EP2041328A1 - Aluminiumlegierung und deren verwendung für ein gussbauteil insbesondere eines kraftwagens - Google Patents
Aluminiumlegierung und deren verwendung für ein gussbauteil insbesondere eines kraftwagensInfo
- Publication number
- EP2041328A1 EP2041328A1 EP07787546A EP07787546A EP2041328A1 EP 2041328 A1 EP2041328 A1 EP 2041328A1 EP 07787546 A EP07787546 A EP 07787546A EP 07787546 A EP07787546 A EP 07787546A EP 2041328 A1 EP2041328 A1 EP 2041328A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- cast
- aluminum alloy
- cast component
- motor vehicle
- weight
- 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
- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 37
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 30
- 239000000956 alloy Substances 0.000 claims abstract description 30
- 238000005266 casting Methods 0.000 claims abstract description 26
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 25
- 239000003921 oil Substances 0.000 claims abstract description 20
- 229910052749 magnesium Inorganic materials 0.000 claims abstract description 17
- 239000011777 magnesium Substances 0.000 claims abstract description 17
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims abstract description 16
- 229910052742 iron Inorganic materials 0.000 claims abstract description 14
- 238000004519 manufacturing process Methods 0.000 claims abstract description 14
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 14
- 239000010703 silicon Substances 0.000 claims abstract description 14
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 9
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 9
- 229910052712 strontium Inorganic materials 0.000 claims abstract description 9
- CIOAGBVUUVVLOB-UHFFFAOYSA-N strontium atom Chemical compound [Sr] CIOAGBVUUVVLOB-UHFFFAOYSA-N 0.000 claims abstract description 9
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims abstract description 7
- 239000010936 titanium Substances 0.000 claims abstract description 7
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 7
- 238000010438 heat treatment Methods 0.000 claims description 20
- 238000000034 method Methods 0.000 claims description 19
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 13
- 229910052748 manganese Inorganic materials 0.000 claims description 11
- 239000011572 manganese Substances 0.000 claims description 11
- 238000004512 die casting Methods 0.000 claims description 9
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 8
- 239000012535 impurity Substances 0.000 claims description 7
- 238000005275 alloying Methods 0.000 claims description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 3
- 239000010949 copper Substances 0.000 claims description 3
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 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 abstract description 2
- 239000000356 contaminant Substances 0.000 abstract 1
- 239000000047 product Substances 0.000 description 14
- CSDREXVUYHZDNP-UHFFFAOYSA-N alumanylidynesilicon Chemical compound [Al].[Si] CSDREXVUYHZDNP-UHFFFAOYSA-N 0.000 description 11
- 229910000676 Si alloy Inorganic materials 0.000 description 6
- 238000000137 annealing Methods 0.000 description 6
- 230000005496 eutectics Effects 0.000 description 6
- 239000000203 mixture Substances 0.000 description 5
- 239000000463 material Substances 0.000 description 4
- 238000012360 testing method Methods 0.000 description 4
- 230000015572 biosynthetic process Effects 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 239000013078 crystal Substances 0.000 description 2
- 230000001419 dependent effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 238000003801 milling Methods 0.000 description 2
- 238000012946 outsourcing Methods 0.000 description 2
- 238000011282 treatment Methods 0.000 description 2
- 229910019018 Mg 2 Si Inorganic materials 0.000 description 1
- 229910019752 Mg2Si Inorganic materials 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- FFBHFFJDDLITSX-UHFFFAOYSA-N benzyl N-[2-hydroxy-4-(3-oxomorpholin-4-yl)phenyl]carbamate Chemical compound OC1=C(NC(=O)OCC2=CC=CC=C2)C=CC(=C1)N1CCOCC1=O FFBHFFJDDLITSX-UHFFFAOYSA-N 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 238000004881 precipitation hardening Methods 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 238000009864 tensile test Methods 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
- 238000012549 training Methods 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/043—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with silicon as the next major constituent
-
- 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
-
- 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
- C22C21/04—Modified aluminium-silicon alloys
Definitions
- the invention relates to an aluminum alloy, in particular a die-cast alloy and its use in a cast component, in particular for a motor vehicle. Moreover, the invention relates to a cast component, in particular for a motor vehicle made of such an aluminum alloy.
- One way describes the use of relatively inexpensive secondary alloys, for example of the type AISiI OMg, which, however, a relatively high iron content of about 0.5 to 1, 2 wt .-% Fe and a low manganese content of about 0.1 wt .-% Mn exhibit.
- the high iron content is required, inter alia, against the background of the relatively low addition of manganese, so that the tendency of the aluminum alloy to adhere within the die is reduced and the finished cast component can be reliably removed from the mold.
- a cast component produced from such a secondary alloy in the form of an oil pan for a motor vehicle can be taken as known from EP 0 61 1 832 B1, in which a local heat treatment is carried out at a corresponding temperature or a corresponding period of time, so that component regions differ Set hardness.
- the oil sump in the region of a flange remains largely untreated and accordingly has a hardness of 85 to 110 HB and a ductility of 0.5 to 2.5%, while this is heat treated in a bottom area accordingly, so that it has a hardness of 55 to 80 HB and a ductility of above 4%.
- such a primary alloy can already be taken from EP 0 997 550 B1 as known, which - in contrast to the previously described Secondary alloys - a lower iron content of 0.15 to 0.35 wt .-% Fe and a contrast high manganese content of 0.3 to 0.6 wt .-% Mn.
- the intermetallic AlFeSi phases customary with secondary alloys do not exist in such a primary alloy. For example, this results in a rather roundish in cross-section, intermetallic Al 12 (Mn, Fe) Si 2 phase, which accordingly has no or no pronounced needle-shaped training.
- strontium is preferably added to the above-described primary alloy, which stops the needle-shaped growth of the silicon within the AISi eutectic.
- the cast components produced by such a primary alloy have only an elongation at break of A 5 of ⁇ 5% after demoulding, they are first used as safety components in the automotive industry in a subsequent heat treatment process at a temperature of 400 to 490 ° C partially solution-annealed for a period of 20 to 120 min and then cooled in air.
- a significant increase in the ductility of the cast component is achieved, so that sets an elongation at break of A 5 > 12%.
- the hardness of the cast component drops to a value of about 60 to 65 HB.
- Object of the present invention is therefore to provide an aluminum alloy and their use for a cast component in particular a motor vehicle of the type mentioned, with which the production of such a cast component can be realized much easier and therefore cheaper. Moreover, it is an object of the invention to produce a cast component made of such an aluminum alloy in particular for the motor vehicle industry with correspondingly high mechanical requirements in a simpler and more cost-effective manner. This object is achieved by an aluminum alloy with the features of claim 1, with their use in a cast component in particular a motor vehicle with the features of claim 6 and by a cast component of such an aluminum alloy in particular for a motor vehicle with the features of claim 10.
- Advantageous embodiments with expedient and non-trivial developments of the invention are specified in the dependent claims.
- the aluminum alloy which is to be used in particular as a die-cast alloy, comprises the following alloying elements:
- the proportion of AISi eutectic is significantly reduced and contrast, the proportion of aluminum mixed crystals significantly increased.
- the aluminum-silicon alloy according to the invention can be created with the aluminum alloy according to the invention, which have a hardness of> 80 HB, and preferably between 84 HB and 88 HB already in the cast state - ie without additional heat treatment after demoulding. It should be noted that these values are measured inside the cast component, ie below the casting skin of the component.
- the aluminum alloy according to the invention it is possible, despite the relatively high hardness, to achieve a very high ductility of the cast component, whose elongation at break is determined by the Removal - ie in the cast state and without further heat treatment - has a value of A 5 > 5%, and preferably 8% to 12%.
- the aluminum alloy according to the invention has a selected range of between 0.22 and 0.4% by weight of magnesium compared to that according to EP 0 997 550 B1, since the hardness of the cast component produced from the aluminum alloy is not limited to Eutectic, but also depends on the resulting outsourcing. Due to the specially selected magnesium content, Mg 2 Si ultrafine precipitates are formed by which the strength or hardness of the cast component can be adjusted. In other words, the hardness of the cast component produced from the aluminum alloy according to the invention is also dependent on the magnesium content.
- a particularly high hardness of the cast component of the aluminum alloy according to the invention can be achieved if the magnesium content is in a selected range of 0.3 to 0.4% by weight, and preferably 0 , 32 to 0.36 wt .-% is.
- the aluminum alloy according to the invention or the cast component produced therefrom already has the above-described high hardness or high elongation at break in the cast state, this is particularly suitable for use in motor vehicle construction.
- the use of the aluminum-silicon alloy according to the invention in oil pans for motor vehicles has proven to be particularly advantageous since it must have a relatively high ductility with an elongation at break A 5 of> 5% in order to provide adequate protection against crack formation within the oil pan to be able to, which may arise in particular due to falling rocks below the motor vehicle.
- the sumps in the connection or flange area must be sealed with a corresponding motor housing, it is necessary that they have a correspondingly high hardness of> 80 HB. Since a cast component produced from the present aluminum-silicon alloy fulfills these requirements already in the cast state without further heat treatment, it is thus possible to create an oil pan or another component for a motor vehicle that is easy to manufacture and therefore cost-effective.
- the aluminum alloy can be used in a die-casting process for the production of cast components, in particular for a motor vehicle, as a result, a particularly fast and cost-effective production of the cast components is possible.
- the inventive aluminum-silicon alloy used in the Following the casting process to be subjected to a heat treatment process.
- the component can additionally be hot-hardened after partial solution annealing in the temperature range of the precipitation hardening of Mg2Si.
- This thermosetting is preferably carried out in a temperature range of about 190 to 240 ° C, in particular about 190 to 220 ° C.
- the casting component produced by the new aluminum-silicon alloy is characterized in particular by the fact that it has an at least approximately uniform hardness of> 80 HB and preferably between 84 and 88 HB in the cast state in all component regions.
- the cast component advantageously has an at least approximately uniform elongation at break A 5 of> 5% and preferably 8% to 12% in all component regions.
- Fig. 2 is another process flow diagram of a heat treatment of a component of a motor vehicle.
- the silicon content is between 7 and 9 wt .-% and the magnesium content between 0.32 and 0.36 wt .-%.
- the present aluminum alloy is eminently suitable for use in die-casting of oil pans where an elongation at break A 5 of> 5% has to be achieved, in particular to prevent cracking when rockfall occurs during driving of the motor vehicle.
- the oil pans cast by means of the above aluminum-silicon alloy have a hardness of> 80 HB, and in particular between 84 and 88 HB, so that the oil pans in the connection or flange area correspond to one another Motor housing of the motor vehicle can be tightly closed.
- the casting skin of the as-cast condition The existing oil pans were correspondingly removed by a machining process, for example by milling, so that realistic hardness values of the oil pans in the cast state could be determined.
- the magnesium content is in particular about 0.3 wt .-%.
- the individual oil pans have not been heat treated. Consequently, the measured values relate to the casting state of the components, wherein the casting skin in the respective test area has in turn been correspondingly removed by a machining method, for example by milling.
- the present aluminum alloy in turn, is particularly well suited for use in die casting of oil pans where an elongation at break A 5 of> 5% must be achieved. Also in this alloy composition, a hardness of> 80 HB could be achieved.
- the B-pillars have been produced in a die casting process from an aluminum-silicon casting alloy in two variants, which have the following compositions:
- Variant 1 7.8 to 8.2% by weight of silicon 0.5 to 0.6% by weight of manganese 0.15 to 0.2% by weight of iron 0.27 to 0.33% by weight of magnesium 0.04 to 0.08% by weight of titanium 140 to 180 ppm of strontium
- Process 1 The two variants of the aluminum-silicon casting alloy - in particular variant 2 with a content of about 0.6 wt .-% magnesium - were, for example, the following, in FIGS. 1 and 2 using flowcharts explained heat treatments, subjected to:
- the B-pillars (product P) after casting in a step 1 - using a portion of the casting heat - are solution-annealed in a step 2 and quenched in the air by means of a fan.
- the product P is not cooled to room temperature, for example, after demolding from the casting tool, but rather solution-annealed at a temperature of about 200 ° C in step 2.
- a sprue A or other casting residues remain on the product P.
- the component After the solution heat treatment in step 2, the component is still relatively soft or ductile and can therefore be deburred in step 3. In this case, the sprue A or other casting residues are removed from the product P. The product P remains soft.
- the B-pillar or product P is straightened in step 4.
- the product P is further soft for this purpose.
- step 5 the product P is removed in step 5, specifically at one of the aging temperatures which will be described in more detail below. Thereafter, the product which is soft until after step 4 is adjusted according to its desired material properties.
- FIG. 2 shows a method which differs from that according to FIG. 1 in particular in that the steps 2 and 3 are reversed in their sequence and therefore no utilization of part of the casting heat takes place in the present case.
- step 1 the product P in the present case after step 1 is cooled together with the sprue A or other casting residues to room temperature or to about 20 ° C. Thereafter, the deburring 3 and the removal of the sprue and the casting remains, wherein the product is still soft.
- the solution annealing 2 and the subsequent cooling takes place for example in the air by means of a fan.
- the product P remains soft.
- Steps 4 and 5 so the straightening of the B-pillar or the product P and the outsourcing in one of the hereinafter described in more detail Auslageremperaturen, then again take place analogously to the method according to Fig.1.
- step 5 the product which is soft until after step 4 is in turn adjusted in accordance with its desired material properties.
- the solution annealing carried out in the respective step 2 of the two methods according to FIGS. 1 and 2 was carried out in different tests at different temperatures between 460 and 490 ° C. and during different annealing times of 15 to 120 minutes.
- the removal performed in the respective step 5 of the two methods according to FIGS. 1 and 2 likewise took place in different tests at different temperatures between 160 and 240 ° C. and during different removal times of 20 to 240 minutes.
- the heat treatment components were created for use, for example, in the body, in the chassis or in the drive train of the motor vehicle, which has a yield strength R p0,2 between 90 and 180 MPa, a tensile strength R m between 180 and 250 MPa and an elongation at break A 5 in the range between 8 and 22%.
- the present aluminum alloy is again particularly good for
- the high-strength components of a T5 annealing were subjected to different temperatures between 160 and 240 ° C and for different times from 20 to 240 min.
Landscapes
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Organic Chemistry (AREA)
- Metallurgy (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Crystallography & Structural Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Motor Or Generator Frames (AREA)
- Body Structure For Vehicles (AREA)
- Air-Conditioning For Vehicles (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Compositions Of Macromolecular Compounds (AREA)
- Induction Machinery (AREA)
Description
Claims
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SI200730180T SI2041328T1 (sl) | 2006-07-14 | 2007-07-13 | Aluminijeva zlitina in uporaba le-te za lite dele, posebno motornega vozila |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102006032699A DE102006032699B4 (de) | 2006-07-14 | 2006-07-14 | Aluminiumlegierung und deren Verwendung für ein Gussbauteil insbesondere eines Kraftwagens |
PCT/EP2007/057278 WO2008006908A1 (de) | 2006-07-14 | 2007-07-13 | Aluminiumlegierung und deren verwendung für ein gussbauteil insbesondere eines kraftwagens |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2041328A1 true EP2041328A1 (de) | 2009-04-01 |
EP2041328B1 EP2041328B1 (de) | 2010-01-27 |
Family
ID=38523382
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP07787546A Active EP2041328B1 (de) | 2006-07-14 | 2007-07-13 | Aluminiumlegierung und deren verwendung für ein gussbauteil insbesondere eines kraftwagens |
Country Status (9)
Country | Link |
---|---|
US (1) | US20090297393A1 (de) |
EP (1) | EP2041328B1 (de) |
JP (1) | JP2009543944A (de) |
AT (1) | ATE456682T1 (de) |
CA (1) | CA2657731A1 (de) |
DE (2) | DE102006032699B4 (de) |
ES (1) | ES2340218T3 (de) |
SI (1) | SI2041328T1 (de) |
WO (1) | WO2008006908A1 (de) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102010007531B4 (de) * | 2010-02-11 | 2014-11-27 | Audi Ag | Verfahren zum Herstellen eines Karosseriebauteils |
DE102010060670A1 (de) * | 2010-11-19 | 2012-05-24 | Martinrea Honsel Germany Gmbh | Zylinderkopf für Verbrennungsmotoren aus einer Aluminiumlegierung |
ES2507865T3 (es) * | 2010-12-28 | 2014-10-15 | Casa Maristas Azterlan | Método para obtener propiedades mecánicas mejoradas en moldeos de aluminio reciclado libres de fases beta con forma de plaqueta |
CZ2015521A3 (cs) * | 2015-07-28 | 2016-12-14 | Univerzita J. E. Purkyně V Ústí Nad Labem | Hliníková slitina, zejména pro výrobu odlitků segmentů forem pro lisování pneumatik, a způsob tepelného zpracování odlitků segmentů forem |
EP3334850A4 (de) * | 2015-08-13 | 2019-03-13 | Alcoa USA Corp. | Verbesserte 3xx-aluminium-gusslegierungen und verfahren zur herstellung davon |
US11198925B2 (en) | 2016-03-31 | 2021-12-14 | Rio Tinto Alcan International Limited | Aluminum alloys having improved tensile properties |
DE102018214739A1 (de) * | 2018-08-30 | 2020-03-05 | Magna BDW technologies GmbH | Hochfestes Gehäuse, sowie Verfahren zur Herstellung von hochfesten Guss-Gehäusen |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0791624B2 (ja) * | 1988-05-11 | 1995-10-04 | 本田技研工業株式会社 | アルミニウム合金鋳物品の製造方法 |
JPH058296A (ja) * | 1991-07-05 | 1993-01-19 | Sumitomo Electric Ind Ltd | 管のライニング更生工法 |
DE4304134C1 (de) * | 1993-02-11 | 1994-09-15 | Albert Handtmann Metallguswerk | Verfahren zur Herstellung von Gußteilen |
FR2721041B1 (fr) * | 1994-06-13 | 1997-10-10 | Pechiney Recherche | Tôle d'alliage aluminium-silicium destinée à la construction mécanique, aéronautique et spatiale. |
CH689143A5 (de) * | 1994-06-16 | 1998-10-30 | Rheinfelden Aluminium Gmbh | Aluminium-Silizium Druckgusslegierung mit hoher Korrosionsbestaendigkeit, insbesondere fuer Sicherheitsbauteile. |
EP0992601A1 (de) * | 1998-10-05 | 2000-04-12 | Alusuisse Technology & Management AG | Verfahren zur Herstellung eines Bauteiles aus einer Aluminiumlegierung durch Druckgiessen |
DE10002021C2 (de) * | 1999-09-24 | 2002-10-17 | Honsel Guss Gmbh | Verfahren zur Wärmebehandlung von Strukturgußteilen aus einer dafür zu verwendenden Aluminiumlegierung |
JP2002339030A (ja) * | 2001-05-17 | 2002-11-27 | Yamaha Motor Co Ltd | ダイカスト用アルミニウム合金 |
JP2003027169A (ja) * | 2001-07-19 | 2003-01-29 | Yamaha Motor Co Ltd | アルミニウム合金およびアルミニウム合金鋳物品 |
FR2841164B1 (fr) * | 2002-06-25 | 2004-07-30 | Pechiney Aluminium | Piece moulee en alliage d'alluminium a haute resistance au fluage |
DE502004009801D1 (de) * | 2003-01-23 | 2009-09-10 | Rheinfelden Aluminium Gmbh | Druckgusslegierung aus Aluminiumlegierung |
US7666353B2 (en) * | 2003-05-02 | 2010-02-23 | Brunswick Corp | Aluminum-silicon alloy having reduced microporosity |
US20050199318A1 (en) * | 2003-06-24 | 2005-09-15 | Doty Herbert W. | Castable aluminum alloy |
JP2005264301A (ja) * | 2004-03-22 | 2005-09-29 | Toyota Central Res & Dev Lab Inc | 鋳造アルミニウム合金とアルミニウム合金鋳物およびその製造方法 |
JP2005281829A (ja) * | 2004-03-30 | 2005-10-13 | Honda Motor Co Ltd | Al−Si系合金及びこの合金からなる合金部材 |
ES2368923T3 (es) * | 2004-06-29 | 2011-11-23 | Aluminium Rheinfelden Gmbh | Aleación de aluminio para la colada a presión. |
JP2006183122A (ja) * | 2004-12-28 | 2006-07-13 | Denso Corp | ダイカスト用アルミニウム合金およびアルミニウム合金鋳物の製造方法 |
-
2006
- 2006-07-14 DE DE102006032699A patent/DE102006032699B4/de not_active Withdrawn - After Issue
-
2007
- 2007-07-13 CA CA002657731A patent/CA2657731A1/en not_active Abandoned
- 2007-07-13 DE DE502007002755T patent/DE502007002755D1/de active Active
- 2007-07-13 AT AT07787546T patent/ATE456682T1/de active
- 2007-07-13 SI SI200730180T patent/SI2041328T1/sl unknown
- 2007-07-13 US US12/373,301 patent/US20090297393A1/en not_active Abandoned
- 2007-07-13 ES ES07787546T patent/ES2340218T3/es active Active
- 2007-07-13 JP JP2009518904A patent/JP2009543944A/ja active Pending
- 2007-07-13 WO PCT/EP2007/057278 patent/WO2008006908A1/de active Application Filing
- 2007-07-13 EP EP07787546A patent/EP2041328B1/de active Active
Non-Patent Citations (1)
Title |
---|
See references of WO2008006908A1 * |
Also Published As
Publication number | Publication date |
---|---|
ATE456682T1 (de) | 2010-02-15 |
SI2041328T1 (sl) | 2010-04-30 |
US20090297393A1 (en) | 2009-12-03 |
JP2009543944A (ja) | 2009-12-10 |
WO2008006908A1 (de) | 2008-01-17 |
CA2657731A1 (en) | 2008-01-17 |
DE102006032699A1 (de) | 2008-01-17 |
ES2340218T3 (es) | 2010-05-31 |
EP2041328B1 (de) | 2010-01-27 |
DE102006032699B4 (de) | 2010-09-09 |
DE502007002755D1 (de) | 2010-03-18 |
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