EP2865774B1 - Aluminium casting alloy - Google Patents
Aluminium casting alloy Download PDFInfo
- Publication number
- EP2865774B1 EP2865774B1 EP13382424.3A EP13382424A EP2865774B1 EP 2865774 B1 EP2865774 B1 EP 2865774B1 EP 13382424 A EP13382424 A EP 13382424A EP 2865774 B1 EP2865774 B1 EP 2865774B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- weight
- alloy
- aluminium casting
- aluminium
- casting alloy
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 229910045601 alloy Inorganic materials 0.000 title claims description 50
- 239000000956 alloy Substances 0.000 title claims description 50
- 229910052782 aluminium Inorganic materials 0.000 title claims description 26
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title claims description 26
- 239000004411 aluminium Substances 0.000 title claims description 22
- 238000005266 casting Methods 0.000 title claims description 19
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 16
- 239000010949 copper Substances 0.000 claims description 11
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 10
- 229910052802 copper Inorganic materials 0.000 claims description 9
- 239000011572 manganese Substances 0.000 claims description 9
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 8
- 229910052742 iron Inorganic materials 0.000 claims description 8
- 239000011777 magnesium Substances 0.000 claims description 7
- 229910052710 silicon Inorganic materials 0.000 claims description 7
- 229910052749 magnesium Inorganic materials 0.000 claims description 6
- 229910052748 manganese Inorganic materials 0.000 claims description 6
- 239000010703 silicon Substances 0.000 claims description 6
- 239000011701 zinc Substances 0.000 claims description 6
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 5
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 5
- 229910052759 nickel Inorganic materials 0.000 claims description 5
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 4
- 239000010936 titanium Substances 0.000 claims description 4
- 229910052725 zinc Inorganic materials 0.000 claims description 4
- 229910052718 tin Inorganic materials 0.000 claims description 3
- 229910052719 titanium Inorganic materials 0.000 claims description 3
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 2
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 2
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 claims description 2
- 235000019589 hardness Nutrition 0.000 description 11
- 239000000203 mixture Substances 0.000 description 7
- 238000005299 abrasion Methods 0.000 description 6
- 229910000765 intermetallic Inorganic materials 0.000 description 5
- 229910005347 FeSi Inorganic materials 0.000 description 4
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 4
- 238000004512 die casting Methods 0.000 description 4
- 230000000052 comparative effect Effects 0.000 description 3
- 238000005476 soldering Methods 0.000 description 3
- 238000007669 thermal treatment Methods 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 2
- 230000032683 aging Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910016943 AlZn Inorganic materials 0.000 description 1
- 229910000967 As alloy Inorganic materials 0.000 description 1
- 229910000676 Si alloy Inorganic materials 0.000 description 1
- 238000003723 Smelting Methods 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- CSDREXVUYHZDNP-UHFFFAOYSA-N alumanylidynesilicon Chemical group [Al].[Si] CSDREXVUYHZDNP-UHFFFAOYSA-N 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 238000012512 characterization method Methods 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 238000005868 electrolysis reaction Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- BHEPBYXIRTUNPN-UHFFFAOYSA-N hydridophosphorus(.) (triplet) Chemical compound [PH] BHEPBYXIRTUNPN-UHFFFAOYSA-N 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 229910052745 lead Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012805 post-processing Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
Definitions
- the field of the invention is related to aluminium casting alloys.
- the present invention relates to a hypoeutectic secondary aluminum-silicon alloy, useful to produce, by high pressure die casting, components which have to fulfill premium abrasion resistance requirements in as-cast condition at room temperature.
- Aluminum casting alloys have not been traditionally well suited for abrasion applications in which, among others, high hardness properties must be present.
- abrasion requirements are, among other, piston cylinders, brake discs or steering boxes.
- Brake discs and piston cylinders must support not only abrasion but also thermal fatigue resistance, and if aluminium is employed instead of steel, hypereutectic alloys have been traditionally applied to produce automotive components by gravity die casting (GC).
- GC gravity die casting
- Hypereutectic alloys present primary silicon grains that are normally refined with phosporous and T5 thermal treatment to resist abrasion.
- Nickel is the most important alloying element, with also Copper and dissoluted Zinc, to keep mechanical properties at high temperatures.
- hypereutectic alloys are not so well suited. They do not fulfill the required hardness (above 115-120HB), Nickel is superfluous and Phosphorous is so volatile that requires skilled technicians to melt the alloy, which must be hold at temperatures above 750°C. Only high hardness and high strength are the objective properties, which opens the door to components produced by high pressure die casting (HPDC) with hypoeutectic aluminum.
- HPDC high pressure die casting
- HPDC process has been widely employed to new applications in the last twenty years, due to its low cost for big series, a high component reproducibility and reliability and it is hence mostly preferred when compared with GC.
- Alloys of primary quality with a Fe/Mn ratio of 1 ⁇ 2 has been disclosed in the prior art, and decrease die soldering and reduce as much as possible the negative effect of Al 5 FeSi intermetallics on the elongation values.
- WO2006/066314 discloses an aluminium-based high pressure die casting comprising (in wt.%): 4 to 4.9% Cu; 0.09-0.7% Mg; 0.19-0.21% Mn; 0.1-0.12% Ni; 8.3-9.2% Si ; 0.98-1% Fe; 0.5-0.56 Zn; ⁇ 0.1% Sn; ⁇ 0.1% Pb; ⁇ 0.1% Ti, ⁇ 0.1 % Cr, and the remainder consisting of aluminium and incidental impurities.
- elongation and mechanical properties elongation (A) equal to or more than 1%, yield strength (Rp0.2) equal to or more than 200 MPa, ultimate tensile strength (Rm) equal to or more than 300 MPa and Brinell Hardness (HB) equal to or more than 120 HB.
- elongation and mechanical properties are required for components designed to support simultaneously high abrasion and high static bending/torsion loads, maintaining a minimal ductility and other processing properties as alloy fluidity, low die soldering, easy welding or high machinability, among others.
- a preferred embodiment of the present invention is an aluminium casting alloy, wherein said alloy consists of:
- Silicon content has been set into a wide range between 7-11% by weight to guarantee high fluidity, especially for thin wall castings.
- Copper content has been set at values above 4% as it is required to get hardness above 125 HB and high strength.
- Magnesium content is also a key element to maximize the hardness and mechanical properties, whose content must be coupled with the copper content, showing best performance when both set above 0.5% by weight and 4% by weight, respectively.
- Iron content plays a key role into the mechanical properties and hence it has been limited to 0.6-1% by weight to guarantee both low mold soldering and small volume fraction of Al 5 FeSi intermetallics, which are minimized by the manganese content, implying an elongation above 1%.
- the manganese content helps to transform the Al 5 FeSi intermetallics into Al 12 (Mn,Fe)Si 2 and to reduce as much as possible the negative effect of those intermetallics. Values of manganese above 0.3% by weight were not found to be useful in terms of Al 5 FeSi intermetallics transformation.
- a further embodiment of the invention is the aluminium casting alloy of the invention, wherein said alloy comprises 8-9% by weight of silicon.
- a further embodiment of the invention is the aluminium casting alloy of the invention, wherein said alloy comprises 0.8-1 % by weight of iron.
- a further embodiment of the invention is the aluminium casting alloy of the invention, wherein said alloy comprises 4-4.5% by weight of copper.
- a further embodiment of the invention is the aluminium casting alloy of the invention, wherein said alloy comprises 0.05-0.3% by weight of manganese.
- a further embodiment of the invention is the aluminium casting alloy of the invention, wherein said alloy comprises 0.6-0.7% by weight of magnesium.
- Example 1 Aluminium casting alloys (prepararation, composition and mechanical properties)
- Aluminium compositions have been prepared by melting a standard EN-AC 46500 alloy in a holding furnace at 690°C and later poured into the injection vessel, being injected into the mold cavity of a 950 tonnes closing force HPDC machine at 685°C. No vacuum conditions were applied.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Cell Electrode Carriers And Collectors (AREA)
- Conductive Materials (AREA)
- Fuel Cell (AREA)
- Refinement Of Pig-Iron, Manufacture Of Cast Iron, And Steel Manufacture Other Than In Revolving Furnaces (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
Description
- The field of the invention is related to aluminium casting alloys. Specifically, the present invention relates to a hypoeutectic secondary aluminum-silicon alloy, useful to produce, by high pressure die casting, components which have to fulfill premium abrasion resistance requirements in as-cast condition at room temperature.
- Aluminum casting alloys have not been traditionally well suited for abrasion applications in which, among others, high hardness properties must be present.
- Regarding the automotive sector, in which most of the aluminum castings are consumed, some well-known parts that must fulfill abrasion requirements are, among other, piston cylinders, brake discs or steering boxes. Brake discs and piston cylinders must support not only abrasion but also thermal fatigue resistance, and if aluminium is employed instead of steel, hypereutectic alloys have been traditionally applied to produce automotive components by gravity die casting (GC). Hypereutectic alloys present primary silicon grains that are normally refined with phosporous and T5 thermal treatment to resist abrasion. Nickel is the most important alloying element, with also Copper and dissoluted Zinc, to keep mechanical properties at high temperatures.
- For room temperature applications (i.e. steering boxes) hypereutectic alloys are not so well suited. They do not fulfill the required hardness (above 115-120HB), Nickel is superfluous and Phosphorous is so volatile that requires skilled technicians to melt the alloy, which must be hold at temperatures above 750°C. Only high hardness and high strength are the objective properties, which opens the door to components produced by high pressure die casting (HPDC) with hypoeutectic aluminum.
- HPDC process has been widely employed to new applications in the last twenty years, due to its low cost for big series, a high component reproducibility and reliability and it is hence mostly preferred when compared with GC.
- Unfortunately, typical hardnesses of hypoeutectic alloys lie on values around 80-100 HB, what is still below the required 120HB. Therefore, when producing steering boxes, a steel sleeve is placed in the internal surface of the box to accommodate the steering shaft. Both shaft and box are typically AlSi9Cu3 as cast components produced by HPDC, and even the addition of a new step (sleeve placement) is worth when compared with expensive GC production with hypereutectic alloy with a T5 thermal treatment.
- Some other new alloys have been later developed to eliminate the thermal treatments, as those belonging to the AlZn families, which after 1 week of natural aging reach hardness values close to 120 HB. Unfortunately, the main disadvantage of these alloys is that quality requirements are only achievable by primary alloys. Primary alloys means mainly Iron content below 0.15% by weight, Copper content below 0.03% by weight and Zinc content below 0.1% by weight, being those contents only achievable if Aluminium is produced by electrolysis smelting from raw alumina. All refined aluminium alloys produced from scraps, drosses and swarfs coming from post-processing operations and end of life products is hence limited to low mechanical secondary alloy applications, what is a large limitation for industry sustainability and for the aluminum recycling sector.
- Alloys of primary quality with a Fe/Mn ratio of ½ has been disclosed in the prior art, and decrease die soldering and reduce as much as possible the negative effect of Al5FeSi intermetallics on the elongation values.
-
WO2006/066314 discloses an aluminium-based high pressure die casting comprising (in wt.%): 4 to 4.9% Cu; 0.09-0.7% Mg; 0.19-0.21% Mn; 0.1-0.12% Ni; 8.3-9.2% Si ; 0.98-1% Fe; 0.5-0.56 Zn; <0.1% Sn; <0.1% Pb; <0.1% Ti, <0.1 % Cr, and the remainder consisting of aluminium and incidental impurities. - The problem to be solved is the provision of a novel alloy of secondary quality produced for HPDC which can be used in as-cast condition and that presents the following values of elongation and mechanical properties: elongation (A) equal to or more than 1%, yield strength (Rp0.2) equal to or more than 200 MPa, ultimate tensile strength (Rm) equal to or more than 300 MPa and Brinell Hardness (HB) equal to or more than 120 HB. Said values of elongation and mechanical properties are required for components designed to support simultaneously high abrasion and high static bending/torsion loads, maintaining a minimal ductility and other processing properties as alloy fluidity, low die soldering, easy welding or high machinability, among others.
- A preferred embodiment of the present invention is an aluminium casting alloy, wherein said alloy consists of:
- 7-11% by weight of silicon,
- 0.6-1% by weight of iron,
- 4-5% by weight of copper,
- 0.05-0.5% by weight of manganese,
- 0.05-1.2% by weight of zinc,
- 0.56-0.9% by weight of magnesium,
- 0.01-0.15% by weight of titanium,
- 0.01-0.1% by weight of chrome,
- 0.01-0.1% by weight of nickel,
- 0.01-0.1 % by weight of lead and
- 0.01-0.1% by weight of tin,
- herewith aluminium casting alloy of the invention.
- Silicon content has been set into a wide range between 7-11% by weight to guarantee high fluidity, especially for thin wall castings.
- Copper content has been set at values above 4% as it is required to get hardness above 125 HB and high strength.
- Magnesium content is also a key element to maximize the hardness and mechanical properties, whose content must be coupled with the copper content, showing best performance when both set above 0.5% by weight and 4% by weight, respectively.
- Iron content plays a key role into the mechanical properties and hence it has been limited to 0.6-1% by weight to guarantee both low mold soldering and small volume fraction of Al5FeSi intermetallics, which are minimized by the manganese content, implying an elongation above 1%.
- The manganese content helps to transform the Al5FeSi intermetallics into Al12(Mn,Fe)Si2 and to reduce as much as possible the negative effect of those intermetallics. Values of manganese above 0.3% by weight were not found to be useful in terms of Al5FeSi intermetallics transformation.
- A further embodiment of the invention is the aluminium casting alloy of the invention, wherein said alloy comprises 8-9% by weight of silicon.
- A further embodiment of the invention is the aluminium casting alloy of the invention, wherein said alloy comprises 0.8-1 % by weight of iron.
- A further embodiment of the invention is the aluminium casting alloy of the invention, wherein said alloy comprises 4-4.5% by weight of copper.
- A further embodiment of the invention is the aluminium casting alloy of the invention, wherein said alloy comprises 0.05-0.3% by weight of manganese.
- A further embodiment of the invention is the aluminium casting alloy of the invention, wherein said alloy comprises 0.6-0.7% by weight of magnesium.
- Aluminium compositions have been prepared by melting a standard EN-AC 46500 alloy in a holding furnace at 690°C and later poured into the injection vessel, being injected into the mold cavity of a 950 tonnes closing force HPDC machine at 685°C. No vacuum conditions were applied.
- A serial of 30 specimens were produced, for each composition. Casted specimens were cooled down in air. Specimens dimensions and later mechanical characterization were set and carried out following, respectively, UNE-EN ISO 6892-1 B:2010 standards. For the hardness determination, plate specimens with 5 mm thickness have been casted and tested.
- Several compositions were tested, the content of the content if specified in Table 1. The obtained results are also specified in Table 1.
Table 1 Alloy 1 (comparative composition, not according to the invention) Alloy 2 (comparative composition, not according to the invention) Alloy 3 Alloy 4 Si (% by weight) 8.68 9.08 8.9 10.41 Fe (% by weight) 0.95 1.07 1.32 1.32 Cu (% by weight) 1.78 3.1 4.33 3.97 Mn (% by weight) 0.33 0.272 0.272 0.54 Mg (% by weight) 0.046 0.62 0.56 0.54 Zn (% by weight) 1.74 1.23 1.19 1.14 Ti (% by weight) 0.023 0.188 0.225 0.272 Cr (% by weight) 0.018 0.195 0.198 0.189 Ni (% by weight) 0.062 0.099 0.106 0.102 Pb (% by weight) 0.051 0.091 0.092 0.087 Sn (% by weight) 0.018 0.034 0.036 0.035 Rp0.2 (MPa) 150 208 227 218 Rm (MPa) 290 300 305 290 A (%) 4.5 1.75 1.2 1.1 Brinell Hardness (HB) - 116 125 122 - The values obtained after one month of natural aging is shown in Table 2.
Table 2 Alloy 2 (comparative composition, not according to the invention) Alloy 3 Alloy 4 Rp0.2 (MPa) 220 241.5 230 Rm (MPa) 317 324 300 A (%) 2.2 2.4 2 Brinell Hardness (HB) 120 135 130
Claims (6)
- Aluminium casting alloy, characterized in that said alloy is consisting of:7-11% by weight of silicon,0.6-1 % by weight of iron,4-5% by weight of copper,0.05-0.5% by weight of manganese,0.05-1.2% by weight of zinc,0.56-0.9% by weight of magnesium,0.01-0.15% by weight of titanium,0.01-0.1 % by weight of chrome,0.01-0.1% by weight of nickel,0.01-0.1% by weight of lead,0.01-0.1 % by weight of tin,and aluminium as the remainder.
- Aluminium casting alloy according to claim 1, characterized in that said alloy is consisting of 8-9% by weight of silicon.
- Aluminium casting alloy according to claim 1 or claim 2, characterized in that said alloy is consisting of 0.8-1% by weight of iron.
- Aluminium casting alloy according to any one of claims 1 to 3, characterized in that said alloy is consisting of 4-4.5% by weight of copper.
- Aluminium casting alloy according to any one of claims 1 to 4, characterized in that said alloy is consisting of 0.05-0.3% by weight of manganese.
- Aluminium casting alloy according to any one of claims 1 to 5, characterized in that said alloy is consisting of 0.6-0.7% by weight of magnesium.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP13382424.3A EP2865774B1 (en) | 2013-10-23 | 2013-10-23 | Aluminium casting alloy |
| ES13382424.3T ES2582530T3 (en) | 2013-10-23 | 2013-10-23 | Cast aluminum alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP13382424.3A EP2865774B1 (en) | 2013-10-23 | 2013-10-23 | Aluminium casting alloy |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP2865774A1 EP2865774A1 (en) | 2015-04-29 |
| EP2865774B1 true EP2865774B1 (en) | 2016-04-13 |
Family
ID=49517464
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP13382424.3A Active EP2865774B1 (en) | 2013-10-23 | 2013-10-23 | Aluminium casting alloy |
Country Status (2)
| Country | Link |
|---|---|
| EP (1) | EP2865774B1 (en) |
| ES (1) | ES2582530T3 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2024194350A1 (en) | 2023-03-20 | 2024-09-26 | Federal-Mogul Nürnberg GmbH | Method for producing a brake disk or a brake drum, brake disk or brake drum, use of an aluminum alloy to produce a brake disk or a brake drum, and disk brake or drum brake |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105671353B (en) * | 2016-01-26 | 2017-09-26 | 山东正诺集团有限公司 | A kind of enhanced aluminium base of inorganic particulate is braked the preparation method of disk material |
| CN106591640B (en) * | 2016-11-18 | 2019-04-16 | 广州致远新材料科技有限公司 | A kind of wear-resistant aluminum alloy |
| EP3342888B1 (en) * | 2016-12-28 | 2019-05-29 | Befesa Aluminio, S.L. | Aluminium casting alloy |
| KR101955993B1 (en) * | 2017-02-17 | 2019-03-08 | 주식회사 지.에이.엠 | High strength aluminium alloy and high strength aluminium alloy casting |
| CN108411166A (en) * | 2018-02-28 | 2018-08-17 | 山东河山机械股份有限公司 | A kind of pack alloy and preparation method thereof |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0111082A1 (en) * | 1982-10-16 | 1984-06-20 | Cosworth Research And Development Limited | Aluminium alloy for casting |
| GB2332449B (en) * | 1997-12-20 | 2002-05-22 | Ae Goetze Automotive Ltd | Aluminium alloy |
| US6908590B2 (en) * | 2002-03-19 | 2005-06-21 | Spx Corporation | Aluminum alloy |
| JP5236948B2 (en) * | 2004-12-23 | 2013-07-17 | コモンウェルス サイエンティフィック アンドインダストリアル リサーチ オーガナイゼーション | Heat treatment of aluminum alloy high pressure die castings. |
-
2013
- 2013-10-23 ES ES13382424.3T patent/ES2582530T3/en active Active
- 2013-10-23 EP EP13382424.3A patent/EP2865774B1/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2024194350A1 (en) | 2023-03-20 | 2024-09-26 | Federal-Mogul Nürnberg GmbH | Method for producing a brake disk or a brake drum, brake disk or brake drum, use of an aluminum alloy to produce a brake disk or a brake drum, and disk brake or drum brake |
| DE102023106915A1 (en) | 2023-03-20 | 2024-09-26 | Federal-Mogul Nürnberg GmbH | Method for producing a brake disc, brake disc and use of an aluminium alloy for producing a brake disc |
Also Published As
| Publication number | Publication date |
|---|---|
| EP2865774A1 (en) | 2015-04-29 |
| ES2582530T3 (en) | 2016-09-13 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP2865774B1 (en) | Aluminium casting alloy | |
| JP5355320B2 (en) | Aluminum alloy casting member and manufacturing method thereof | |
| KR101124235B1 (en) | Aluminium alloy and aluminium alloy casting | |
| US20100288401A1 (en) | Aluminum casting alloy | |
| EP3954798B1 (en) | Die-cast aluminum alloy, preparation method therefor, and structural member for communication product | |
| KR20100041532A (en) | High strength aluminum alloys for die casting | |
| EP3342890B1 (en) | Aluminium casting alloy | |
| JP7565284B2 (en) | Casting alloys for high pressure vacuum die casting | |
| EP3342889B1 (en) | Aluminium casting alloy | |
| CN117568671A (en) | Die-casting aluminum alloy material free of heat treatment, preparation method thereof and automobile structural member | |
| EP2865772B1 (en) | Aluminium casting alloy | |
| KR101274089B1 (en) | High strength aluminum alloys for die casting | |
| EP2865773B1 (en) | Aluminium casting alloy | |
| US6649126B2 (en) | Aluminum alloy for high pressure die-casting | |
| KR20220141725A (en) | Aluminum alloy | |
| EP4083248A1 (en) | Aluminum alloy and preparation method thereof, and aluminum alloy structural member | |
| EP3342888B1 (en) | Aluminium casting alloy | |
| KR101780463B1 (en) | Aluminium alloy composition for die casting | |
| JP5522692B2 (en) | High strength copper alloy forging | |
| KR101269516B1 (en) | Scandium free high strength aluminum alloys for die casting | |
| KR102617997B1 (en) | Manufacturing method of die casting Al alloy | |
| US20210404038A1 (en) | 2xxx aluminum lithium alloys | |
| JP2011208178A (en) | Casting aluminum alloy | |
| JP2005082865A (en) | Non-heat treated aluminum alloy for die-casting, die-cast product obtained by using the alloy, and method for producing the product | |
| KR101311915B1 (en) | Aluminium alloy and aluminium alloy casting |
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: 20131023 |
|
| AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
| AX | Request for extension of the european patent |
Extension state: BA ME |
|
| R17P | Request for examination filed (corrected) |
Effective date: 20150519 |
|
| RAX | Requested extension states of the european patent have changed |
Extension state: ME Payment date: 20150519 Extension state: BA Payment date: 20150519 |
|
| RBV | Designated contracting states (corrected) |
Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
| RIC1 | Information provided on ipc code assigned before grant |
Ipc: C22C 21/02 20060101AFI20151125BHEP |
|
| GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
| INTG | Intention to grant announced |
Effective date: 20160107 |
|
| RIN1 | Information on inventor provided before grant (corrected) |
Inventor name: CRESPO CAMINO, IGNACIO Inventor name: ANZA ORTIZ DE APODACA, INIGO Inventor name: ABUIN ARICETA, ALBERTO Inventor name: SAENZ DE TEJADA PICORNELL, FRANCISCO Inventor name: VICARIO GOMEZ, IBAN |
|
| 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): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
| AX | Request for extension of the european patent |
Extension state: BA ME |
|
| REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D |
|
| REG | Reference to a national code |
Ref country code: AT Ref legal event code: REF Ref document number: 790236 Country of ref document: AT Kind code of ref document: T Effective date: 20160415 Ref country code: CH Ref legal event code: EP |
|
| REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 602013006467 Country of ref document: DE |
|
| REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG4D |
|
| REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2582530 Country of ref document: ES Kind code of ref document: T3 Effective date: 20160913 |
|
| REG | Reference to a national code |
Ref country code: AT Ref legal event code: MK05 Ref document number: 790236 Country of ref document: AT Kind code of ref document: T Effective date: 20160413 |
|
| REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 4 |
|
| REG | Reference to a national code |
Ref country code: NL Ref legal event code: MP Effective date: 20160413 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160713 Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160413 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: 20160413 Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160413 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: 20160413 |
|
| 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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160816 Ref country code: SE 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: 20160413 Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160413 Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160413 Ref country code: AT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160413 Ref country code: RS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160413 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160413 Ref country code: IT 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: 20160413 |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 602013006467 Country of ref document: DE |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160413 Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160413 Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160413 Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160413 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: 20160413 |
|
| 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: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160413 |
|
| 26N | No opposition filed |
Effective date: 20170116 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160413 |
|
| REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
| REG | Reference to a national code |
Ref country code: IE Ref legal event code: MM4A |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20161031 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20161031 |
|
| 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: 20161023 |
|
| REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 5 |
|
| 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 NON-PAYMENT OF DUE FEES Effective date: 20161023 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO Effective date: 20131023 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160413 Ref country code: MK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160413 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: 20160413 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160413 Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160413 Ref country code: MT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20161031 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160413 |
|
| REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 6 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160413 Ref country code: AL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20160413 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20230911 Year of fee payment: 11 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: ES Payment date: 20231114 Year of fee payment: 11 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20230830 Year of fee payment: 11 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20240927 Year of fee payment: 12 |