EP1228253A1 - Composition d'acier, procede de fabrication et pieces formees dans ces compositions, en particulier soupapes - Google Patents
Composition d'acier, procede de fabrication et pieces formees dans ces compositions, en particulier soupapesInfo
- Publication number
- EP1228253A1 EP1228253A1 EP01931816A EP01931816A EP1228253A1 EP 1228253 A1 EP1228253 A1 EP 1228253A1 EP 01931816 A EP01931816 A EP 01931816A EP 01931816 A EP01931816 A EP 01931816A EP 1228253 A1 EP1228253 A1 EP 1228253A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- steel
- composition according
- weight
- compositions
- nitrogen
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 229910000831 Steel Inorganic materials 0.000 title claims abstract description 65
- 239000010959 steel Substances 0.000 title claims abstract description 65
- 239000000203 mixture Substances 0.000 title claims abstract description 58
- 238000000034 method Methods 0.000 title claims abstract description 12
- 229910052757 nitrogen Inorganic materials 0.000 claims abstract description 27
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 23
- 229910052758 niobium Inorganic materials 0.000 claims abstract description 20
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 10
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 5
- 239000012535 impurity Substances 0.000 claims abstract description 5
- 229910052742 iron Inorganic materials 0.000 claims abstract description 5
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 36
- 239000010955 niobium Substances 0.000 claims description 27
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims description 19
- 238000004519 manufacturing process Methods 0.000 claims description 18
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 15
- 239000011651 chromium Substances 0.000 claims description 10
- 238000010438 heat treatment Methods 0.000 claims description 7
- 238000010587 phase diagram Methods 0.000 claims description 7
- 230000009466 transformation Effects 0.000 claims description 7
- 230000000930 thermomechanical effect Effects 0.000 claims description 6
- 238000005242 forging Methods 0.000 claims description 5
- 230000008569 process Effects 0.000 claims description 5
- 238000005096 rolling process Methods 0.000 claims description 5
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 4
- 239000002893 slag Substances 0.000 claims description 3
- 230000006641 stabilisation Effects 0.000 claims description 2
- 238000011105 stabilization Methods 0.000 claims description 2
- 238000007493 shaping process Methods 0.000 claims 1
- 230000003647 oxidation Effects 0.000 abstract description 21
- 238000007254 oxidation reaction Methods 0.000 abstract description 21
- 229910052748 manganese Inorganic materials 0.000 abstract description 4
- 229910052759 nickel Inorganic materials 0.000 abstract description 3
- 229910052710 silicon Inorganic materials 0.000 abstract description 2
- 230000001747 exhibiting effect Effects 0.000 abstract 1
- 238000012360 testing method Methods 0.000 description 22
- 230000007797 corrosion Effects 0.000 description 12
- 238000005260 corrosion Methods 0.000 description 12
- 230000005496 eutectics Effects 0.000 description 10
- 239000012071 phase Substances 0.000 description 10
- 238000007711 solidification Methods 0.000 description 8
- 230000008023 solidification Effects 0.000 description 8
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 7
- 230000032683 aging Effects 0.000 description 7
- 229910052751 metal Inorganic materials 0.000 description 7
- 239000002184 metal Substances 0.000 description 7
- 150000001247 metal acetylides Chemical class 0.000 description 7
- 238000001556 precipitation Methods 0.000 description 7
- 229910001566 austenite Inorganic materials 0.000 description 6
- 238000005554 pickling Methods 0.000 description 6
- 238000005266 casting Methods 0.000 description 5
- 239000011572 manganese Substances 0.000 description 5
- 239000000047 product Substances 0.000 description 5
- 238000010008 shearing Methods 0.000 description 5
- FAPWRFPIFSIZLT-UHFFFAOYSA-M Sodium chloride Chemical compound [Na+].[Cl-] FAPWRFPIFSIZLT-UHFFFAOYSA-M 0.000 description 4
- 230000008901 benefit Effects 0.000 description 4
- 230000002349 favourable effect Effects 0.000 description 4
- 239000000446 fuel Substances 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 150000004767 nitrides Chemical class 0.000 description 4
- 239000002244 precipitate Substances 0.000 description 4
- 239000000243 solution Substances 0.000 description 4
- 238000011282 treatment Methods 0.000 description 4
- PMZURENOXWZQFD-UHFFFAOYSA-L Sodium Sulfate Chemical compound [Na+].[Na+].[O-]S([O-])(=O)=O PMZURENOXWZQFD-UHFFFAOYSA-L 0.000 description 3
- 229910045601 alloy Inorganic materials 0.000 description 3
- 239000000956 alloy Substances 0.000 description 3
- 238000002485 combustion reaction Methods 0.000 description 3
- 238000009826 distribution Methods 0.000 description 3
- 239000007788 liquid Substances 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- 238000001953 recrystallisation Methods 0.000 description 3
- 150000003839 salts Chemical class 0.000 description 3
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 2
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 2
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 230000001186 cumulative effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- GNTDGMZSJNCJKK-UHFFFAOYSA-N divanadium pentaoxide Chemical compound O=[V](=O)O[V](=O)=O GNTDGMZSJNCJKK-UHFFFAOYSA-N 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000001125 extrusion Methods 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 229910000464 lead oxide Inorganic materials 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- YEXPOXQUZXUXJW-UHFFFAOYSA-N oxolead Chemical compound [Pb]=O YEXPOXQUZXUXJW-UHFFFAOYSA-N 0.000 description 2
- 239000011780 sodium chloride Substances 0.000 description 2
- 229910052938 sodium sulfate Inorganic materials 0.000 description 2
- 235000011152 sodium sulphate Nutrition 0.000 description 2
- 230000035882 stress Effects 0.000 description 2
- 239000011593 sulfur Substances 0.000 description 2
- 238000009864 tensile test Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 230000004584 weight gain Effects 0.000 description 2
- 235000019786 weight gain Nutrition 0.000 description 2
- ZAMOUSCENKQFHK-UHFFFAOYSA-N Chlorine atom Chemical compound [Cl] ZAMOUSCENKQFHK-UHFFFAOYSA-N 0.000 description 1
- 229910001199 N alloy Inorganic materials 0.000 description 1
- 238000003915 air pollution Methods 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 239000007864 aqueous solution Substances 0.000 description 1
- 229910000963 austenitic stainless steel Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000033228 biological regulation Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 150000003841 chloride salts Chemical class 0.000 description 1
- 239000000460 chlorine Substances 0.000 description 1
- 229910052801 chlorine Inorganic materials 0.000 description 1
- BIJOYKCOMBZXAE-UHFFFAOYSA-N chromium iron nickel Chemical compound [Cr].[Fe].[Ni] BIJOYKCOMBZXAE-UHFFFAOYSA-N 0.000 description 1
- 238000004581 coalescence Methods 0.000 description 1
- 239000000567 combustion gas Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000007872 degassing Methods 0.000 description 1
- 210000001787 dendrite Anatomy 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000004090 dissolution Methods 0.000 description 1
- TXKMVPPZCYKFAC-UHFFFAOYSA-N disulfur monoxide Inorganic materials O=S=S TXKMVPPZCYKFAC-UHFFFAOYSA-N 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 230000002431 foraging effect Effects 0.000 description 1
- 239000003517 fume Substances 0.000 description 1
- 230000035784 germination Effects 0.000 description 1
- 238000007654 immersion Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- RUTXIHLAWFEWGM-UHFFFAOYSA-H iron(3+) sulfate Chemical compound [Fe+3].[Fe+3].[O-]S([O-])(=O)=O.[O-]S([O-])(=O)=O.[O-]S([O-])(=O)=O RUTXIHLAWFEWGM-UHFFFAOYSA-H 0.000 description 1
- 229910000360 iron(III) sulfate Inorganic materials 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- 229910001338 liquidmetal Inorganic materials 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 238000003303 reheating Methods 0.000 description 1
- 238000013515 script Methods 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000011734 sodium Substances 0.000 description 1
- 239000007790 solid phase Substances 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 238000004781 supercooling Methods 0.000 description 1
- 238000005303 weighing Methods 0.000 description 1
- 229910000859 α-Fe Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/48—Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum
-
- 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
- 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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/58—Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
Definitions
- the present invention relates to steel compositions more particularly intended for the manufacture of intake and exhaust valves for vehicles with internal combustion engines.
- this type of parts is subjected to significant mechanical stresses at temperatures which do not cease increasing with the increase in the power and the yields of the engines.
- the engine intake includes a turbo
- this temperature is generally between 200 and 400 ° C, but can reach 800 ° C at the exhaust when the fuel used is gasoline.
- the exhaust valves can thus be subjected to temperatures of up to 900 ° C on each explosion followed by an exhaust.
- the materials used for these valves must also resist sudden and significant variations in temperature. This increase in valve operating temperatures makes them even more sensitive to oxidation and corrosion by certain components contained in the fuels used, such as lead, sulfur or vanadium pentoxide, thereby reducing their duration of life.
- the steel or alloy used for their manufacture must also fulfill certain additional criteria.
- the manufacture of the valves generally takes place in two stages. The metallurgist will first develop a grade of steel or alloy which he will then deliver to the valve manufacturer in the form of rectified bars, but also peeled or according to any other surface condition specified by the customer. This manufacturer will then proceed to shear these bars, an operation also called cutting in plots.
- the cut into pieces is carried out at high temperature, and is followed by the transformation by extrusion of the pieces into valves at temperatures ranging from 1150 to 1200 ° C., which supposes that the granular structure of the bar delivered remains stable up to forging temperatures.
- the pieces are obtained by shearing at room temperature, which requires a slightly brittle metal to avoid non-uniform shearing and cracking of these pieces.
- a slightly brittle metal to avoid non-uniform shearing and cracking of these pieces.
- problems linked to the segregation of carbides in the pieces which leads, in particular, to excessive wear of the tools.
- the steels of the prior art are particularly problematic during shearing because the appearance of cracks in the parts requires frequent adjustments of the production lines.
- the materials traditionally used for the manufacture of such valves are, in particular, austenitic stainless steels, which have an iron-nickel-chromium base and are distributed between steels with high manganese content (up to 10% by weight) and steels with high nickel content (up to 21% by weight).
- Their resistance to oxidation at high temperature is not always satisfactory, in particular when, for example, the engine operates in a marine atmosphere and ingests chlorine, or even when an increase in the efficiency of the engine involves combustion gases. warmer.
- the present invention therefore essentially aims to remedy the aforementioned drawbacks of known steel compositions, by providing steel compositions having in particular an oxidation resistance, mechanical characteristics as well as improved processing properties. , which are in particular able to allow the manufacture of exhaust valves having a holding excellent mechanical and oxidation resistance in the range of 800 to 900 ° C.
- a first object of the invention consists of a steel composition comprising, expressed in percentages by weight: C 0.25 - 0.35%
- the steel composition comprises, expressed in percentages by weight:
- FIG. 5 represents a steel structure of the prior art.
- the heterogeneity of the structure can have other drawbacks during the manufacture of the parts.
- the automobile manufacturer shears round steel wires having a diameter of
- the nitrogen, niobium and carbon contents which are the three elements forming the niobium carbonitride Nb (C, N), are chosen such that the compositions results are hyper-eutectic in theoretical phase diagrams.
- the phase diagram of FIG. 3 represents an example of such a composition for which the eutectic E corresponds to a carbon content of approximately 0.15% by weight.
- compositions can be described as hyper-eutectic in theoretical phase diagrams, that in industrial practice the inventors still observe the primary precipitation of the austenite phase: this disagreement between theory and experimental reality can be justified by supercooling, germination and phase growth phenomena.
- the recrystallized structures are therefore homogeneous, a property which is very appreciable and very difficult to obtain in a reproducible manner by using the steel compositions of the prior art.
- the present inventors have also sought to limit the carbon content of the compositions according to the invention in order to reduce the potential rate of intergranular precipitation of the harmful carbide M23C6, during the final heat treatment for stabilizing the parts or when using these parts. .
- This potential rate of precipitation remains high, however, in the compositions according to the invention, nitrogen replacing carbon to form nitrides and carbonitrides.
- the ductility at room temperature measured by the elongation in the tensile test As d , remains very good.
- the oxidation resistance characteristics are also excellent.
- the present inventors have also found that the structure obtained at the end of the solidification of the ingots undergoes a significant modification after the conventional thermomechanical transformation operations (rolling, etc.). Indeed, we see that the network of rods of eutectic carbonitrides Nb (C, N) disappears, leaving room for a relatively homogeneous distribution of globular carbonitrides Nb (C, N) in processed products, such as rolled bars, by example, as can be seen in FIG. 6. When the nitrogen, niobium and carbon contents are such that the resulting compositions are hypo-eutectic in the theoretical phase diagrams, the niobium carbonitrides do not precipitate until the end of solidification, leading to an a priori less advantageous distribution.
- Chromium is essentially used to obtain good resistance to oxidation thanks to the passivated oxide layer which it forms on the surface of the metal. It also has a beneficial influence on the mechanical behavior at high temperature. Its content in the compositions according to the invention is 24 to 28%, preferably 25 to 26% by weight.
- Nickel has a sought-after gamma effect. Due to its price, it is limited to a content just sufficient for the solidification of the matrix in austenitic mode. Its content in the compositions according to the invention is 10 to 15%, preferably 11.5 to 12.5% by weight. Carbon has a desired hardening effect, but too high a content leads to the precipitation of embrittling carbides which are harmful to oxidation resistance. Its content in the compositions according to the invention is from 0.25 to 0.35% by weight, preferably from 0.25 to 0.32%.
- Nitrogen is a highly gammagenic element which in particular allows the compositions according to the invention to remain in the austenitic range by delaying the precipitation of the intermetallic phases. Its content is however limited due to the difficulties encountered in introducing it into steel compositions due to its low solubility limit in liquid steel. Its content is from 0.5 to 0.7%, preferably from 0.61 to 0.7% by weight. These contents also correspond to the quasi-saturation at equilibrium of the liquid metal at conventional processing temperatures, which is an advantage, because this addition is then easy with the usual means known to those skilled in the art.
- Niobium in addition to its carburogenic properties which are favorable for mechanical resistance to heat, makes it possible to obtain the eutectic previously described.
- Its content in the compositions according to the invention is 1.75 to 2.50%, preferably 1.90 to 2.30% by weight.
- the silicon is limited to a content of 0.30% by weight at most, although it improves the resistance to oxidation, because it is strongly sigmagenic and also lowers the solubility of nitrogen.
- the steel compositions according to the invention can be manufactured according to the methods applicable to the usual materials cited in reference, taking these characteristics into account.
- an electric furnace or an AOD reactor or any other means suitable for the production of steels containing high contents of the nitrogen alloy element, including secondary refining processes by slag remelting, may be used. electrically.
- the reflow can be done, for example, under slag with consumable electrode if one is looking for great inclusiveness.
- thermomechanical hot transformation process such as forging or rolling then by a softening treatment, which will preferably be carried out by maintaining at 1050-1 100 ° C for 1 to 16 hours. in air or in another fluid, which guarantees complete fine grain recrystallization and satisfactory ductility characteristics.
- the heat treatment for dissolving and recrystallization as well as the preheating of the products for manufacturing the valves may be carried out between 1100 and 1200 ° C; the higher temperatures bringing a grain magnification which remains limited.
- the stabilization heat treatment is intended to guarantee a certain structural and dimensional stability at the temperatures of use. It can be carried out, for example, in the form of a maintenance at 700-1000 ° C for 1 to 16 hours in air or in another fluid. In general, it is preferable to carry out this treatment at a temperature greater than or equal to the temperature of use of the part in service.
- valve steels being very strongly dependent on their thermal state
- the values which will be compared hereinafter are average values obtained for different thermal states of use all comprising a solution treatment at high temperature followed by '' aging at a lower temperature.
- the three grades A, B and C were previously treated by dissolving and aging at 850 ° C for 4 hours, while the reference steel grades were treated conventionally for each steel, which is favorable to them. in the comparison.
- the steel specimen is a 6 mm diameter cylinder on
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Physics & Mathematics (AREA)
- Heat Treatment Of Steel (AREA)
- Heat Treatment Of Articles (AREA)
- Application Of Or Painting With Fluid Materials (AREA)
- Contacts (AREA)
- Solid Fuels And Fuel-Associated Substances (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
Description
Claims
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0005967 | 2000-05-10 | ||
| FR0005967A FR2808807B1 (fr) | 2000-05-10 | 2000-05-10 | Composition d'acier, procede de fabrication et pieces formees dans ces compositions, en particulier soupapes |
| PCT/FR2001/001388 WO2001086009A1 (fr) | 2000-05-10 | 2001-05-07 | Composition d'acier, procede de fabrication et pieces formees dans ces compositions, en particulier soupapes |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| EP1228253A1 true EP1228253A1 (fr) | 2002-08-07 |
| EP1228253B1 EP1228253B1 (fr) | 2005-07-20 |
| EP1228253B8 EP1228253B8 (fr) | 2005-09-21 |
Family
ID=8850073
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP01931816A Expired - Lifetime EP1228253B8 (fr) | 2000-05-10 | 2001-05-07 | Composition d'acier, procede de fabrication et pieces formees dans ces compositions, en particulier soupapes |
Country Status (11)
| Country | Link |
|---|---|
| US (1) | US6656418B2 (fr) |
| EP (1) | EP1228253B8 (fr) |
| JP (1) | JP5288674B2 (fr) |
| AT (1) | ATE299953T1 (fr) |
| AU (1) | AU5850901A (fr) |
| BR (1) | BR0106337B1 (fr) |
| DE (1) | DE60112032T2 (fr) |
| ES (1) | ES2248325T3 (fr) |
| FR (1) | FR2808807B1 (fr) |
| MX (1) | MXPA02000345A (fr) |
| WO (1) | WO2001086009A1 (fr) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3575430A1 (fr) * | 2018-05-30 | 2019-12-04 | Garrett Transportation I Inc. | Alliages d'acier inoxydable, composants de turbocompresseur formés à partir d'alliages d'acier inoxydable et procédés de fabrication associés |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP5223046B2 (ja) * | 2005-11-02 | 2013-06-26 | 国立大学法人九州大学 | 生体用高窒素ニッケルフリーオーステナイト系ステンレス鋼の結晶粒微細化熱処理方法 |
| FR2896514B1 (fr) * | 2006-01-26 | 2008-05-30 | Aubert & Duval Soc Par Actions | Acier martensitique inoxydable et procede de fabrication d'une piece en cet acier, telle qu'une soupape. |
| JP6020957B2 (ja) * | 2012-02-02 | 2016-11-02 | 住友電気工業株式会社 | 内燃機関用材料の評価試験方法 |
| WO2017021565A1 (fr) | 2015-08-05 | 2017-02-09 | Gerdau Investigacion Y Desarrollo Europa, S.A. | Acier faiblement allié à résistance élevée et à résistance élevée à l'oxydation à chaud |
| US11725266B2 (en) | 2019-10-30 | 2023-08-15 | Garrett Transportation I Inc. | Stainless steel alloys, turbocharger components formed from the stainless steel alloys, and methods for manufacturing the same |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5040099B1 (fr) * | 1971-03-09 | 1975-12-22 | ||
| DE3310693A1 (de) * | 1983-03-24 | 1984-10-04 | Fried. Krupp Gmbh, 4300 Essen | Korrosionsbestaendiger chromstahl und verfahren zu seiner herstellung |
| JP2543417B2 (ja) * | 1989-12-05 | 1996-10-16 | トヨタ自動車株式会社 | 弁用鋼 |
| FR2664909B1 (fr) * | 1990-07-18 | 1994-03-18 | Aubert Duval Acieries | Acier austenitique ayant une resistance amelioree a haute temperature et procede pour son obtention et la realisation de pieces mecaniques, en particulier de soupapes. |
| JP2945112B2 (ja) * | 1990-10-09 | 1999-09-06 | 株式会社東芝 | 吸振ばね合金およびこれを用いたばね部材と、このばね部材を用いた電子機器 |
| US5257453A (en) * | 1991-07-31 | 1993-11-02 | Trw Inc. | Process for making exhaust valves |
| JPH0849512A (ja) * | 1994-08-03 | 1996-02-20 | Hitachi Metals Ltd | エンジンバルブ |
| JP3486713B2 (ja) * | 1998-02-25 | 2004-01-13 | 株式会社クボタ | 可逆式熱間圧延機のファーネスコイラードラム鋳造用高温強度・耐熱疲労特性にすぐれた耐熱鋳鋼 |
| JP3486714B2 (ja) * | 1998-09-25 | 2004-01-13 | 株式会社クボタ | 可逆式熱間圧延機の保熱炉内コイラードラム鋳造用耐肌荒れ性等にすぐれた耐熱鋳鋼 |
-
2000
- 2000-05-10 FR FR0005967A patent/FR2808807B1/fr not_active Expired - Lifetime
-
2001
- 2001-05-07 EP EP01931816A patent/EP1228253B8/fr not_active Expired - Lifetime
- 2001-05-07 ES ES01931816T patent/ES2248325T3/es not_active Expired - Lifetime
- 2001-05-07 MX MXPA02000345A patent/MXPA02000345A/es active IP Right Grant
- 2001-05-07 AU AU58509/01A patent/AU5850901A/en not_active Abandoned
- 2001-05-07 DE DE60112032T patent/DE60112032T2/de not_active Expired - Lifetime
- 2001-05-07 AT AT01931816T patent/ATE299953T1/de active
- 2001-05-07 WO PCT/FR2001/001388 patent/WO2001086009A1/fr not_active Ceased
- 2001-05-07 BR BRPI0106337-5A patent/BR0106337B1/pt not_active IP Right Cessation
- 2001-05-07 JP JP2001582596A patent/JP5288674B2/ja not_active Expired - Lifetime
- 2001-05-07 US US10/030,860 patent/US6656418B2/en not_active Expired - Lifetime
Non-Patent Citations (1)
| Title |
|---|
| See references of WO0186009A1 * |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3575430A1 (fr) * | 2018-05-30 | 2019-12-04 | Garrett Transportation I Inc. | Alliages d'acier inoxydable, composants de turbocompresseur formés à partir d'alliages d'acier inoxydable et procédés de fabrication associés |
| US10927439B2 (en) | 2018-05-30 | 2021-02-23 | Garrett Transportation I Inc | Stainless steel alloys, turbocharger components formed from the stainless steel alloys, and methods for manufacturing the same |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2003532795A (ja) | 2003-11-05 |
| ATE299953T1 (de) | 2005-08-15 |
| WO2001086009A1 (fr) | 2001-11-15 |
| MXPA02000345A (es) | 2004-05-21 |
| FR2808807B1 (fr) | 2002-07-19 |
| US6656418B2 (en) | 2003-12-02 |
| EP1228253B1 (fr) | 2005-07-20 |
| ES2248325T3 (es) | 2006-03-16 |
| EP1228253B8 (fr) | 2005-09-21 |
| DE60112032T2 (de) | 2006-07-20 |
| BR0106337B1 (pt) | 2014-09-30 |
| JP5288674B2 (ja) | 2013-09-11 |
| AU5850901A (en) | 2001-11-20 |
| DE60112032D1 (de) | 2005-08-25 |
| BR0106337A (pt) | 2002-04-02 |
| FR2808807A1 (fr) | 2001-11-16 |
| US20030044304A1 (en) | 2003-03-06 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN102171375B (zh) | 用于制造Ni基合金的方法以及Ni基合金 | |
| EP1979583B1 (fr) | Procédé de fabrication d'une soupape de moteur à explosion, et soupape ainsi obtenue | |
| CN114196854B (zh) | 一种高强度难变形镍基高温合金及其制备方法 | |
| WO2008029011A2 (fr) | Tôle d'acier pour la fabrication de structures allegees et procede de fabrication de cette tôle | |
| CH501058A (fr) | Alliage de nickel | |
| JPWO2017056674A1 (ja) | 低熱膨張超耐熱合金及びその製造方法 | |
| CN111417739B (zh) | Ni基合金的制造方法及Ni基合金 | |
| EP0855449B1 (fr) | Alliage à base de nickel résistant à la corrosion intergranulaire à des temperatures élevées ayant une structure de grains colonnaire, procédé de fabrication de cet alliage, pièce de grandes dimensions, et procédé de fabrication d'un pièce de grandes dimensions en cet alliage | |
| EP0008996A1 (fr) | Procédé de traitement thermique des alliages aluminium-cuivre-magnésium-silicium | |
| EP1228253B1 (fr) | Composition d'acier, procede de fabrication et pieces formees dans ces compositions, en particulier soupapes | |
| CN118531265A (zh) | 高强韧铸造铝合金及其制备方法和应用 | |
| CA2444175C (fr) | Acier a outils a tenacite renforcee, procede de fabrication de pieces dans cet acier et pieces obtenues | |
| FR2832425A1 (fr) | Alliage austentique pour tenue a chaud a coulabilite et transformation ameliorees | |
| JP4088546B2 (ja) | 高温特性に優れたアルミニウム合金鍛造材の製造方法 | |
| EP0388283B1 (fr) | Acier inoxydable ferritique et procédé pour l'élaboration d'un tel acier | |
| JP2543417B2 (ja) | 弁用鋼 | |
| EP0601915B1 (fr) | Alliage à base de nickel du système quaternaire Ni-Fe-Cr-Mo à durcissement par précipitation de phase gamma prime et résistant aux modes de corrosion rencontrés notamment dans l'industrie pétrolière | |
| FR2928661A1 (fr) | Alliage a base de ni pour rotor de turbine a vapeur et rotor de turbine a vapeur | |
| JP2001294959A (ja) | 単結晶Ni基耐熱合金およびタービン翼 | |
| JPH09241767A (ja) | 超耐熱合金の消耗電極式再溶解法 | |
| WO2023187301A1 (fr) | Tôle en alliage 6xxx de recyclage et procédé de fabrication | |
| EP0424277B1 (fr) | Procédé d'amélioration de la résistance à la corrosion d'un alliage à base de nickel et alliage ainsi réalisé | |
| FR2543577A1 (fr) | Superalliages a base de nickel renforces par du monocarbure et pieces solidifiees unidirectionnellement obtenues a partir de ces alliages | |
| CN118664174A (zh) | 一种焊接用镍基盘条及其制备方法 | |
| JP2003221627A (ja) | 高清浄マルエージング鋼の製造方法 |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
| 17P | Request for examination filed |
Effective date: 20020112 |
|
| AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE TR |
|
| AX | Request for extension of the european patent |
Free format text: AL;LT;LV;MK;RO;SI |
|
| GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
| GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
| GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
| AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE TR |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20050720 Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20050720 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20050720 |
|
| REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
| REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
| REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: FRENCH |
|
| REF | Corresponds to: |
Ref document number: 60112032 Country of ref document: DE Date of ref document: 20050825 Kind code of ref document: P |
|
| RAP2 | Party data changed (patent owner data changed or rights of a patent transferred) |
Owner name: AUBERT & DUVAL |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20051020 |
|
| NLT2 | Nl: modifications (of names), taken from the european patent patent bulletin |
Owner name: AUBERT & DUVAL Effective date: 20050907 |
|
| REG | Reference to a national code |
Ref country code: SE Ref legal event code: TRGR |
|
| REG | Reference to a national code |
Ref country code: GR Ref legal event code: EP Ref document number: 20050403181 Country of ref document: GR |
|
| NLV1 | Nl: lapsed or annulled due to failure to fulfill the requirements of art. 29p and 29m of the patents act | ||
| GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 20060123 |
|
| REG | Reference to a national code |
Ref country code: IE Ref legal event code: FD4D |
|
| REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2248325 Country of ref document: ES Kind code of ref document: T3 |
|
| PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20060531 |
|
| 26N | No opposition filed |
Effective date: 20060421 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20060507 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20050720 |
|
| REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 16 |
|
| REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 17 |
|
| REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 18 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20200522 Year of fee payment: 20 Ref country code: PT Payment date: 20200504 Year of fee payment: 20 Ref country code: GR Payment date: 20200512 Year of fee payment: 20 Ref country code: CH Payment date: 20200520 Year of fee payment: 20 Ref country code: DE Payment date: 20200520 Year of fee payment: 20 Ref country code: TR Payment date: 20200505 Year of fee payment: 20 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: BE Payment date: 20200527 Year of fee payment: 20 Ref country code: IT Payment date: 20200528 Year of fee payment: 20 Ref country code: GB Payment date: 20200527 Year of fee payment: 20 Ref country code: SE Payment date: 20200527 Year of fee payment: 20 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: AT Payment date: 20200522 Year of fee payment: 20 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: ES Payment date: 20200728 Year of fee payment: 20 |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R071 Ref document number: 60112032 Country of ref document: DE |
|
| REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
| REG | Reference to a national code |
Ref country code: GB Ref legal event code: PE20 Expiry date: 20210506 |
|
| REG | Reference to a national code |
Ref country code: AT Ref legal event code: MK07 Ref document number: 299953 Country of ref document: AT Kind code of ref document: T Effective date: 20210507 |
|
| REG | Reference to a national code |
Ref country code: BE Ref legal event code: MK Effective date: 20210507 |
|
| REG | Reference to a national code |
Ref country code: SE Ref legal event code: EUG |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PT Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20210518 |
|
| REG | Reference to a national code |
Ref country code: ES Ref legal event code: FD2A Effective date: 20210826 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20210506 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: ES Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20210508 |