EP1612286B1 - Aluminium alloy for pressure die casting - Google Patents
Aluminium alloy for pressure die casting Download PDFInfo
- Publication number
- EP1612286B1 EP1612286B1 EP05405361A EP05405361A EP1612286B1 EP 1612286 B1 EP1612286 B1 EP 1612286B1 EP 05405361 A EP05405361 A EP 05405361A EP 05405361 A EP05405361 A EP 05405361A EP 1612286 B1 EP1612286 B1 EP 1612286B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- aluminium alloy
- ppm
- alloy according
- titanium
- aluminium
- 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
- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 18
- 238000004512 die casting Methods 0.000 title claims abstract description 17
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 27
- 239000000956 alloy Substances 0.000 claims abstract description 27
- 239000010936 titanium Substances 0.000 claims abstract description 13
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 11
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 11
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims abstract description 9
- 229910052796 boron Inorganic materials 0.000 claims abstract description 9
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 8
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims abstract description 7
- 229910052742 iron Inorganic materials 0.000 claims abstract description 6
- 229910052750 molybdenum Inorganic materials 0.000 claims abstract description 6
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 6
- 229910052712 strontium Inorganic materials 0.000 claims abstract description 6
- CIOAGBVUUVVLOB-UHFFFAOYSA-N strontium atom Chemical compound [Sr] CIOAGBVUUVVLOB-UHFFFAOYSA-N 0.000 claims abstract description 6
- 229910052726 zirconium Inorganic materials 0.000 claims abstract description 6
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims abstract description 5
- 239000011733 molybdenum Substances 0.000 claims abstract description 5
- 239000010703 silicon Substances 0.000 claims abstract description 5
- 229910005540 GaP Inorganic materials 0.000 claims abstract description 4
- GPXJNWSHGFTCBW-UHFFFAOYSA-N Indium phosphide Chemical compound [In]#P GPXJNWSHGFTCBW-UHFFFAOYSA-N 0.000 claims abstract description 4
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 claims abstract description 4
- HZXMRANICFIONG-UHFFFAOYSA-N gallium phosphide Chemical compound [Ga]#P HZXMRANICFIONG-UHFFFAOYSA-N 0.000 claims abstract description 4
- 239000011777 magnesium Substances 0.000 claims abstract description 4
- 229910052749 magnesium Inorganic materials 0.000 claims abstract description 4
- 239000011574 phosphorus Substances 0.000 claims abstract description 4
- 229910052698 phosphorus Inorganic materials 0.000 claims abstract description 4
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 claims abstract description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 3
- DGAQECJNVWCQMB-PUAWFVPOSA-M Ilexoside XXIX Chemical compound C[C@@H]1CC[C@@]2(CC[C@@]3(C(=CC[C@H]4[C@]3(CC[C@@H]5[C@@]4(CC[C@@H](C5(C)C)OS(=O)(=O)[O-])C)C)[C@@H]2[C@]1(C)O)C)C(=O)O[C@H]6[C@@H]([C@H]([C@@H]([C@H](O6)CO)O)O)O.[Na+] DGAQECJNVWCQMB-PUAWFVPOSA-M 0.000 claims abstract description 3
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims abstract description 3
- 239000011575 calcium Substances 0.000 claims abstract description 3
- 229910052791 calcium Inorganic materials 0.000 claims abstract description 3
- 229910052802 copper Inorganic materials 0.000 claims abstract description 3
- 239000010949 copper Substances 0.000 claims abstract description 3
- 229910052708 sodium Inorganic materials 0.000 claims abstract description 3
- 239000011734 sodium Substances 0.000 claims abstract description 3
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims abstract 4
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims abstract 2
- 239000011701 zinc Substances 0.000 claims abstract 2
- 229910052725 zinc Inorganic materials 0.000 claims abstract 2
- 238000004519 manufacturing process Methods 0.000 claims description 5
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims description 4
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims description 3
- 229910052748 manganese Inorganic materials 0.000 claims description 3
- 239000011572 manganese Substances 0.000 claims description 3
- 239000012535 impurity Substances 0.000 claims description 2
- 239000004411 aluminium Substances 0.000 claims 4
- 238000005266 casting Methods 0.000 abstract description 7
- 238000007670 refining Methods 0.000 abstract description 4
- 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 1
- 238000000137 annealing Methods 0.000 description 5
- 238000010438 heat treatment Methods 0.000 description 5
- 230000006399 behavior Effects 0.000 description 3
- 230000005496 eutectics Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000004140 cleaning Methods 0.000 description 2
- 238000011109 contamination Methods 0.000 description 2
- 230000018109 developmental process Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000010791 quenching Methods 0.000 description 2
- 230000000171 quenching effect Effects 0.000 description 2
- 229910000789 Aluminium-silicon alloy Inorganic materials 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 238000009749 continuous casting Methods 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000006735 deficit Effects 0.000 description 1
- 230000001934 delay Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000004634 feeding behavior Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 238000010422 painting Methods 0.000 description 1
- 238000010926 purge Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000002123 temporal effect Effects 0.000 description 1
- 238000003878 thermal aging Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/06—Making non-ferrous alloys with the use of special agents for refining or deoxidising
-
- 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 for die casting of components with high elongation in the cast state.
- the die casting technology has developed so far today that it is possible to produce components with high quality standards.
- the quality of a die-cast part depends not only on the machine setting and the chosen method, but also to a great extent on the chemical composition and microstructure of the aluminum alloy used. These two latter parameters are known to influence the castability, the feeding behavior ( G. Schindelbauer, J. Czikel “Shape Fillability and Volume Deficit of Common Die Casting Alloys", foundry research 42, 1990, p. 88/89 ), the mechanical properties and - especially important in diecasting - the lifespan of the Casting Tools (LA Norström, B. Klarenfjord, M. Svenson “General Aspect on Wash-out Mechanism in Aluminum Diecasting Dies", 17th International NADCA Diecasting Congress 1993, Cleveland OH ).
- the die-cast parts In order that the required mechanical properties, in particular a high elongation at break, can be achieved, the die-cast parts usually have to be subjected to a heat treatment.
- This heat treatment is necessary for the molding of the casting phases and thus for achieving a tough breaking behavior.
- a heat treatment usually means a solution annealing at temperatures just below the solidus temperature with subsequent quenching in water or another medium to temperatures ⁇ 100 ° C.
- the material thus treated now has a low yield strength and tensile strength.
- a thermal aging is then carried out. This can also be done by the process, e.g. by thermal application during painting or by stress-relief annealing of an entire group of components.
- die castings are cast close to the final dimensions, they usually have a complicated geometry with thin wall thicknesses.
- delays have to be expected, such as reworking, e.g. by directing the castings or, in the worst case, rejects.
- the solution annealing also causes additional costs and the economics of this production method could be significantly increased if alloys were available which meet the required properties without a heat treatment.
- AISi alloy with good mechanical values in the as-cast state is known from US Pat EP-A-0 687 742 known.
- EP-A-0 911 420 AlMg alloys which have a very high ductility in the cast state, but tend to have hot or cold cracks in the case of a complicated shape design and are therefore unsuitable.
- Another disadvantage of ductile die-cast alloys is their slow aging in the cast state, which causes a temporal change in the mechanical properties, including a loss of elongation. can result. This behavior is tolerated in many applications, since the property limits are not exceeded or fallen below, but is not tolerable in some applications and can only be turned off by a targeted heat treatment.
- the invention has for its object to provide a die casting suitable aluminum alloy, which is very easy to cast, has a high elongation in the cast state and no longer ages after casting.
- the alloy should be well weldable and crimpable, can be riveted and have a high corrosion resistance.
- the alloy composition according to the invention it is possible to achieve a high elongation in die-cast parts in the cast state with good values for the yield strength and the tensile strength, so that the alloy is particularly suitable for the production of safety components in the automotive industry.
- molybdenum it has been found that by adding molybdenum, the elongation can be increased again without loss of the other mechanical properties.
- the desired effect is achieved with an addition of 0.08 to 0.25 wt .-% Mo.
- the elongation can be even further improved.
- the preferred content is 0.10 to 0.18 wt% Zr.
- the relatively large proportion of eutectic silicon is refined by strontium. Compared to granular die-cast alloys with higher impurities, the alloy according to the invention also has advantages in terms of fatigue strength.
- the fracture toughness is higher due to the very small present mixed crystals and the refined eutectic.
- the strontium content is preferably between 50 and 150 ppm and should generally not fall below 50 ppm, since otherwise the casting behavior can be worsened. Instead of strontium, sodium and / or calcium may be added.
- the preferred silicon content is 8.0 to 10.0 wt% Si.
- the limitation of the magnesium content to 0.08 to 0.25 wt .-% Mg causes the eutectic structure is not significantly coarsened and the alloy has only a low curing potential, which contributes to a high elongation.
- the proportion of manganese prevents sticking in the mold and ensures good mold release.
- the manganese content gives the casting a high structural strength at elevated temperature, so that with demolding with very little to no distortion is expected.
- the iron content is preferably limited to max. Limited to 0.25 wt .-% Fe.
- the alloy according to the invention can be riveted in the cast state.
- the alloy according to the invention is preferably produced as a horizontal continuous casting ingot.
- a die-cast alloy with low oxide contamination can be melted without expensive melt cleaning: an important prerequisite for achieving high elongation values in the die-cast part.
- any contamination of the melt, in particular by copper or iron, must be avoided.
- the cleaning of the inventive time-finished AISi alloy is preferably carried out by means of a purge gas treatment with inert gases by means of an impeller.
- Grain refining is preferably carried out in the case of the alloy according to the invention.
- the alloy gallium phosphide and / or indium phosphide in an amount corresponding to 1 to 250 ppm, preferably 1 to 30 ppm of phosphorus can be supplied.
- the alloy for grain refining may also contain titanium and boron, the addition of titanium and boron via a master alloy with 1 to 2 wt .-% Ti and 1 to 2 wt .-% B, balance aluminum.
- the aluminum master alloy contains 1.3 to 1.8% by weight of Ti and 1.3 to 1.8% by weight of B, and has a Ti / B weight ratio of about 0.8 to 1.2.
- the content of the master alloy in the alloy of the present invention is preferably adjusted to 0.05 to 0.5% by weight.
- the aluminum alloy according to the invention is particularly suitable for the production of safety components in diecasting.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
- Moulds For Moulding Plastics Or The Like (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Body Structure For Vehicles (AREA)
- Mold Materials And Core Materials (AREA)
- Refinement Of Pig-Iron, Manufacture Of Cast Iron, And Steel Manufacture Other Than In Revolving Furnaces (AREA)
- Metal Extraction Processes (AREA)
- Manufacture Of Metal Powder And Suspensions Thereof (AREA)
Abstract
Description
Die Erfindung betrifft eine Aluminiumlegierung zum Druckgiessen von Bauteilen mit hoher Dehnung im Gusszustand.The invention relates to an aluminum alloy for die casting of components with high elongation in the cast state.
Die Druckgiesstechnik hat sich heute soweit entwickelt, dass es möglich ist, Bauteile mit hohen Qualitätsansprüchen herzustellen. Die Qualität eines Druckgussteils hängt aber nicht nur von der Maschineneinstellung und dem gewählten Verfahren ab, sondern in hohem Masse auch von der chemischen Zusammensetzung und der Gefügestruktur der verwendeten Aluminiumlegierung. Diese beiden letztgenannten Parameter beeinflussen bekanntermassen die Giessbarkeit, das Speisungsverhalten (
In der Vergangenheit wurde der Entwicklung von speziell für das Druckgiessen anspruchsvoller Bauteile geeigneten Aluminiumlegierungen einige Aufmerksamkeit geschenkt. Gerade von Konstrukteuren der Automobilindustrie wird immer mehr gefordert, z. B. schweissbare Bauteile mit hoher Duktilität im Druckguss zu realisieren, da bei hohen Stückzahlen das Druckgiessen die kostengünstigste Produktionsmethode darstellt.In the past, some attention has been paid to the development of aluminum alloys that are especially suitable for the die casting of demanding components. Especially by designers of the automotive industry is increasingly required, for. B. to realize weldable components with high ductility in die casting, since at high quantities die casting is the most cost-effective production method.
Durch die Weiterentwicklung der Druckgiesstechnik ist es heute möglich, schweissbare Bauteile von hoher Qualität herzustellen. Dies hat den Anwendungsbereich für Druckgussteile auf Komponenten im Chassis erweitert.
Der Duktilität kommt gerade bei kompliziert gestalteten Teilen immer mehr Bedeutung zu.Thanks to the further development of die casting technology, it is now possible to produce weldable components of high quality. This has expanded the scope of application for die castings to components in the chassis.
Ductility is becoming more and more important, especially for complicated parts to.
Damit die geforderten mechanischen Eigenschaften, insbesondere eine hohe Bruchdehnung, erreicht werden können, müssen die Druckgussteile üblicherweise einer Wärmebehandlung unterzogen werden. Diese Wärmebehandlung ist zur Einformung der Gussphasen und damit zur Erzielung eines zähen Bruchverhaltens notwendig. Eine Wärmebehandlung bedeutet in der Regel eine Lösungsglühung bei Temperaturen knapp unterhalb der Solidustemperatur mit nachfolgendem Abschrecken in Wasser oder einem anderen Medium auf Temperaturen <100°C. Der so behandelte Werkstoff weist nun eine geringe Dehngrenze und Zugfestigkeit auf. Um diese Eigenschaften auf den gewünschten Wert zu heben, wird anschliessend eine Warmauslagerung durchgeführt. Diese kann auch prozessbedingt erfolgen, z.B. durch eine thermische Beaufschlagung beim Lackieren oder durch das Entspannungsglühen einer ganzen Bauteilgruppe.In order that the required mechanical properties, in particular a high elongation at break, can be achieved, the die-cast parts usually have to be subjected to a heat treatment. This heat treatment is necessary for the molding of the casting phases and thus for achieving a tough breaking behavior. A heat treatment usually means a solution annealing at temperatures just below the solidus temperature with subsequent quenching in water or another medium to temperatures <100 ° C. The material thus treated now has a low yield strength and tensile strength. In order to raise these properties to the desired value, a thermal aging is then carried out. This can also be done by the process, e.g. by thermal application during painting or by stress-relief annealing of an entire group of components.
Da Druckgussteile endabmessungsnah gegossen werden, haben sie meist eine komplizierte Geometrie mit dünnen Wandstärken. Während des Lösungsglühens und besonders beim Abschreckprozess muss mit Verzug gerechnet werden, der eine Nacharbeit z.B. durch Richten der Gussteile oder im schlimmsten Fall Ausschuss nach sich ziehen kann. Die Lösungsglühung verursacht zudem zusätzliche Kosten und die Wirtschaftlichkeit dieser Produktionsmethode könnte wesentlich erhöht werden, wenn Legierungen zur Verfügung stehen würden, welche die geforderten Eigenschaften ohne eine Wärmebehandlung erfüllen.Because die castings are cast close to the final dimensions, they usually have a complicated geometry with thin wall thicknesses. During solution annealing, and especially during the quenching process, delays have to be expected, such as reworking, e.g. by directing the castings or, in the worst case, rejects. The solution annealing also causes additional costs and the economics of this production method could be significantly increased if alloys were available which meet the required properties without a heat treatment.
Eine AISi-Legierung mit guten mechanischen Werten im Gusszustand ist aus der
Aus
Der Erfindung liegt die Aufgabe zugrunde, eine zum Druckgiessen geeignete Aluminiumlegierung bereitzustellen, die sehr gut giessbar ist, im Gusszustand eine hohe Dehnung aufweist und nach dem Giessen nicht mehr altert. Darüber hinaus soll die Legierung gut schweissbar und bördelbar sein, genietet werden können und eine hohe Korrosionsbeständigkeit aufweisen.The invention has for its object to provide a die casting suitable aluminum alloy, which is very easy to cast, has a high elongation in the cast state and no longer ages after casting. In addition, the alloy should be well weldable and crimpable, can be riveted and have a high corrosion resistance.
Erfindungsgemäss wird die Aufgabe gelöst durch eine Aluminiumlegierung mit den Merkmalen des Anspruchs 1.According to the invention, the object is achieved by an aluminum alloy having the features of claim 1.
Mit der erfindungsgemässen Legierungszusammensetzung lässt sich bei Druckgussteilen im Gusszustand bei guten Werten für die Dehngrenze und die Zugfestigkeit eine hohe Dehnung erzielen, so dass die Legierung insbesondere zur Herstellung von Sicherheitsbauteilen im Automobilbau geeignet ist. Überraschenderweise hat sich gezeigt, dass durch eine Zugabe von Molybdän die Dehnung ohne Einbusse bei den anderen mechanischen Eigenschaften nochmals angehoben werden kann. Die gewünschte Wirkung wird mit einer Zugabe von 0,08 bis 0,25 Gew.-% Mo erreicht.With the alloy composition according to the invention, it is possible to achieve a high elongation in die-cast parts in the cast state with good values for the yield strength and the tensile strength, so that the alloy is particularly suitable for the production of safety components in the automotive industry. Surprisingly, it has been found that by adding molybdenum, the elongation can be increased again without loss of the other mechanical properties. The desired effect is achieved with an addition of 0.08 to 0.25 wt .-% Mo.
Mit einer kombinierten Zugabe von Molybdän und 0,05 bis 0,3 Gew.-% Zr kann die Dehnung sogar noch weiter verbessert werden. Der bevorzugte Gehalt liegt bei 0,10 bis 0,18 Gew.-% Zr.With a combined addition of molybdenum and 0.05 to 0.3 wt% Zr, the elongation can be even further improved. The preferred content is 0.10 to 0.18 wt% Zr.
Der relativ grosse Anteil eutektischen Siliziums wird durch Strontium veredelt. Gegenüber körnigen Druckgusslegierungen mit höheren Verunreinigungen besitzt die erfindungsgemässe Legierung auch Vorteile hinsichtlich der Dauerschwingfestigkeit. Die Risszähigkeit ist aufgrund der sehr klein vorliegenden Mischkristalle und des veredelten Eutektikums höher. Der Strontiumgehalt liegt bevorzugt zwischen 50 und 150 ppm und sollte im allgemeinen nicht unter 50 ppm fallen, da sonst das Giessverhalten verschlechtert werden kann. Anstelle von Strontium kann Natrium und/oder Calcium zugegeben werden.The relatively large proportion of eutectic silicon is refined by strontium. Compared to granular die-cast alloys with higher impurities, the alloy according to the invention also has advantages in terms of fatigue strength. The fracture toughness is higher due to the very small present mixed crystals and the refined eutectic. The strontium content is preferably between 50 and 150 ppm and should generally not fall below 50 ppm, since otherwise the casting behavior can be worsened. Instead of strontium, sodium and / or calcium may be added.
Der bevorzugte Siliziumgehalt beträgt 8,0 bis 10,0 Gew.-% Si.The preferred silicon content is 8.0 to 10.0 wt% Si.
Die Beschränkung des Magnesiumgehaltes auf 0,08 bis 0,25 Gew.-% Mg bewirkt, dass das eutektische Gefüge nicht nennenswert vergröbert wird und die Legierung nur ein geringes Aushärtungspotential hat, was zu einer hohen Dehnung beiträgt.The limitation of the magnesium content to 0.08 to 0.25 wt .-% Mg causes the eutectic structure is not significantly coarsened and the alloy has only a low curing potential, which contributes to a high elongation.
Durch den Anteil an Mangan wird das Kleben in der Form vermieden und eine gute Entformbarkeit gewährleistet. Der Mangangehalt gibt dem Gussteil eine hohe Gestaltfestigkeit bei erhöhter Temperatur, so dass beim Entformen mit sehr geringem bis gar keinem Verzug zu rechnen ist.
Der Eisengehalt wird vorzugsweise auf max. 0,25 Gew.-% Fe beschränkt.The proportion of manganese prevents sticking in the mold and ensures good mold release. The manganese content gives the casting a high structural strength at elevated temperature, so that with demolding with very little to no distortion is expected.
The iron content is preferably limited to max. Limited to 0.25 wt .-% Fe.
Die erfindungsgemässe Legierung lässt sich im Gusszustand nieten.The alloy according to the invention can be riveted in the cast state.
Mit einer Stabilisierungsglühung während 1 bis 2 h in einem Temperaturbereich von etwa 280 bis 320° C können sehr hohe Dehnungswerte erreicht werden.With a stabilization annealing for 1 to 2 h in a temperature range of about 280 to 320 ° C very high elongation values can be achieved.
Die erfindungsgemässe Legierung wird bevorzugt als Horizontal-Stranggussmassel hergestellt. Damit kann ohne aufwendige Schmelzereinigung eine Druckgusslegierung mit geringer Oxidverunreinigung erschmolzen werden: eine wichtige Voraussetzung zur Erzielung hoher Dehnungswerte im Druckgussteil.The alloy according to the invention is preferably produced as a horizontal continuous casting ingot. Thus, a die-cast alloy with low oxide contamination can be melted without expensive melt cleaning: an important prerequisite for achieving high elongation values in the die-cast part.
Beim Einschmelzen ist jede Verunreinigung der Schmelze, insbesondere durch Kupfer oder Eisen, zu vermeiden. Die Reinigung der erfindungsgemässen dauerveredelten AISi-Legierung erfolgt bevorzugt mittels einer Spülgasbehandlung mit inerten Gasen mittels Impeller.During melting, any contamination of the melt, in particular by copper or iron, must be avoided. The cleaning of the inventive time-finished AISi alloy is preferably carried out by means of a purge gas treatment with inert gases by means of an impeller.
Bevorzugt wird bei der erfindungsgemässen Legierung eine Kornfeinung durchgeführt. Hierzu kann der Legierung Galliumphosphid und/oder Indiumphosphid in einer Menge entsprechend 1 bis 250 ppm, vorzugsweise 1 bis 30 ppm Phosphor zugeführt werden. Alternativ oder zusätzlich kann die Legierung zur Kornfeinung auch Titan und Bor enthalten, wobei die Zugabe von Titan und Bor über eine Vorlegierung mit 1 bis 2 Gew.-% Ti und 1 bis 2 Gew.-% B, Rest Aluminium, erfolgt. Bevorzugt enthält die Aluminium-Vorlegierung 1,3 bis 1,8 Gew.-% Ti und 1,3 bis 1,8 Gew.-% B und weist ein Ti/B-Gewichtsverhältnis von etwa 0,8 bis 1,2 auf. Der Gehalt der Vorlegierung in der erfindungsgemässen Legierung wird bevorzugt auf 0,05 bis 0,5 Gew.-% eingestellt.Grain refining is preferably carried out in the case of the alloy according to the invention. For this purpose, the alloy gallium phosphide and / or indium phosphide in an amount corresponding to 1 to 250 ppm, preferably 1 to 30 ppm of phosphorus can be supplied. Alternatively or additionally, the alloy for grain refining may also contain titanium and boron, the addition of titanium and boron via a master alloy with 1 to 2 wt .-% Ti and 1 to 2 wt .-% B, balance aluminum. Preferably, the aluminum master alloy contains 1.3 to 1.8% by weight of Ti and 1.3 to 1.8% by weight of B, and has a Ti / B weight ratio of about 0.8 to 1.2. The content of the master alloy in the alloy of the present invention is preferably adjusted to 0.05 to 0.5% by weight.
Die erfindungsgemässe Aluminiumlegierung eignet sich insbesondere zur Herstellung von Sicherheitsbauteilen im Druckgiessverfahren.The aluminum alloy according to the invention is particularly suitable for the production of safety components in diecasting.
Claims (9)
- Aluminium alloy for diecasting of components with high elongation in the cast state with8.0 to 11.5 w.% silicon0.3 to 0.8 w.% manganese0.08 to 0,25 w.% magnesiummax 0.4 w.% ironmax 0.1 w.% coppermax 0.1 w.% zincmax 0.15 w.% titanium0.08 to 0.25 w.% molybdenumoptionally also0.05 to 0.3 w.% zirconium30 to 300 ppm strontium or 5 to 30 ppm sodium and/or 1 to 30 ppm calcium for permanent refinement,gallium phosphide and/or indium phosphide in a quantity corresponding to 1 to 250 ppm phosphorus for grain refinementtitanium and boron added by way of an aluminium master alloy with 1 to 2 w.% Ti and 1 to 2 w.% B for grain refinement,and as the remainder aluminium and unavoidable impurities.
- Aluminium alloy according to claim 1, characterised by 50 to 150 ppm strontium.
- Aluminium alloy according to claim 1 or 2, characterised by 8.0 to 10.0 w.% silicon.
- Aluminium alloy according to claim 1 to 3, characterised by max 0.25 w.% iron.
- Aluminium alloy according to claim 1 or 4, characterised by 0.10 to 0.18 w.% zirconium.
- Aluminium alloy according to any of claims 1 to 5, characterised by gallium phosphide and/or indium phosphide in a quantity corresponding to 1 to 30 ppm phosphorus.
- Aluminium alloy according to any of claims 1 to 6, characterised by an aluminium master alloy with 1.3 to 1.8 w.% titanium and 1.3 to 1.8 w.% boron and a titanium/boron weight ratio between 0.8 and 1.2.
- Aluminium alloy according to claim 7, characterised by 0.05 to 0.5 w.% aluminium master alloy.
- Use of an aluminium alloy according to any of claims 1 to 8 for diecasting of safety components in car manufacture.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SI200531356T SI1612286T1 (en) | 2004-06-29 | 2005-05-26 | Aluminium alloy for pressure die casting |
PL05405361T PL1612286T3 (en) | 2004-06-29 | 2005-05-26 | Aluminium alloy for pressure die casting |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH10912004 | 2004-06-29 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP1612286A2 EP1612286A2 (en) | 2006-01-04 |
EP1612286A3 EP1612286A3 (en) | 2007-05-30 |
EP1612286B1 true EP1612286B1 (en) | 2011-07-13 |
Family
ID=34974215
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP05405361A Active EP1612286B1 (en) | 2004-06-29 | 2005-05-26 | Aluminium alloy for pressure die casting |
Country Status (15)
Country | Link |
---|---|
US (1) | US7108042B2 (en) |
EP (1) | EP1612286B1 (en) |
JP (1) | JP2006016693A (en) |
KR (2) | KR101295458B1 (en) |
CN (1) | CN1737176A (en) |
AT (1) | ATE516379T1 (en) |
BR (1) | BRPI0502521B8 (en) |
CA (1) | CA2510545C (en) |
DK (1) | DK1612286T3 (en) |
ES (1) | ES2368923T3 (en) |
MX (1) | MXPA05006962A (en) |
NO (1) | NO339588B1 (en) |
PL (1) | PL1612286T3 (en) |
PT (1) | PT1612286E (en) |
SI (1) | SI1612286T1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3235917A1 (en) | 2016-04-19 | 2017-10-25 | Rheinfelden Alloys GmbH & Co. KG | Alloy for pressure die casting |
EP3235916A1 (en) | 2016-04-19 | 2017-10-25 | Rheinfelden Alloys GmbH & Co. KG | Cast alloy |
Families Citing this family (48)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102006032699B4 (en) * | 2006-07-14 | 2010-09-09 | Bdw Technologies Gmbh & Co. Kg | Aluminum alloy and its use for a cast component, in particular a motor vehicle |
DE102008029864B4 (en) * | 2008-06-24 | 2011-02-24 | Bdw Technologies Gmbh | Cast component and method for its manufacture |
CN101760676B (en) * | 2008-11-12 | 2013-04-03 | 郑东海 | Formulation of cast aluminum alloy wheel hub |
CN101935772B (en) * | 2010-09-26 | 2012-05-30 | 郑州大学 | Method for preparing aluminum titanium carbon rare earth refiner |
KR101273582B1 (en) * | 2010-10-19 | 2013-06-11 | 한국생산기술연구원 | Oxidation-Resistant Aluminum Alloy and Manufacturing method thereof |
DE102010055011A1 (en) * | 2010-12-17 | 2012-06-21 | Trimet Aluminium Ag | Readily castable ductile aluminum-silicon alloy comprises silicon, magnesium, manganese, copper, titanium, iron, molybdenum, zirconium, strontium, and aluminum and unavoidable impurities, and phosphorus for suppressing primary silicon phase |
KR101380935B1 (en) * | 2011-03-25 | 2014-04-07 | 주식회사 스틸앤리소시즈 | Aluminium alloy for die casting and aluminium sub-frame for vehicle |
US9038704B2 (en) | 2011-04-04 | 2015-05-26 | Emerson Climate Technologies, Inc. | Aluminum alloy compositions and methods for die-casting thereof |
AT511397B1 (en) * | 2011-05-03 | 2013-02-15 | Sag Motion Ag | METHOD OF REFINING AND PERMITTING MODIFICATION OF AIMGSI ALLOYS |
CN102296212B (en) * | 2011-09-13 | 2013-01-23 | 成都银河动力有限公司 | P-Fe alloy type modifier and method for applying P-Fe alloy type modifier in aluminum-silicon alloy melting |
DE102013002632B4 (en) * | 2012-02-16 | 2015-05-07 | Audi Ag | Aluminum-silicon diecasting alloy and method of making a die cast component |
EP2653579B1 (en) * | 2012-04-17 | 2014-10-15 | Georg Fischer Druckguss GmbH & Co. KG | Aluminium alloy |
US9771635B2 (en) * | 2012-07-10 | 2017-09-26 | GM Global Technology Operations LLC | Cast aluminum alloy for structural components |
EP2735621B1 (en) * | 2012-11-21 | 2015-08-12 | Georg Fischer Druckguss GmbH & Co. KG | Aluminium die casting alloy |
CN103898376A (en) * | 2012-12-31 | 2014-07-02 | 上海万泰汽车零部件有限公司 | Die-cast aluminum alloy for automobile engine |
CN103911528A (en) * | 2013-01-06 | 2014-07-09 | 德尔福技术有限公司 | High corrosion resistance aluminum alloy for die-casting process |
CN104561776B (en) * | 2013-10-23 | 2018-01-16 | 明安国际企业股份有限公司 | The stainless steel component alloy of glof club head |
KR101641170B1 (en) * | 2014-09-02 | 2016-07-20 | 삼성전자주식회사 | Aluminum alloy for diecasting and manufacturing method thereof |
CN104233014B (en) * | 2014-09-30 | 2016-08-24 | 南通迪瓦特节能风机有限公司 | A kind of axial compressor rotor sheet alloy material and preparation method thereof |
CN104498784A (en) * | 2014-12-25 | 2015-04-08 | 马鸿斌 | Novel aluminum-titanium alloy and preparation process thereof |
EP3121302B1 (en) * | 2015-04-15 | 2018-09-19 | Daiki Aluminium Industry Co., Ltd. | Aluminum alloy for die casting, and die-cast aluminum alloy using same |
DE102015007929A1 (en) | 2015-06-20 | 2016-12-22 | Daimler Ag | Cast aluminum alloy, method of manufacturing an aluminum cast alloy component and using an aluminum casting alloy |
CA2995250A1 (en) * | 2015-08-13 | 2017-02-16 | Alcoa Usa Corp. | Improved 3xx aluminum casting alloys, and methods for making the same |
DE102015015610A1 (en) * | 2015-12-03 | 2017-06-08 | Audi Ag | Aluminum-silicon diecasting alloy, method of making a die cast component of the alloy and body component with a die cast component |
CN105369082B (en) * | 2015-12-11 | 2017-11-03 | 天津爱田汽车部件有限公司 | A kind of pack alloy |
DE102016004216A1 (en) * | 2016-04-07 | 2016-09-29 | Daimler Ag | Aluminum alloy, in particular for a casting method, and method for producing a component from such an aluminum alloy |
CN106119624A (en) * | 2016-08-25 | 2016-11-16 | 马鸿斌 | A kind of high heat conduction aluminum alloy and preparation method thereof |
CN106367639A (en) * | 2016-10-09 | 2017-02-01 | 马鸿斌 | High-thermal-conductivity aluminum alloy and preparing method thereof |
CN106702225A (en) * | 2016-11-15 | 2017-05-24 | 马鸿斌 | High-thermal-conductivity aluminum alloy and preparation method thereof |
EP3342890B1 (en) | 2016-12-28 | 2019-05-29 | Befesa Aluminio, S.L. | Aluminium casting alloy |
EP3342888B1 (en) | 2016-12-28 | 2019-05-29 | Befesa Aluminio, S.L. | Aluminium casting alloy |
ES2753164T3 (en) | 2016-12-28 | 2020-04-07 | Befesa Aluminio S L | Aluminum alloy for casting |
CN106591643A (en) * | 2017-01-15 | 2017-04-26 | 丹阳荣嘉精密机械有限公司 | High mechanical property die-casting aluminum alloy and preparation method thereof |
CN106947892A (en) * | 2017-05-12 | 2017-07-14 | 南通江中光电有限公司 | A kind of high tough anticorrosion aluminium material and preparation method thereof |
KR102344357B1 (en) * | 2017-05-17 | 2021-12-27 | 엘에스전선 주식회사 | Aluminum alloy for cable's conductor |
CN107254609A (en) * | 2017-06-09 | 2017-10-17 | 太仓东旭精密机械有限公司 | A kind of Al-alloy parts |
KR102285860B1 (en) | 2019-07-19 | 2021-08-04 | 주식회사 에프티넷 | Aluminium casting alloy with high toughness and method of there |
MX2022004016A (en) * | 2019-10-01 | 2022-05-02 | Ahresty Corp | Aluminum alloy diecast, diecast unit and method for producing same. |
CN110629079A (en) * | 2019-10-25 | 2019-12-31 | 江苏铭利达科技有限公司 | Aluminum alloy material for new energy automobile |
CN110714148A (en) * | 2019-11-21 | 2020-01-21 | 珠海市润星泰电器有限公司 | High-performance semi-solid die-casting aluminum alloy and preparation method thereof |
CN113584359A (en) * | 2020-04-30 | 2021-11-02 | 华劲新材料研究院(广州)有限公司 | High-thermal-conductivity die-casting aluminum alloy material produced by using secondary aluminum and preparation method thereof |
JP7282054B2 (en) * | 2020-05-19 | 2023-05-26 | 堺アルミ株式会社 | Low thermal expansion aluminum alloy rolled material and its manufacturing method |
CN112708793B (en) * | 2020-12-17 | 2022-02-15 | 烟台路通精密科技股份有限公司 | Method for smelting cast aluminum-silicon alloy ingredients |
CN115821127A (en) * | 2022-08-10 | 2023-03-21 | 帅翼驰新材料集团有限公司 | High pressure cast aluminum alloys with improved performance after baking |
CN115287485A (en) * | 2022-08-10 | 2022-11-04 | 帅翼驰新材料集团有限公司 | Method for manufacturing high-pressure cast aluminum alloy with performance improved after baking |
CN115181878B (en) | 2022-09-14 | 2022-12-23 | 苏州慧金新材料科技有限公司 | Integrated die casting aluminum alloy for new energy automobile, and preparation method and application thereof |
CN115386771B (en) * | 2022-10-27 | 2023-01-06 | 广州致远新材料科技有限公司 | Aluminum alloy material and die casting method of barrier gate transmission structural member |
CN116024467A (en) * | 2023-02-03 | 2023-04-28 | 清华大学 | High-strength and high-toughness die-casting aluminum-silicon alloy and preparation method and application thereof |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB605282A (en) * | 1945-12-01 | 1948-07-20 | Nat Smelting Co | Improvements in or relating to aluminium silicon alloys |
JPS6047898B2 (en) * | 1981-12-11 | 1985-10-24 | 住友アルミニウム製錬株式会社 | Aluminum alloy for casting with excellent heat resistance |
JPS6070159A (en) * | 1983-09-26 | 1985-04-20 | Mitsui Alum Kogyo Kk | Heat resistant aluminum alloy for casting |
DE3724928A1 (en) * | 1987-07-28 | 1989-02-16 | Bayerische Motoren Werke Ag | MANUFACTURING METHOD FOR LIGHT METAL CASTING COMPONENTS, IN PARTICULAR LIGHT METAL CASTING WHEELS FOR PERSONAL VEHICLES |
CH684800A5 (en) * | 1991-10-23 | 1994-12-30 | Rheinfelden Aluminium Gmbh | A method for grain refining of aluminum cast alloys, in particular aluminum-silicon casting alloys. |
ZA938824B (en) * | 1992-12-07 | 1994-06-30 | Rheinfelden Aluminium Gmbh | Grain refiner for aluminium casting alloys, in particular aluminium-silicon casting alloys. |
CH689143A5 (en) * | 1994-06-16 | 1998-10-30 | Rheinfelden Aluminium Gmbh | Aluminum-silicon casting alloys with high corrosion resistance, particularly for safety components. |
JPH08267210A (en) * | 1995-01-19 | 1996-10-15 | Nippon Light Metal Co Ltd | Large sized integrated thin cast product, production thereof and metallic mold for casting |
DE19754959C2 (en) * | 1997-12-11 | 2001-05-17 | Porsche Ag | Wheel for a motor vehicle with hollow spokes |
EP0992601A1 (en) * | 1998-10-05 | 2000-04-12 | Alusuisse Technology & Management AG | Method for fabricating a component from an aluminium alloy by pressure die-casting |
FR2827305A1 (en) * | 2001-07-10 | 2003-01-17 | Pechiney Aluminium | Ductile aluminum alloy destined for casting under pressure of structural and security components for motor vehicles |
FR2833616B1 (en) * | 2001-12-17 | 2004-07-30 | Pechiney Aluminium | HIGH DUCTILITY AND RESILIENCE ALUMINUM ALLOY PRESSURE CAST PART |
JP4007488B2 (en) * | 2002-01-18 | 2007-11-14 | 日本軽金属株式会社 | Aluminum alloy for die casting, manufacturing method of die casting product and die casting product |
PT1443122E (en) * | 2003-01-23 | 2009-10-20 | Rheinfelden Aluminium Gmbh | Die cast aluminium alloy |
-
2005
- 2005-05-26 SI SI200531356T patent/SI1612286T1/en unknown
- 2005-05-26 ES ES05405361T patent/ES2368923T3/en active Active
- 2005-05-26 EP EP05405361A patent/EP1612286B1/en active Active
- 2005-05-26 PT PT05405361T patent/PT1612286E/en unknown
- 2005-05-26 AT AT05405361T patent/ATE516379T1/en active
- 2005-05-26 DK DK05405361.6T patent/DK1612286T3/en active
- 2005-05-26 PL PL05405361T patent/PL1612286T3/en unknown
- 2005-06-01 KR KR1020050046629A patent/KR101295458B1/en active IP Right Grant
- 2005-06-23 CA CA2510545A patent/CA2510545C/en active Active
- 2005-06-24 MX MXPA05006962A patent/MXPA05006962A/en active IP Right Grant
- 2005-06-28 US US11/170,051 patent/US7108042B2/en not_active Expired - Fee Related
- 2005-06-28 BR BRPI0502521A patent/BRPI0502521B8/en not_active IP Right Cessation
- 2005-06-28 NO NO20053158A patent/NO339588B1/en not_active IP Right Cessation
- 2005-06-29 JP JP2005190485A patent/JP2006016693A/en active Pending
- 2005-06-29 CN CNA2005100811483A patent/CN1737176A/en active Pending
-
2013
- 2013-02-20 KR KR20130018089A patent/KR101490581B1/en active IP Right Grant
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3235917A1 (en) | 2016-04-19 | 2017-10-25 | Rheinfelden Alloys GmbH & Co. KG | Alloy for pressure die casting |
EP3235916A1 (en) | 2016-04-19 | 2017-10-25 | Rheinfelden Alloys GmbH & Co. KG | Cast alloy |
WO2017182103A1 (en) | 2016-04-19 | 2017-10-26 | Rheinfelden Alloys Gmbh & Co. Kg | Cast alloy |
WO2017182102A1 (en) | 2016-04-19 | 2017-10-26 | Rheinfelden Alloys Gmbh & Co. Kg | Die casting alloy |
US11421305B2 (en) | 2016-04-19 | 2022-08-23 | Rheinfelden Alloys Gmbh & Co. Kg | Cast alloy |
Also Published As
Publication number | Publication date |
---|---|
US7108042B2 (en) | 2006-09-19 |
KR101295458B1 (en) | 2013-08-09 |
BRPI0502521A (en) | 2007-02-13 |
EP1612286A2 (en) | 2006-01-04 |
JP2006016693A (en) | 2006-01-19 |
CN1737176A (en) | 2006-02-22 |
NO339588B1 (en) | 2017-01-09 |
CA2510545A1 (en) | 2005-12-29 |
CA2510545C (en) | 2014-09-30 |
BRPI0502521B8 (en) | 2016-09-13 |
MXPA05006962A (en) | 2006-01-24 |
KR20060046361A (en) | 2006-05-17 |
SI1612286T1 (en) | 2011-10-28 |
KR101490581B1 (en) | 2015-02-05 |
US20060011321A1 (en) | 2006-01-19 |
ATE516379T1 (en) | 2011-07-15 |
BRPI0502521B1 (en) | 2015-08-11 |
PL1612286T3 (en) | 2011-12-30 |
KR20130023330A (en) | 2013-03-07 |
PT1612286E (en) | 2011-09-19 |
EP1612286A3 (en) | 2007-05-30 |
DK1612286T3 (en) | 2011-10-24 |
ES2368923T3 (en) | 2011-11-23 |
NO20053158L (en) | 2005-12-30 |
NO20053158D0 (en) | 2005-06-28 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1612286B1 (en) | Aluminium alloy for pressure die casting | |
EP1443122B1 (en) | Die cast aluminium alloy | |
DE10352932B4 (en) | Cast aluminum alloy | |
EP3365472B1 (en) | Aluminium alloy | |
EP2735621B1 (en) | Aluminium die casting alloy | |
EP1719820A2 (en) | Aluminium cast alloy | |
DE102006039684B4 (en) | Aluminum safety component | |
EP1896621B1 (en) | Aluminium alloy | |
EP2653579A1 (en) | Aluminium alloy | |
WO2017182102A1 (en) | Die casting alloy | |
DE202006006518U1 (en) | Aluminum casting alloy, useful in production of safety components, contains silicon | |
EP1118685A1 (en) | Aluminium cast alloy | |
EP1564308A1 (en) | Casting of an aluminium alloy | |
DE102017114162A1 (en) | HIGH STRENGTH AND HIGH CRYAN RESISTANT ALUMINUM ALLOY ALLOYS AND HPDC MOTOR BLOCKS | |
DE102009036056A1 (en) | Impact-resistant aluminum alloy suitable for thick-walled die castings, especially crank cases, has specified composition | |
EP0853133B1 (en) | Use of an aluminium alloy for pressure die casting | |
EP0911420B1 (en) | Aluminium casting alloy | |
DE60211830T2 (en) | Creep resistant magnesium alloys with good castability | |
DE60316679T2 (en) | Brake product, brake system and method for the production thereof | |
AT407533B (en) | ALUMINUM ALLOY | |
EP2088216B1 (en) | Aluminium alloy | |
EP0908527A1 (en) | Aluminium casting alloy | |
AT404844B (en) | Pressure-casting alloy | |
EP1118686B1 (en) | Aluminium cast alloy | |
DE102021106985A1 (en) | Process for the production of an Al-Mg-Si aluminum alloy with an increased titanium content |
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 |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU MC NL PL PT RO SE SI SK TR |
|
AX | Request for extension of the european patent |
Extension state: AL BA HR LV MK YU |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
AK | Designated contracting states |
Kind code of ref document: A3 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU MC NL PL PT RO SE SI SK TR |
|
AX | Request for extension of the european patent |
Extension state: AL BA HR LV MK YU |
|
17P | Request for examination filed |
Effective date: 20070714 |
|
AKX | Designation fees paid |
Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU MC NL PL PT RO SE SI SK TR |
|
AXX | Extension fees paid |
Extension state: HR Payment date: 20070714 Extension state: YU Payment date: 20070714 Extension state: BA Payment date: 20070714 |
|
17Q | First examination report despatched |
Effective date: 20080425 |
|
GRAJ | Information related to disapproval of communication of intention to grant by the applicant or resumption of examination proceedings by the epo deleted |
Free format text: ORIGINAL CODE: EPIDOSDIGR1 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
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 BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU MC NL PL PT RO SE SI SK TR |
|
AX | Request for extension of the european patent |
Extension state: BA HR YU |
|
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: GERMAN |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: NV Representative=s name: ISLER & PEDRAZZINI AG |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 502005011612 Country of ref document: DE Effective date: 20110908 |
|
REG | Reference to a national code |
Ref country code: PT Ref legal event code: SC4A Free format text: AVAILABILITY OF NATIONAL TRANSLATION Effective date: 20110913 |
|
REG | Reference to a national code |
Ref country code: DK Ref legal event code: T3 |
|
REG | Reference to a national code |
Ref country code: SE Ref legal event code: TRGR |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: T3 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2368923 Country of ref document: ES Kind code of ref document: T3 Effective date: 20111123 |
|
REG | Reference to a national code |
Ref country code: PL Ref legal event code: T3 |
|
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: 20111113 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: 20110713 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: 20110713 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FD4D |
|
REG | Reference to a national code |
Ref country code: HU Ref legal event code: AG4A Ref document number: E012186 Country of ref document: HU |
|
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: 20110713 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: 20111014 |
|
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: 20110713 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: 20110713 |
|
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: 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: 20110713 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: 20110713 |
|
26N | No opposition filed |
Effective date: 20120416 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 502005011612 Country of ref document: DE Effective date: 20120416 |
|
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: 20120531 |
|
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: 20111013 |
|
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: 20120526 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: PT Payment date: 20140523 Year of fee payment: 10 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DK Payment date: 20140521 Year of fee payment: 10 Ref country code: BE Payment date: 20140523 Year of fee payment: 10 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 11 |
|
REG | Reference to a national code |
Ref country code: PT Ref legal event code: MM4A Free format text: LAPSE DUE TO NON-PAYMENT OF FEES Effective date: 20151126 |
|
REG | Reference to a national code |
Ref country code: DK Ref legal event code: EBP Effective date: 20150531 |
|
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 NON-PAYMENT OF DUE FEES Effective date: 20151126 |
|
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 NON-PAYMENT OF DUE FEES Effective date: 20150531 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 12 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: HU Payment date: 20160519 Year of fee payment: 12 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 13 |
|
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 NON-PAYMENT OF DUE FEES Effective date: 20150531 |
|
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 NON-PAYMENT OF DUE FEES Effective date: 20170527 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 14 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: NL Payment date: 20220519 Year of fee payment: 18 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: SE Payment date: 20220519 Year of fee payment: 18 Ref country code: IT Payment date: 20220524 Year of fee payment: 18 Ref country code: GB Payment date: 20220519 Year of fee payment: 18 Ref country code: FR Payment date: 20220523 Year of fee payment: 18 Ref country code: DE Payment date: 20220519 Year of fee payment: 18 Ref country code: CZ Payment date: 20220524 Year of fee payment: 18 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: TR Payment date: 20220518 Year of fee payment: 18 Ref country code: SI Payment date: 20220516 Year of fee payment: 18 Ref country code: PL Payment date: 20220428 Year of fee payment: 18 Ref country code: CH Payment date: 20220519 Year of fee payment: 18 Ref country code: AT Payment date: 20220523 Year of fee payment: 18 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: ES Payment date: 20220725 Year of fee payment: 18 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 502005011612 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: SE Ref legal event code: EUG |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: MM Effective date: 20230601 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MM01 Ref document number: 516379 Country of ref document: AT Kind code of ref document: T Effective date: 20230526 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20230526 |
|
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 NON-PAYMENT OF DUE FEES Effective date: 20230527 Ref country code: SE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230527 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230531 Ref country code: CZ Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230526 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230531 Ref country code: AT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230526 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230601 |
|
REG | Reference to a national code |
Ref country code: SI Ref legal event code: KO00 Effective date: 20240222 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230526 Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20231201 Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230526 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230531 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FD2A Effective date: 20240701 |
|
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 NON-PAYMENT OF DUE FEES Effective date: 20230527 |
|
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 NON-PAYMENT OF DUE FEES Effective date: 20230527 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PL Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230526 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PL Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20230526 |