to 1.0 mass % of Ni, 0.0001 to 0.01 mass % of Mg, 0.005 to 0.5 mass % of Sb, 0.001 to 0.3 mass % of Zr, 0.001 to 0.3 mass % of Ta, 0.001 to 0.3 mass % of Hf, 0.001 to 0.3 mass % of Co, 0.0001 to 0.01 mass
- a ferritic stainless steel sheet improves in heat resistance and formability to provide a material suitable for an automobile brake disc rotor, thereby attaining significant effects such as reducing a weight and improving an appearance thereof.
- the steel sheet is heated to about 1000 degrees C. for the hot stamping.
- the steel sheet before the hot stamping is required to have sufficient ductility for the hot stamping, which is performed at about 1000 degrees C.
- an automobile brake disc rotor after the hot stamping is required to achieve sufficient high-temperature strength.
- a temperature range for forming through the hot stamping may allow formation of precipitates.
- the precipitates being finely dispersed in the steel can improve strength of a material.
- presence of the precipitates before the forming results in excessively high strength to reduce elongation, making it likely for cracking to occur during the forming through the hot stamping. Accordingly, the invention secures hot stamping formability and strength after the hot stamping by finely forming the precipitates during the hot stamping.
- a crystal grain size of the steel during the hot stamping is given an attention.
- the crystal grain size is small, a ratio of grain boundaries in the steel is high, thus resulting in formation of more precipitates at the grain boundaries during the hot stamping.
- the precipitates formed at the grain boundaries are likely to grow and coarsen, and thus fine precipitates are not likely to be obtained.
- the precipitates are formed mainly in the grains by growing and appropriately controlling the crystal grain size during heating in the hot stamping.
- the precipitates in the grains are less likely to grow than the precipitates at the grain boundaries and thus are less likely to coarsen during use.
- the precipitates are finely formed in the grains during the hot stamping to effectively exhibit precipitation strengthening after the hot stamping, thereby securing strength after the forming.
- finely forming the precipitates in the grains is crucial in terms of high-temperature strength after the hot stamping; and for this purpose, growing the crystal grain size during the heating in the hot stamping to a certain extent is required.
- refinement of the precipitates can be achieved by having the crystal grain size after the hot stamping in a range from 100 to 200 ⁇ m.
- the crystal grain size during the hot stamping is the same as the crystal grain size after the hot stamping. With a crystal grain size in the above range, the precipitates are finely formed in the grains and are not likely to grow, from which it is presumed that there is a corresponding relationship therebetween.
- a metal structure in the invention has been defined by the crystal grain size after the hot stamping.
- the precipitates are finely formed during the hot stamping and are not likely to grow, thereby effectively exhibiting precipitation strengthening.
- a crystal grain size after the hot stamping being 100 ⁇ m or more, the precipitates are finely formed and thus sufficient proof strength up to near 700 degrees C. has been obtained.
- a crystal grain size after the hot stamping being 130 ⁇ m or more, sufficient proof strength has been obtained also in an intermediate temperature range (i.e., near 300 degrees C.).
- the crystal grains in the steel grow by the heating in the hot stamping to increase the crystal grain size.
- the crystal grain size after the hot stamping exceeding 200 ⁇ m means that the crystal grain size of the steel sheet before the hot stamping is also large, and consequently, toughness of the steel sheet significantly reduces. Accordingly, an upper limit of the crystal grain size after the hot stamping has been set at 200 ⁇ m.
- the precipitates each having a grain size of 500 nm or less are defined to be present at a density of 0.01 to 20 pieces per square micrometer in the steel after the hot stamping.
- the precipitates each having a grain size of 500 nm or less being present at a density of 0.01 to 20 pieces per square micrometer, sufficient proof strength up to near 700 degrees C. is obtained.
- a grain size exceeding 500 nm precipitation strengthening is not likely to function.
- a density of the precipitates being less than 0.01 pieces per square micrometer precipitation strengthening is also not likely to function due to a small precipitation amount.
- a density exceeding 20 pieces per square micrometer excessively increases strength, making it likely for cracking to occur.
- it is preferable that the precipitates being in the grains and each having a grain size of 500 nm or less are present at a density of 0.01 to 20 pieces per square micrometer.
- the crystal grain size and the density of the precipitates in the steel can be evaluated.
- the product to be evaluated is a steel sheet before the hot stamping
- the crystal grain size and the density of the precipitates in the steel may be evaluated after subjecting the steel sheet to a hot stamping pseudo heat treatment.
- the hot stamping pseudo heat treatment may be a heat treatment including: heating the steel sheet to 1000 degrees C.; and subsequently cooling by retaining the steel sheet in a range from 890 to 700 degrees C. for one to ten minutes (e.g., two minutes).
- the C content is preferably as small as possible and thus is set at 0.05% or less.
- the C content is preferably 0.020% or less, more preferably 0.0015% or less.
- the C content is preferably 0.001% or more.
- the N content is preferably as small as possible and thus is set at 0.05% or less.
- the N content is preferably 0.020% or less, more preferably 0.015% or less.
- the N content is preferably 0.001% or more.
- Si is an element useful as a deoxidizer and is also an element improving high-temperature strength, oxidation resistance and high-temperature salt-damage resistance.
- the high-temperature strength, oxidation resistance and high-temperature salt-damage resistance improve in line with an increase in the Si content.
- controlling of precipitation is crucial, and thus this effect is attained by finely forming precipitates in a large amount.
- Si has an effect of finely forming aging precipitates and the effect is stably exhibited at 0.3% or more of Si.
- an upper limit of the Si content is set at 4.0%.
- the Si content is preferably in a range from 0.3% to 3.5%.
- the Si content is preferably 3.0% or less.
- Mn is an element added as a deoxidizer and contributes to increasing high-temperature strength in an intermediate temperature range.
- addition of Mn at more than 2.0% causes MnS (which does not contribute to strengthening) to precipitate in a large amount to reduce the high-temperature strength after a pseudo heat treatment; and precipitates Mn oxides on a surface layer at a high temperature to make it likely to cause unfavorable adhesion of scales and abnormal oxidation.
- an upper limit of the Mn content is set at 2.0%.
- the Mn content is preferably in a range from 0.01% to 1.5%, more preferably 1.0% or less.
- the P content in the invention is set at 0.01% or more.
- the P content is more preferably 0.02% or more.
- the P content of more than 0.05% not only causes more significant hardening but also deteriorates corrosion resistance, toughness and picklability. Accordingly, an upper limit of the P content is set at 0.05%.
- the P content is more preferably 0.04% or less.
- S is an element deteriorating corrosion resistance and oxidation resistance.
- a lower limit of the S content is set at 0.0001%.
- the S content is preferably 0.0010% or more.
- excessive addition of S allows S to be bonded to Ti and C to reduce an amount of solid solution Ti and coarsen precipitates, thereby reducing toughness and high-temperature strength of a steel sheet.
- an upper limit of the S content is set at 0.02%.
- the S content is preferably 0.0090% or less.
- Cr is an essential element for ensuring oxidation resistance and corrosion resistance in the invention. Less than 10% of Cr cannot secure, particularly, oxidation resistance, to further reduce proof strength at 700 degrees C. after hot stamping and coarsen a crystal grain size. Meanwhile, since more than 20% of Cr causes a reduction in workability and deterioration of toughness and makes the number of precipitates after hot stamping excessively large, the Cr content is set in a range from 10 to 20%. In terms of productivity and scale peelability, the Cr content is preferably in a range from 12% to 18%, more preferably 15% or less.
- One or both of 0.001 to 0.5% of Ti and 0.01 to 0.8% of Nb are contained.
- Ti is an element bonded to C, N and S to improve corrosion resistance, intergranular corrosion resistance, normal-temperature ductility and deep drawability. Accordingly, Ti is added as required. Combined addition where Ti is added in an appropriate amount with Nb and Mo increases an amount of solid solution of Nb and Mo and improves high-temperature strength in hot rolling and annealing, thereby improving thermal fatigue properties. This effect is exhibited at 0.001% or more of Ti and thus a lower limit of the Ti content is set at 0.001%.
- addition of more than 0.5% of Ti not only increases an amount of solid solution Ti to reduce ductility of a steel sheet at a normal temperature and a high temperature but also makes the number of precipitates after hot stamping excessive and further forms coarse Ti precipitates to be an initiation point of cracking in hole expansion, thereby deteriorating press workability. Since oxidation resistance also deteriorates, an added amount of Ti is set at 0.5% or less. In terms of occurrence of surface flaws and toughness, the Ti content is preferably in a range from 0.05% to 0.2%.
- Nb is an element effective in improving high-temperature strength through solid solution strengthening and precipitation strengthening by fine precipitates. Nb also has a function of fixing C and N as carbonitrides to contribute to growth of recrystallization texture affecting corrosion resistance and an r value of a product sheet. These effects are exhibited at 0.01% or more of Nb and thus a lower limit of the Nb content is set at 0.01%. Meanwhile, since addition of more than 0.8% of Nb reduces high-temperature ductility of the steel sheet and makes the number of precipitates after hot stamping excessive to further significantly harden the steel sheet and deteriorate productivity, an upper limit of the Nb content is set at 0.8%. In terms of a material cost and toughness, the Nb content is preferably in a range from 0.3% to 0.6%.
- a balance consists of Fe and impurities as components in the steel.
- the invention may further contain the following components in place of a part of Fe as required.
- B is an element improving secondary workability, high-temperature strength and thermal fatigue properties of a product in pressing.
- B causes fine precipitation of Laves phases and the like and exhibits long-term stability of this precipitation strengthening, thereby contributing to inhibiting a reduction in strength and improving a thermal fatigue life. This effect is exhibited at 0.0001% or more of B.
- the B content is set at 0.0030% or less. In terms of corrosion resistance and a production cost, the B content is preferably 0.0010% or less, more preferably 0.0005% or less.
- Al is an element to be added as a deoxidizing element and improve oxidation resistance. Al is also useful for improving high-temperature strength as a solid solution strengthening element. This effect is stably exhibited at 0.001% or more of Al. Meanwhile, since excessive addition of Al hardens steel to significantly reduce uniform elongation and toughness, an upper limit of the Al content is set at 4.0%. In terms of occurrence of surface flaws, weldability and productivity, the Al content is preferably in a range from 0.01% to 2.2%.
- Cu is an element effective in improving corrosion resistance. This effect is stably exhibited at 0.01% or more of Cu. Although Cu also improves high-temperature strength through precipitation strengthening by precipitation of ⁇ -Cu, excessive addition of Cu reduces hot workability. Accordingly, an upper limit of the Cu content is set at 3.0%. In terms of thermal fatigue properties, productivity and weldability, the Cu content is preferably 1.6% or less.
- Mo is an element effective in solid solution strengthening at a high temperature and improves corrosion resistance and high-temperature salt-damage resistance. Accordingly, Mo is added at 0.01% or more as required. Since addition of 3.0% or more of Mo significantly deteriorates normal-temperature ductility and oxidation resistance, the Mo content is set at 3.0% or less. In terms of thermal fatigue properties and productivity, the Mo content is preferably in a range from 0.3% to 0.9%.
- W is an element effective in solid solution strengthening at a high temperature and forms Laves phases (Fe 2 W) to exhibit an effect of precipitation strengthening.
- Laves phases Fe 2 W
- Nb, Mo, W Laves phases of Fe 2
- W inhibits coarsening of the Laves phases to improve precipitation strengthening capability. This effect is exhibited by addition of 0.001% or more of W.
- an upper limit of the W content is set at 2.0%. In terms of productivity, low-temperature toughness and oxidation resistance, an added amount of W is preferably 1.5% or less.
- V is an element improving corrosion resistance and thus is added as required. This effect is stably exhibited by addition of 0.001% or more of V. Meanwhile, since addition of more than 1% of V coarsens precipitates to reduce high-temperature strength and deteriorate oxidation resistance, an upper limit of the V content is set at 1%. In terms of a production cost and productivity, the V content is preferably in a range from 0.08% to 0.5%.
- Sn is an element improving corrosion resistance, improves high-temperature strength in an intermediate temperature range, and thus is added as required. These effects are exhibited at 0.01% or more of Sn. Meanwhile, since addition of more than 0.5% of Sn significantly reduces productivity and toughness, the Sn content is set at 0.5% or less. In terms of oxidation resistance and a production cost, the Sn content is preferably 0.1% or more.
- Ni is an element improving acid resistance, toughness and high-temperature strength and thus is added as required. These effects are exhibited at 0.01% or more of Ni. Meanwhile, since addition of more than 1.0% of Ni increases a cost, the Ni content is set at 1.0% or less. In terms of productivity, the Ni content is preferably in a range from 0.08% to 0.5%.
- Mg may be added as a deoxidizing element and is an element refining a slab structure to contribute to improving formability.
- Mg oxides become precipitation sites of carbonitrides such as Ti(C, N) and Nb(C, N) and have an effect of allowing finely dispersed precipitation thereof. This effect is exhibited at 0.0001% or more of Mg, thereby contributing to improving toughness.
- an upper limit of the Mg content is set at 0.01%.
- the Mg content is preferably in a range from 0.0003% to 0.0010%.
- Sb contributes to improving corrosion resistance and high-temperature strength, and is added at 0.005% or more as required. Since addition of more than 0.5% of Sb may excessively cause slab cracking and a reduction in ductility in producing a steel sheet, an upper limit of the Sb content is set at 0.5%. In terms of a refining cost and productivity, the Sb content is preferably in a range from 0.01% to 0.3%.
- Zr is a carbonitride forming element and an element improving corrosion resistance and deep drawability, and thus is added as required. These effects are exhibited at 0.001% or more of Zr. Meanwhile, since addition of more than 0.3% of Zr significantly deteriorates productivity, the Zr content is set at 0.3% or less. In terms of a cost and surface grade, the Zr content is preferably in a range from 0.1% to 0.2%.
- Zr, Ta and Hf are bonded to C and N to contribute to improving toughness and thus are added at 0.001% or more as required.
- an upper limit of each of the Zr, Ta and Hf contents is set at 0.3%.
- the Zr, Ta and Hf contents are each preferably in a range from 0.01% to 0.08%.
- Co contributes to improving high-temperature strength and thus is added at 0.001% or more as required. Since addition of more than 0.3% of Co deteriorates toughness, an upper limit of the Co content is set at 0.3%. In terms of a refining cost and productivity, the Co content is preferably in a range from 0.01% to 0.1%.
- Ca may be added for desulfurization, of which effect is exhibited at 0.0001% or more of Ca.
- an upper limit of the Ca content is set at 0.01%.
- the Ca content is preferably in a range from 0.0003% to 0.0020%.
- REM may be added as required in order to improve toughness and oxidation resistance through refinement of various precipitates, of which effect is exhibited at 0.001% or more of REM.
- an upper limit of the REM content is set at 0.2%.
- the REM content is preferably 0.05% or less.
- REM rare-earth elements
- Sc scandium
- Y yttrium
- lanthanoid lanthanoid
- Ga may be added at 0.3% or less in order to improve corrosion resistance and inhibit hydrogen embrittlement.
- a lower limit of the Ga content is preferably 0.0002%.
- the Ga content is preferably 0.0020% or less.
- the production method of a steel sheet according to the invention includes processes of steelmaking, hot rolling, annealing and pickling.
- steelmaking steel containing the above essential components and components added as required is suitably melted in a converter furnace and subsequently subjected to secondary refining.
- the molten steel is formed into a slab according to a known casting process (continuous casting).
- the slab is heated to a predetermined temperature and hot-rolled to have a predetermined thickness through continuous rolling.
- the hot rolling is performed by rolling the slab using a hot rolling mill including a plurality of stands, which is followed by winding.
- the annealing process after the hot rolling may be omitted.
- a finishing temperature after the hot rolling is preferably in a range from 900 to 1100 degrees C.
- a finishing temperature of less than 900 degrees C. does not sufficiently grow the crystal grain size of the steel sheet, consequently failing to grow the crystal grain size after the hot stamping to 100 ⁇ m or more.
- a finishing temperature of more than 1100 degrees C. excessively grows the crystal grain size of the steel sheet to make the crystal grain size after the hot stamping more than 200 ⁇ m.
- the finishing temperature after the hot rolling is more preferably more than 950 degrees C. Setting the finishing temperature at more than 950 degrees C. allows the crystal grain size to grow to be 130 ⁇ m or more, thereby exhibiting an effect of improving strength in an intermediate temperature range.
- the winding temperature is preferably 650 degrees C. or less.
- the hot stamping in which the steel sheet is heated to a predetermined temperature, formed into a hat shape at a high temperature and subsequently cooled is used.
- a heating temperature is set in a range from 900 to 1000 degrees C.
- the cooling is performed subsequent to the forming.
- the cooling is performed by retaining the steel sheet in a range from 890 to 700 degrees C. for one to ten minutes. Since a retention time of less than one minute does not cause sufficient precipitation to make an amount of precipitation strengthening small, a lower limit of the retention time is set at one minute.
- the excessively long retention time grows and coarsens finely formed precipitates to reduce the amount of precipitation strengthening. Since the excessively long retention time also significantly reduces productivity, an upper limit of the retention time is set at ten minutes. In terms of stability of the precipitates, the retention time is preferably in a range from 1.5 minutes to five minutes.
- a “ferritic stainless steel sheet for an automobile brake disc rotor in a form of a hot-stamped product” in the invention refers to a steel sheet obtained after hot stamping.
- the ferritic stainless steel sheet refers to a hot-stamped product for an automobile brake disc rotor for which a stainless steel sheet is used.
- the hot-stamped product for an automobile brake disc rotor made of a stainless steel sheet refers to a hot-stamped product for an automobile brake disc rotor obtained by subjecting a steel sheet to hot stamping.
- the automobile brake disc rotor made of a stainless steel sheet refers to an automobile brake disc rotor obtained by subjecting a stainless steel sheet to hot stamping and further machining.
- the thus obtained hot-rolled steel sheet (other than B15) was subjected to a hot stamping pseudo heat treatment (hereinafter simply referred to as a “pseudo heat treatment”) by: heating the steel sheet to 1000 degrees C.; then retaining the steel sheet in a range from 890 to 700 degrees C. for two minutes; and subsequently water-cooling the steel sheet.
- a hot stamping pseudo heat treatment hereinafter simply referred to as a “pseudo heat treatment”
- “cracking” was indicated in a column of “Quality after Pseudo Heat Treatment/Notes” in Table 4.
- the material that was subjected to the hot stamping pseudo heat treatment was measured for a crystal grain size at a t/4 portion (according to JIS G 0551, and numerical values were rounded off to the closest whole number).
- an image magnification at 50 times and the number of imaging fields at five
- an average crystal grain size of the five imaging fields was calculated.
- five fields of the same material that was subjected to the pseudo heat treatment were observed under bright field microscopy at the image magnification of 12500 times using a 200 kV field emission transmission electron microscope (EM-2100F) produced by JEOL Ltd., thereby evaluating precipitates.
- An equivalent circle diameter of the precipitates observed in the bright field microscope image was measured to obtain the grain size of the precipitates.
- the precipitates each having a grain size of 500 nm or less were used to calculate an average density of the precipitates at the five fields.
- a high-temperature tensile test piece was taken from the material that was subjected to the pseudo heat treatment such that a rolling direction thereof was a tensile direction.
- the test piece was subjected to a tensile test at 300 degrees C. and 700 degrees C. to measure 0.2% proof strength (according to JIS G 0567, and numerical values were rounded off to the closest whole number).
- 0.2% proof strength at 300 degrees C. of 150 MPa or more and 0.2% proof strength at 700 degrees C. of 80 MPa or more the material is applicable to a general disc rotor and thinning thereof is achievable. Accordingly, steel having 0.2% proof strength at 300 degrees C. of 150 MPa or more and 0.2% proof strength at 700 degrees C.
- a high-temperature tensile test piece was taken from the hot-rolled steel sheet such that a rolling direction thereof was a tensile direction.
- the test piece was subjected to a tensile test at 1000 degrees C. to measure fracture elongation (according to JIS G 0567, and numerical values were rounded off to the closest whole number).
- the steel sheet can be machined into a hat shape. Accordingly, steel having fracture elongation at 1000 degrees C. of 50% or more was evaluated to pass and was indicated by a mark “A” in Tables 3 and 4.
- steel having fracture elongation at 1000 degrees C. of 65% or more was evaluated to be particularly superior and was indicated by a mark “S”. Steel other than the above was evaluated to fail and was indicated by a mark “X”.
- a Charpy test piece (C direction notch) was prepared from the hot-rolled steel sheet and subjected to a Charpy impact test at a normal temperature.
- an average impact value of three tests was 10 J/cm 2 or less, “unfavorable toughness” was indicated in a column of “Notes” for steel sheet quality.
- Examples have superior 0.2% proof strength at 700 degrees C. after the hot stamping pseudo heat treatment to that of Comparatives. It has been found that the Examples, of which finishing temperature of the hot-rolled steel sheet is more than 950 degrees C., have a crystal grain size of 130 ⁇ m or more and all have particularly superior proof strength at 300 degrees C. that is evaluated to be “S”. In a case where even one of 0.2% proof strength at 300 degrees C. and 700 degrees C. after the pseudo heat treatment and fracture elongation of the hot-rolled steel sheet at 1000 degrees C. was evaluated to fail and in a case where toughness of the hot-rolled steel sheet was unfavorable, application thereof to a disc rotor was determined as unsuitable. Accordingly, it has been found that the steel defined in the invention is excellent in heat resistance and formability.
- Comparatives B1 and B2 which respectively had C and N concentrations exceeding the upper limit thereof, had unfavorable fracture elongation at 1000 degrees C. of the steel sheets.
- Comparative B3 whose Si concentration was below the lower limit thereof, had an insufficient number of precipitates after the pseudo heat treatment, thereby being low in proof strength at 300 degrees C. and 700 degrees C. Comparative B4, whose Si concentration exceeded the upper limit thereof, had unfavorable elongation at 1000 degrees C. of the steel sheet, an excessively small crystal grain size and an excessive number of precipitates after the pseudo heat treatment, thereby causing cracking.
- Comparative B5 whose Mn concentration exceeded the upper limit thereof, had insufficient proof strength at 300 degrees C. and 700 degrees C.
- Comparatives B6 and B7 which respectively had P and S concentrations exceeding the upper limit thereof, had unfavorable toughness of the steel sheets.
- Comparative B8 whose Cr concentration was below the lower limit thereof, had reduced high-temperature strength, resulting in unfavorable proof strength at 300 degrees C. and 700 degrees C. after the pseudo heat treatment. As is evident from an excessively large crystal grain size after the pseudo heat treatment, Comparative B8 also had an excessively large crystal grain size of the steel sheet, thereby causing unfavorable toughness of the steel sheet.
- Comparatives B9, B10 and B11 which respectively had Cr, Ti and Nb concentrations exceeding the upper limit thereof, had unfavorable fracture elongation at 1000 degrees C. of the steel sheets and an excessive number of precipitates during the pseudo heat treatment, thereby causing cracking.
- Comparative B12 had an excessively large crystal grain size of the steel sheet, thereby causing unfavorable toughness of the steel sheet.
- Comparative B13 whose finishing temperature of hot rolling was below the lower limit thereof, had an excessively small crystal grain size after the pseudo heat treatment and an excessively small number of precipitates, consequently obtaining unfavorable proof strength at 300 degrees C. and 700 degrees C.
- Comparative B14 whose winding temperature of the hot rolling exceeded the upper limit thereof, had unfavorable toughness of the steel sheet.
- B15 which was indicated by “Untreated” in the left column in Table 2, was not subjected to the hot stamping pseudo heat treatment but evaluated for a crystal grain size, the number of precipitates and proof strength at 300 degrees C. and 700 degrees C. As a result of failing to progress precipitation and obtaining an excessively small number of precipitates, B15 had unfavorable proof strength at 300 degrees C. and 700 degrees C.
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US17/598,613 Pending US20220177993A1 (en) | 2019-03-28 | 2020-03-12 | Ferritic stainless steel sheet for automobile brake disk rotors, automobile brake disk rotor, and hot-stamped article for automobile brake disk rotors |
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CN116103572B (zh) * | 2023-04-11 | 2023-07-07 | 山西建龙实业有限公司 | 一种双金属制动鼓用钢及其制备热轧钢带的方法 |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6568512B1 (en) * | 2002-05-16 | 2003-05-27 | International Truck Intellectual Property Company, Llc | Corrosion resistant cast-in insert exciter ring |
JP2014145097A (ja) * | 2013-01-28 | 2014-08-14 | Nippon Steel & Sumikin Stainless Steel Corp | 高温プレス成形に適する自動車排気系部材用のフェライト系ステンレス鋼板およびフェライト系ステンレス鋼成形部品の製造方法 |
US20190226045A1 (en) * | 2016-10-17 | 2019-07-25 | Jfe Steel Corporation | Hot-rolled and annealed ferritic stainless steel sheet and method for manufacturing the same |
Family Cites Families (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS51134756A (en) | 1975-05-16 | 1976-11-22 | Furukawa Electric Co Ltd | Method of producing improved polyoxadiazole resin film |
JPS639819Y2 (ja) | 1980-02-01 | 1988-03-23 | ||
JP3411767B2 (ja) * | 1996-01-30 | 2003-06-03 | Jfeスチール株式会社 | 高強度高延性フェライト単相Cr含有鋼板およびその製造方法 |
JP3900169B2 (ja) * | 2003-04-28 | 2007-04-04 | Jfeスチール株式会社 | ディスクブレーキ用マルテンサイト系ステンレス鋼 |
JP4308622B2 (ja) * | 2003-10-21 | 2009-08-05 | Jfeスチール株式会社 | 耐焼戻し軟化性に優れたブレーキディスクおよびその製造方法 |
JP4182865B2 (ja) * | 2003-11-11 | 2008-11-19 | Jfeスチール株式会社 | 耐焼戻し軟化性に優れるディスクブレーキ用ステンレス鋼板 |
JP4843969B2 (ja) * | 2004-03-22 | 2011-12-21 | Jfeスチール株式会社 | 耐熱性と耐食性に優れるディスクブレーキ用ステンレス鋼板 |
JP4517850B2 (ja) * | 2004-12-15 | 2010-08-04 | Jfeスチール株式会社 | 耐熱応力割れ性に優れるディスクブレーキ用ステンレス鋼板 |
JP4569360B2 (ja) | 2005-04-06 | 2010-10-27 | Jfeスチール株式会社 | 焼戻し軟化抵抗と靭性に優れるブレーキディスク |
JP5200332B2 (ja) | 2005-04-21 | 2013-06-05 | Jfeスチール株式会社 | 焼戻し軟化抵抗の大きいブレーキディスク |
EP2042615A4 (en) * | 2006-10-05 | 2011-08-03 | Jfe Steel Corp | BRAKE DISCS WITH EXCELLENT RESISTANCE TO ANNEALING AND EXCELLENT TENACITY |
CN100535168C (zh) * | 2007-02-16 | 2009-09-02 | 宝山钢铁股份有限公司 | 一种热轧铁素体不锈钢带钢的生产方法 |
JP2011225948A (ja) * | 2010-04-21 | 2011-11-10 | Jfe Steel Corp | ブレーキディスク用Cr含有熱延鋼板とブレーキディスク |
JP5737952B2 (ja) * | 2011-01-05 | 2015-06-17 | 日新製鋼株式会社 | Nb含有フェライト系ステンレス鋼熱延コイルおよび製造法 |
CN105189801A (zh) * | 2013-03-19 | 2015-12-23 | 杰富意钢铁株式会社 | 不锈钢板 |
EP2980251B1 (en) * | 2013-03-27 | 2017-12-13 | Nippon Steel & Sumikin Stainless Steel Corporation | Hot-rolled ferritic stainless-steel plate, process for producing same, and steel strip |
JP5908936B2 (ja) * | 2014-03-26 | 2016-04-26 | 新日鐵住金ステンレス株式会社 | フランジ用フェライト系ステンレス鋼板とその製造方法およびフランジ部品 |
CN104294160A (zh) * | 2014-09-09 | 2015-01-21 | 宝钢不锈钢有限公司 | 一种高硬度高韧性低碳马氏体不锈钢及其制造方法 |
JP2016117925A (ja) | 2014-12-19 | 2016-06-30 | 日新製鋼株式会社 | ステンレス製4輪用ディスクブレーキロータおよびその製造方法 |
JP6550325B2 (ja) * | 2015-11-27 | 2019-07-24 | 日鉄ステンレス株式会社 | フランジ用フェライト系ステンレス鋼熱延鋼板およびその製造方法 |
KR20170075857A (ko) * | 2015-12-23 | 2017-07-04 | 주식회사 포스코 | 저경도 마르텐사이트계 스테인레스강 및 그 제조방법 |
JP6786418B2 (ja) * | 2016-03-17 | 2020-11-18 | 日鉄ステンレス株式会社 | ブレーキディスク用マルテンサイト系ステンレス鋼、およびブレーキディスク |
JP6537659B1 (ja) * | 2018-03-28 | 2019-07-03 | 日鉄ステンレス株式会社 | マルテンサイト系ステンレス熱延鋼板、当該鋼板を用いたディスクブレーキロータの製造方法 |
JP6615255B2 (ja) * | 2018-03-28 | 2019-12-04 | 日鉄ステンレス株式会社 | 自動車用ディスクブレーキロータ |
JP6615256B2 (ja) * | 2018-03-30 | 2019-12-04 | 日鉄ステンレス株式会社 | ステンレス鋼板および制動系部品 |
-
2020
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Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6568512B1 (en) * | 2002-05-16 | 2003-05-27 | International Truck Intellectual Property Company, Llc | Corrosion resistant cast-in insert exciter ring |
JP2014145097A (ja) * | 2013-01-28 | 2014-08-14 | Nippon Steel & Sumikin Stainless Steel Corp | 高温プレス成形に適する自動車排気系部材用のフェライト系ステンレス鋼板およびフェライト系ステンレス鋼成形部品の製造方法 |
US20190226045A1 (en) * | 2016-10-17 | 2019-07-25 | Jfe Steel Corporation | Hot-rolled and annealed ferritic stainless steel sheet and method for manufacturing the same |
Non-Patent Citations (1)
Title |
---|
Machine translation of JP 2014-145097A. (Year: 2014) * |
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CA3133206A1 (en) | 2020-10-01 |
EP3950969A4 (en) | 2023-04-19 |
CN113661261A (zh) | 2021-11-16 |
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JPWO2020195915A1 (ja) | 2021-12-23 |
CA3133206C (en) | 2023-01-24 |
EP3950969A1 (en) | 2022-02-09 |
CN113661261B (zh) | 2023-09-19 |
WO2020195915A1 (ja) | 2020-10-01 |
JP7179966B2 (ja) | 2022-11-29 |
KR20210129140A (ko) | 2021-10-27 |
KR102569352B1 (ko) | 2023-08-22 |
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