EP1074636A1 - Aluminium alloy - Google Patents
Aluminium alloy Download PDFInfo
- Publication number
- EP1074636A1 EP1074636A1 EP00116579A EP00116579A EP1074636A1 EP 1074636 A1 EP1074636 A1 EP 1074636A1 EP 00116579 A EP00116579 A EP 00116579A EP 00116579 A EP00116579 A EP 00116579A EP 1074636 A1 EP1074636 A1 EP 1074636A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- alloy
- aluminum
- aluminum alloy
- content
- proportions
- 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
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
Definitions
- the invention relates to an aluminum alloy Manufacture of heat shields with one Alloy content of aluminum greater than 97%.
- Al 99.5 has the following alloy proportions in addition to aluminum within the specified limits: Alloy component Value-to silicon 0.25% copper 0.05% magnesium 0.05% zinc 0.07% manganese 0.05% titanium 0.05% Other 0.03%
- Al 99.5 is advantageous from the point of view of high heat shielding and high formability, but at the same time is problematic from various other aspects.
- Al 99.5 has a low strength. When using heat shields in motor vehicle construction, however, considerable demands are placed on the strength, which result, for example, from the effects of the wind or spray water at high speeds and the impact of stone chips.
- the low strength of Al 99.5 means that sheet metal parts with a greater thickness have to be used to ensure the required strength, which on the one hand increases the costs and on the other hand increases the weight of the heat shielding plate.
- Al 99.5 has good deep-drawing properties due to the high elongation values.
- the yield strength is, however, low at around 30 N / mm 2 .
- the low proof stress of Al 99.5 limits the possibilities during the forming process in the manufacture of heat shielding plates.
- the dynamic load pick-ups are made of Al 99.5 manufactured heat shields due to the strong Coarse grain formation insufficient.
- the structural Reasons to use knobbed sheets, which is desirable per se is in connection with the use of Al 99.5 problematic, since dimensional stability is not guaranteed can be. This ensures this dimensional stability impaired that with knobbed sheets on the formed Knob areas with increased coarse grain formation must be expected after a heat load.
- the invention is based on the object To provide aluminum alloy that a further improved formability compared to Al 99.5, improved strength, higher thermal Stability and less tendency to form coarse grains having.
- the sum of the Alloy proportions of at most two Main alloy components exceeds at least a factor of 5.
- the Overweight according to the invention of at most two for Al 99.5 main alloy components permitted according to DIN compared to the permissible according to DIN for Al 99.5 Remaining alloy components ensures that the aluminum alloy according to the invention clearly has a more homogeneous structure, resulting in strength and the stretchability is improved and at the same time the Tendency to coarse grain formation is reduced. At the same time the elasticity remains at least at the same level.
- Aluminum alloy will double the Yield point while increasing strength guaranteed by up to 50% that the sum of the Alloy proportions of the skin care components Sum of the alloy proportions of the remaining alloy components by at least a factor of 10.
- An optimization of the yield strength and the strength is in an aluminum alloy according to the invention ensures that the alloy content of manganese is between 0.35% and 0.45%.
- An aluminum alloy according to the invention in iron the only main alloy component is one improved yield strength and strength compared to Al 99.5 with improved stretchability.
- an inventive Aluminum alloy is used both in the event that iron and manganese form the main alloy components as well in the event that iron is the only one Main alloy component forms, thereby ensuring that the alloy content of iron between 1.25% and 1.35%.
- the alloy portion of aluminum is at least 98%.
- the alloy content of silicon is not 0.2% exceeds, it is ensured that the desired Increase in the yield strength and strength at least constant extensibility and reduced Coarse grain formation is achieved. Is for the same reasons it is advantageous if the alloy content of magnesium 0.003% and / or the alloy content of zinc 0.03 not exceeds.
- An elongation limit improved to approximately 100 N / mm 2 is guaranteed with an aluminum alloy with proportions of the alloy components also approved according to DIN for Al 99.5 within the following limits: Alloy component Value of Value-to silicon 0.05% 0.1% copper 0.0% 0.05% magnesium 0.0% 0.003% zinc 0.0% 0.03% boron 0.0% 0.002% sodium 0.0% 0.001% lithium 0.0% 0.0002% iron 1.25% 1.35% manganese 0.35% 0.45% chrome 0.0% 0.02% titanium 0.0% 0.03% beryllium 0.0% 0.0% calcium 0.0% 0.001%
- the alloy proportions for a first exemplary embodiment of an aluminum alloy according to the invention are now given below, which have an elastic limit of approximately 110 N / mm 2 , a breaking strength of 124 N / mm 2 and an elongation of approximately 45%.
- the alloy proportions for such an aluminum alloy are as follows: Proportion of alloy Alloy component silicon 0.063% copper 0.005% magnesium 0.0016% zinc 0.0036% boron 0.001% sodium ⁇ 0.001% iron 1.34% manganese 0.37% chrome 0.0014% titanium 0.019%
- the alloy proportions for a second exemplary embodiment of an aluminum alloy according to the invention are now given below, which have a yield strength of approximately 66 N / mm 2 , a strength of approximately 108 N / mm 2 and an extensibility of approximately 52%.
- the alloying proportions for such an aluminum alloy are as follows: Proportion of alloy Alloy component silicon 0.08% copper 0.004% magnesium 0.0021% zinc 0.0044% boron 0.001% sodium ⁇ 0.001% iron 1.3% manganese 0.014% chrome 0.0012% titanium 0.02%
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Body Structure For Vehicles (AREA)
- Laminated Bodies (AREA)
- Reinforced Plastic Materials (AREA)
- Building Environments (AREA)
- Cookers (AREA)
- Shielding Devices Or Components To Electric Or Magnetic Fields (AREA)
Abstract
Description
Die Erfindung betrifft eine Aluminiumlegierung zur Herstellung von Wärmeabschirmblechen mit einem Legierungsanteil von Aluminium größer als 97%.The invention relates to an aluminum alloy Manufacture of heat shields with one Alloy content of aluminum greater than 97%.
Aufgrund der für eine Wärmeabschirmung besonders vorteilhaften physikalischen Eigenschaften von Aluminium - hoher Reflektionsgrad im Infrarot-Bereich und sehr gute Wärmeleitfähigkeit - haben sich Aluminiumlegierungen als Werkstoff zur Herstellung von Wärmeabschirmblechen als Standardlösung durchgesetzt. Um die genannten physikalischen Eigenschaften des Aluminium umfangreich zu nutzen und den hohen Anforderungen an die Umformbarkeit des Werkstoffes bei der Herstellung von Wärmeabschirmblechen gerecht zu werden, werden zur Zeit etwa 80% der Wärmeabschirmbleche in Al 99,5 (AA1050) gefertigt. Eine hinreichend gute Umformbarkeit dieses Werkstoffs durch Tiefziehen ist gewährleistet, da die Dehnung (A5) von Al 99,5 bei etwa 45% liegt.Because of the special for a heat shield advantageous physical properties of aluminum - high degree of reflection in the infrared range and very good Thermal conductivity - have become aluminum alloys Material for the production of heat shielding sheets as Standard solution enforced. To the above physical properties of aluminum use and the high demands on formability of the material in the manufacture of Heat shields are currently being used about 80% of the heat shielding plates in Al 99.5 (AA1050) manufactured. A sufficiently good formability of this Material by deep drawing is guaranteed because the Elongation (A5) of Al 99.5 is about 45%.
Nach DIN weist Al 99,5 neben Aluminium folgende
Legierungsanteile in den angegebenen Grenzen auf:
Die Verwendung von Al 99,5 ist zwar unter den Gesichtspunkten hohe Wärmeabschirmung und hohe Umformbarkeit vorteilhaft, gleichzeitig jedoch unter verschiedenen anderen Aspekten problematisch. Zum einen weist Al 99,5 eine geringe Festigkeit auf. Beim Einsatz von Wärmeabschirmblechen im Kraftfahrzeugbau werden jedoch erhebliche Anforderungen an die Festigkeit gestellt, die sich beispielsweise aus den Einwirkungen des Fahrtwindes oder von Spritzwasser bei hohen Geschwindigkeiten sowie der Einwirkung von Steinschlag ergeben. Die geringe Festigkeit von Al 99,5 führt dazu, daß zur Gewährleistung der erforderlichen Festigkeit Blechformteile mit größerer Dicke eingesetzt werden müssen, was einerseits die Kosten erhöht und andererseits das Gewicht des Wärmeabschirmbleches vergrößert. Die geringe thermische Stabilität von Al 99,5 - Kriechen setzt bereits bei Temperaturen von über 150 °C ein - führt zu einer im Einsatz geringen Formstabilität, die jedoch zur Einhaltung der Abstände des Wärmeabschirmbleches gegenüber beispielsweise einem Katalysator und einem Fahrzeugunterboden zur Gewährleistung der erwünschten Wärmeabschirmung notwendig ist. Al 99,5 weist aufgrund der hohen Dehnungswerte, wie bereits erwähnt eine gute Tiefziehbarkeit auf. Die Dehngrenze ist mit etwa 30 N/mm2 jedoch gering. Die geringe Dehngrenze von Al 99,5 begrenzt die Möglichkeiten während des Umformprozesses bei der Herstellung von Wärmeabschirmblechen.The use of Al 99.5 is advantageous from the point of view of high heat shielding and high formability, but at the same time is problematic from various other aspects. On the one hand, Al 99.5 has a low strength. When using heat shields in motor vehicle construction, however, considerable demands are placed on the strength, which result, for example, from the effects of the wind or spray water at high speeds and the impact of stone chips. The low strength of Al 99.5 means that sheet metal parts with a greater thickness have to be used to ensure the required strength, which on the one hand increases the costs and on the other hand increases the weight of the heat shielding plate. The low thermal stability of Al 99.5 - creep already starts at temperatures of over 150 ° C - leads to a low dimensional stability in use, which however means that the distances between the heat shielding plate and that of a catalytic converter and a vehicle underbody, for example, to ensure the desired heat shielding are maintained necessary is. As already mentioned, Al 99.5 has good deep-drawing properties due to the high elongation values. The yield strength is, however, low at around 30 N / mm 2 . The low proof stress of Al 99.5 limits the possibilities during the forming process in the manufacture of heat shielding plates.
Ein weiteres Problem insbesondere im Dauereinsatz von Wärmeabschirmblechen besteht darin, daß Al 99,5 eine hohe Neigung zur Grobkornbildung insbesondere nach geringen Kaltumformungen aufweist. Diese Grobkornbildung, insbesondere bei der zwangsläufigen thermischen Belastung von Wärmeabschirmblechen, führt dazu, daß speziell in Radien die Gefahr einer Rißentstehung beispielsweise in Befestigungspunkten des Wärmeabschirmbleches besteht. Another problem, especially in the continuous use of Heat shielding is that Al 99.5 is high Tendency to coarse grain formation, especially after small Cold forming has. This coarse grain formation, especially with the inevitable thermal load of heat shields, leads to the fact that especially in Radii the risk of cracking, for example in Fastening points of the heat shield plate.
Auch sind die dynamischen Lastaufnahmen von aus Al 99,5 gefertigten Wärmeabschirmblechen aufgrund der starken Grobkornbildung unzureichend. Die aus strukturellen Gründen an sich erwünschte Verwendung von Noppenblechen ist in Verbindung mit dem Einsatz von Al 99,5 problematisch, da eine Formstabilität nicht gewährleistet werden kann. Diese Formstabilität wird dadurch beeinträchtigt, daß bei Noppenblechen an den umgeformten Noppenbereichen mit einer verstärkten Grobkornbildung nach einer Wärmebelastung gerechnet werden muß.The dynamic load pick-ups are made of Al 99.5 manufactured heat shields due to the strong Coarse grain formation insufficient. The structural Reasons to use knobbed sheets, which is desirable per se is in connection with the use of Al 99.5 problematic, since dimensional stability is not guaranteed can be. This ensures this dimensional stability impaired that with knobbed sheets on the formed Knob areas with increased coarse grain formation must be expected after a heat load.
Ausgehend von dem zuvor beschriebenen Stand der Technik liegt der Erfindung die Aufgabe zugrunde, eine Aluminiumlegierung zur Verfügung zu stellen, die gegenüber Al 99,5 eine weiter verbesserte Umformbarkeit, eine verbesserte Festigkeit, eine höhere thermische Stabilität und eine geringere Neigung zur Grobkornbildung aufweist.Starting from the prior art described above the invention is based on the object To provide aluminum alloy that a further improved formability compared to Al 99.5, improved strength, higher thermal Stability and less tendency to form coarse grains having.
Erfindungsgemäß ist die zuvor hergeleitete und aufgezeigte Aufgabe dadurch gelöst, daß die Summe der Legierungsanteile von höchstens zwei Hauptlegierungskomponenten die Summe der Legierungsanteile der Restlegierungskomponenten um mindestens den Faktor 5 übersteigt. Durch die erfindungsgemäße Übergewichtung von höchstens zwei für Al 99,5 nach DIN zulässigen Hauptlegierungskomponenten gegenüber den nach DIN für Al 99,5 zulässigen Restlegierungskomponenten ist gewährleistet, daß die erfindungsgemäße Aluminiumlegierung ein deutlich homogeneres Gefüge aufweist, wodurch die Festigkeit und die Streckziehbarkeit verbessert ist und gleichzeitig die Neigung zur Grobkornbildung reduziert ist. Gleichzeitig bleibt die Dehnbarkeit zumindest auf gleichem Niveau. According to the previously derived and The stated problem is solved in that the sum of the Alloy proportions of at most two Main alloy components the sum of the Alloy proportions of the remaining alloy components exceeds at least a factor of 5. Through the Overweight according to the invention of at most two for Al 99.5 main alloy components permitted according to DIN compared to the permissible according to DIN for Al 99.5 Remaining alloy components ensures that the aluminum alloy according to the invention clearly has a more homogeneous structure, resulting in strength and the stretchability is improved and at the same time the Tendency to coarse grain formation is reduced. At the same time the elasticity remains at least at the same level.
Gemäß einer ersten Ausgestaltung der erfindungsgemäßen Aluminium-Legierung wird eine Verdoppelung der Streckgrenze bei gleichzeitiger Erhöhung der Festigkeit um bis zu 50% dadurch gewährleistet, daß die Summe der Legierungsanteile der Hautplegierungskomponenten die Summe der Legierungsanteile der Restlegierungskomponenten um mindestens den Faktor 10 übersteigt.According to a first embodiment of the invention Aluminum alloy will double the Yield point while increasing strength guaranteed by up to 50% that the sum of the Alloy proportions of the skin care components Sum of the alloy proportions of the remaining alloy components by at least a factor of 10.
Eine Aluminiumlegierung mit besonders hoher Streckgrenze und guter Festigkeit bei gegenüber Al 99,5 gleichbleibender Dehnung ist dadurch gewährleistet, daß Eisen und Mangan die Hautplegierungskomponenten bilden.An aluminum alloy with a particularly high yield strength and good strength compared to Al 99.5 constant stretching is ensured by the fact that Iron and manganese form the skin care components.
Eine Optimierung der Streckgrenze und der Festigkeit ist bei einer erfindungsgemäßen Aluminiumlegierung dadurch gewährleistet, daß der Legierungsanteil von Mangan zwischen 0,35% und 0,45% liegt.An optimization of the yield strength and the strength is in an aluminum alloy according to the invention ensures that the alloy content of manganese is between 0.35% and 0.45%.
Eine erfindungsgemäße Aluminiumlegierung bei der Eisen die einzige Hauptlegierungskomponente bildet, weist eine gegenüber Al 99,5 verbesserte Streckgrenze und Festigkeit bei gleichzeitig verbesserter Dehnbarkeit auf.An aluminum alloy according to the invention in iron the only main alloy component is one improved yield strength and strength compared to Al 99.5 with improved stretchability.
Die Eigenschaften einer erfindungsgemäßen Aluminiumlegierung werden sowohl für den Fall, daß Eisen und Mangan die Hauptlegierungskomponenten bilden als auch für den Fall, daß Eisen die einzige Hauptlegierungskomponente bildet, dadurch gewährleistet, daß der Legierungsanteil von Eisen zwischen 1,25% und 1,35% liegt.The properties of an inventive Aluminum alloy are used both in the event that iron and manganese form the main alloy components as well in the event that iron is the only one Main alloy component forms, thereby ensuring that the alloy content of iron between 1.25% and 1.35%.
Um die für Wärmeabschirmbleche vorteilhaften physikalischen Eigenschaften des Aluminiums möglichst umfangreich zu nutzen, ist es vorteilhaft, daß bei einer erfindungsgemäßen Aluminiumlegierung der Legierungsanteil von Aluminium mindestens 98% beträgt.To the advantageous for heat shields physical properties of aluminum as possible extensive use, it is advantageous that at a aluminum alloy according to the invention the alloy portion of aluminum is at least 98%.
Dadurch, daß der Legierungsanteil von Silizium 0,2% nicht übersteigt, ist gewährleistet, daß die erwünschte Erhöhung der Streckgrenze und der Festigkeit bei zumindest gleichbleibender Dehnbarkeit und reduzierter Grobkornbildung erreicht wird. Aus denselben Gründen ist es vorteilhaft, wenn der Legierungsanteil von Magnesium 0,003% und/oder der Legierungsanteil von Zink 0,03 nicht übersteigt.Because the alloy content of silicon is not 0.2% exceeds, it is ensured that the desired Increase in the yield strength and strength at least constant extensibility and reduced Coarse grain formation is achieved. Is for the same reasons it is advantageous if the alloy content of magnesium 0.003% and / or the alloy content of zinc 0.03 not exceeds.
Die nach DIN für Al 99,5 ebenfalls zulässigen Legierungsanteile Chrom und Titan beeinträchtigen die erwünschten Eigenschaften der erfindungsgemäßen Aluminiumlegierung auch oberhalb der nach DIN vorgegebenen Legierungsanteile zunächst nicht. Zur Gewährleistung der erwünschten Eigenschaften der erfindungsgemäßen Aluminiumlegierung ist es jedoch vorteilhaft, wenn der Legierungsanteil von Titan 0,03% und/oder der Legierungsanteil von Chrom 0,02% nicht übersteigt.The also permissible according to DIN for Al 99.5 Alloy proportions of chrome and titanium affect the desired properties of the invention Aluminum alloy also above that according to DIN given alloy proportions initially. For Ensuring the desired properties of the aluminum alloy according to the invention, however advantageous if the titanium alloy content is 0.03% and / or the alloy content of chromium is not 0.02% exceeds.
Die Legierungsanteile der weiteren nach DIN zulässigen Legierungskomponenten Kupfer, Natrium und Kalzium beeinträchtigen in den nach DIN zulässigen Legierungsanteilen die erfindungsgemäß gewährleisteten Eigenschaften nur geringfügig.The alloy proportions of the other permitted according to DIN Alloy components copper, sodium and calcium impair in the permissible according to DIN Alloy proportions guaranteed according to the invention Properties only marginally.
Es gibt nun eine Vielzahl von Möglichkeiten, die erfindungsgemäße Aluminiumlegierung zur Herstellung von Wärmeabschirmblechen auszugestalten und weiterzubilden. Hierzu wird beispielsweise einerseits verwiesen auf die dem Patentanspruch 1 nachgeordneten Patentansprüche andererseits auf die folgende Beschreibung von vorteilhaften Legierungszusammensetzungen:There are now a variety of ways that Aluminum alloy according to the invention for the production of To design and develop heat shielding plates. On the one hand, reference is made to the the subordinate claims on the other hand to the following description of advantageous alloy compositions:
Eine etwa auf 100 N/mm2 verbesserte Dehngrenze ist mit
einer Aluminiumlegierung mit Anteilen von den auch nach
DIN für Al 99,5 zugelassenen Legierungskomponenten
innerhalb der folgenden Grenzen gewährleistet:
Innerhalb der vorgegebenen Grenzen können die Legierungsanteile zur Einstellung verschiedener Eigenschaften der Aluminiumlegierung gezielt variiert werden.Within the specified limits Alloy proportions for setting different Properties of the aluminum alloy varied specifically become.
Im folgenden werden nun die Legierungsanteile für ein
erstes Ausführungsbeispiel einer erfindungsgemäßen
Aluminiumlegierung angegeben, die eine Dehngrenze von
etwa 110 N/mm2, eine Bruchfestigkeit von 124 N/mm2 und
eine Dehnung von etwa 45% aufweist. Die Legierungsanteile
für eine derartige Aluminiumlegierung lauten wie folgt:
Im folgenden werden nun die Legierungsanteile für ein
zweites Ausführungsbeispiel einer erfindungsgemäßen
Aluminiumlegierung angegeben, die eine Streckgrenze von
etwa 66 N/mm2, eine Festigkeit von etwa 108 N/mm2 und
eine Dehnbarkeit von etwa 52% aufweist. Die
Legierunsganteile für eine derartige Aluminiumlegierung
lauten wie folgt:
Claims (12)
dadurch gekennzeichnet, daß die Summe der Legierungsanteile von höchstens 2 Hauptlegierungskomponenten die Summe der Legierungsanteile der Restlegierungskomponenten um mindestens den Faktor 5 übersteigt.Aluminum alloy for the production of heat shielding plates with an alloy content of aluminum greater than 97%,
characterized in that the sum of the alloy proportions of at most 2 main alloy components exceeds the sum of the alloy proportions of the remaining alloy components by at least a factor of 5.
dadurch gekennzeichnet, daß die Summe der Legierungsanteile der Hauptlegierungskomponenten die Summe der Legierungsanteile der Restlegierungskomponenten um mindestens den Faktor 10 übersteigt.Aluminum alloy according to claim 1,
characterized in that the sum of the alloy fractions of the main alloy components exceeds the sum of the alloy fractions of the remaining alloy components by at least a factor of 10.
dadurch gekennzeichnet, daß Eisen und Mangan die Hauptlegierungskomponenten bilden.Aluminum alloy according to claim 1 or 2,
characterized in that iron and manganese form the main alloy components.
dadurch gekennzeichnet, daß der Legierungsanteil von Mangan zwischen 0,35% und 0,45% liegt.Aluminum alloy according to claim 3,
characterized in that the alloy content of manganese is between 0.35% and 0.45%.
dadurch gekennzeichnet, daß Eisen die einzige Hauptlegierungskomponente bildet. Aluminum alloy according to claim 1 or 2,
characterized in that iron is the only main alloy component.
dadurch gekennzeichnet, daß der Legierungsanteil von Eisen zwischen 1,25% und 1,35% liegt.Aluminum alloy according to one of claims 3 to 5,
characterized in that the alloy content of iron is between 1.25% and 1.35%.
dadurch gekennzeichnet, daß der Legierungsanteil von Aluminium mindestens 98% beträgt.Aluminum alloy according to one of claims 1 to 6,
characterized in that the alloy content of aluminum is at least 98%.
dadurch gekennzeichnet, daß der Legierungsanteil von Silizium 0,2% nicht übersteigt.Aluminum alloy according to one of claims 1 to 7,
characterized in that the alloy content of silicon does not exceed 0.2%.
dadurch gekennzeichnet, daß der Legierungsanteil von Magnesium 0,003% nicht übersteigt.Aluminum alloy according to one of claims 1 to 8,
characterized in that the magnesium alloy content does not exceed 0.003%.
dadurch gekennzeichnet, daß der Legierungsanteil von Zink 0,03% nicht übersteigt.Aluminum alloy according to one of claims 1 to 9,
characterized in that the zinc alloy content does not exceed 0.03%.
dadurch gekennzeichnet, daß der Legierungsanteil von Titan 0,03% nicht übersteigt.Aluminum alloy according to one of claims 1 to 10,
characterized in that the titanium alloy content does not exceed 0.03%.
dadurch gekennzeichnet, daß der Legierungsanteil von Chrom 0,02% nicht übersteigt.Aluminum alloy according to one of claims 1 to 11,
characterized in that the alloy content of chromium does not exceed 0.02%.
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19936234 | 1999-08-05 | ||
| DE19936234 | 1999-08-05 | ||
| DE19948820 | 1999-10-09 | ||
| DE19948820A DE19948820B4 (en) | 1999-08-05 | 1999-10-09 | Heat shield made of an aluminum alloy |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP1074636A1 true EP1074636A1 (en) | 2001-02-07 |
| EP1074636B1 EP1074636B1 (en) | 2005-03-23 |
Family
ID=26054452
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP00116579A Expired - Lifetime EP1074636B1 (en) | 1999-08-05 | 2000-08-01 | Use of aluminum alloy sheet for heat shielding |
Country Status (6)
| Country | Link |
|---|---|
| EP (1) | EP1074636B1 (en) |
| AT (1) | ATE291646T1 (en) |
| CZ (1) | CZ296688B6 (en) |
| DE (1) | DE29923957U1 (en) |
| ES (1) | ES2238955T3 (en) |
| PT (1) | PT1074636E (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101469386B (en) * | 2007-04-12 | 2011-01-26 | 日本轻金属株式会社 | Aluminum alloy sheet for battery cover and its production method |
| WO2016005484A1 (en) * | 2014-07-09 | 2016-01-14 | Hydro Aluminium Rolled Products Gmbh | Use of an aluminium alloy or of an aluminium sheet product made from an alloy of this type for an aluminium-plastic composite part |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4483719A (en) * | 1983-08-23 | 1984-11-20 | Swiss Aluminium Ltd. | Process for preparing fine-grained rolled aluminum products |
| DD224874A1 (en) * | 1984-06-21 | 1985-07-17 | Mansfeld Kom W Pieck Fi F Ne M | ALUMINUM ALLOYING AND METHOD FOR PROCESSING THE ALLOY |
| EP0486427A1 (en) * | 1990-11-12 | 1992-05-20 | Rieter Automotive (International) Ag | Heat shield adapted for recycling |
| US5380379A (en) * | 1993-08-18 | 1995-01-10 | Alcoa Aluminio Do Nordeste S.A. | Aluminum foil product and manufacturing method |
-
1999
- 1999-10-09 DE DE29923957U patent/DE29923957U1/en not_active Expired - Lifetime
-
2000
- 2000-08-01 PT PT00116579T patent/PT1074636E/en unknown
- 2000-08-01 ES ES00116579T patent/ES2238955T3/en not_active Expired - Lifetime
- 2000-08-01 AT AT00116579T patent/ATE291646T1/en active
- 2000-08-01 EP EP00116579A patent/EP1074636B1/en not_active Expired - Lifetime
- 2000-08-04 CZ CZ20002880A patent/CZ296688B6/en not_active IP Right Cessation
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4483719A (en) * | 1983-08-23 | 1984-11-20 | Swiss Aluminium Ltd. | Process for preparing fine-grained rolled aluminum products |
| DD224874A1 (en) * | 1984-06-21 | 1985-07-17 | Mansfeld Kom W Pieck Fi F Ne M | ALUMINUM ALLOYING AND METHOD FOR PROCESSING THE ALLOY |
| EP0486427A1 (en) * | 1990-11-12 | 1992-05-20 | Rieter Automotive (International) Ag | Heat shield adapted for recycling |
| US5380379A (en) * | 1993-08-18 | 1995-01-10 | Alcoa Aluminio Do Nordeste S.A. | Aluminum foil product and manufacturing method |
Non-Patent Citations (2)
| Title |
|---|
| P.SPIEKERMANN: "Legierungen - ein besonderes patentrechtliches Problem?", MITTEILUNG DER DEUTSCHEN PATENTANWÄLTE, 1993, DE, pages 178 - 190, XP002152326 * |
| W.HUFNAGEL: "Aluminium-Taschenbuch", 1980, ALUMINIUM VERLAG, DUSSELDORF, XP002152327 * |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101469386B (en) * | 2007-04-12 | 2011-01-26 | 日本轻金属株式会社 | Aluminum alloy sheet for battery cover and its production method |
| CN102136554B (en) * | 2007-04-12 | 2014-10-01 | 日本轻金属株式会社 | Aluminum alloy sheet for battery cover and its production method |
| WO2016005484A1 (en) * | 2014-07-09 | 2016-01-14 | Hydro Aluminium Rolled Products Gmbh | Use of an aluminium alloy or of an aluminium sheet product made from an alloy of this type for an aluminium-plastic composite part |
| CN106536772A (en) * | 2014-07-09 | 2017-03-22 | 海德鲁铝业钢材有限公司 | Use of an aluminium alloy or of an aluminium sheet product made from an alloy of this type for an aluminium-plastic composite part |
| US10792892B2 (en) | 2014-07-09 | 2020-10-06 | Hydro Aluminium Rolled Products Gmbh | Use of an aluminium alloy or of an aluminium flat product made from an alloy of this type for an aluminium-plastic composite part |
| CN111893349A (en) * | 2014-07-09 | 2020-11-06 | 海德鲁铝业钢材有限公司 | Application of aluminum alloy or flat aluminum product composed of aluminum alloy to aluminum-plastic composite component |
Also Published As
| Publication number | Publication date |
|---|---|
| PT1074636E (en) | 2005-07-29 |
| CZ20002880A3 (en) | 2001-11-14 |
| CZ296688B6 (en) | 2006-05-17 |
| DE29923957U1 (en) | 2001-07-05 |
| ES2238955T3 (en) | 2005-09-16 |
| EP1074636B1 (en) | 2005-03-23 |
| ATE291646T1 (en) | 2005-04-15 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP2770071B1 (en) | Aluminium alloy for the production of semi-finished products or components for motor vehicles, method for producing an aluminium alloy strip from this aluminium alloy and aluminium alloy strip and uses thereof | |
| DE3107276C2 (en) | Use of a non-rusting ferritic steel as a material for the production of deep-drawn sheets | |
| EP0104139B1 (en) | Aluminium alloy | |
| DE3029658C2 (en) | ||
| DE60021619T3 (en) | brazing | |
| EP1888798B1 (en) | Aluminium plain bearing alloy | |
| DE2810932A1 (en) | ALUMINUM ALLOY WITH IMPROVED WELDABILITY | |
| DE69620771T2 (en) | USE OF ROLLED ALUMINUM ALLOYS FOR CONSTRUCTION PARTS OF VEHICLES | |
| DE69402496T2 (en) | Process for the production of sheet metal from an Al alloy, which has a delayed natural aging, excellent ductility and bake hardenability | |
| DE102017103308A1 (en) | Method for producing steel sheets | |
| EP3363924A1 (en) | Aluminium alloy | |
| WO2018228640A1 (en) | Monotectic aluminum plain bearing alloy, method for producing same, and plain bearing produced therewith | |
| DE112019000856T5 (en) | Process for the manufacture of aluminum alloy components | |
| DE69612922T2 (en) | Iron-chromium alloy with good resistance to grooving and with a smooth surface | |
| EP2662461A1 (en) | Iron-chromium-manganese-nickel alloy | |
| EP2243848B1 (en) | Manganese and magnesium rich aluminium strip | |
| DE69426809T2 (en) | Process for producing easily deformable, high-strength, cold-rolled steel sheets with good resistance to embrittlement by further processing | |
| DE2641924C2 (en) | Austenitic Ni-Cv alloy with high corrosion resistance and hot formability | |
| WO2014033048A1 (en) | Aluminum alloy resistant to intercrystalline corrosion | |
| EP1074636B1 (en) | Use of aluminum alloy sheet for heat shielding | |
| EP1748088B1 (en) | Process for producing a semi-finished product or component for chassis or structural automotive applications | |
| CH654332A5 (en) | ALUMINUM ALLOY WITH HIGH ELECTRIC RESISTANCE AND EXCELLENT FORMABILITY. | |
| DE19948820B4 (en) | Heat shield made of an aluminum alloy | |
| CH690916A5 (en) | Thermaformed and weldable aluminum alloy of the AlMgSi type. | |
| EP0714993B1 (en) | Deep drawable and weldable AlMgSi type aluminium alloy |
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: A1 Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE |
|
| AX | Request for extension of the european patent |
Free format text: AL;LT;LV;MK;RO;SI |
|
| 17P | Request for examination filed |
Effective date: 20010608 |
|
| AKX | Designation fees paid |
Free format text: AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE |
|
| 17Q | First examination report despatched |
Effective date: 20040211 |
|
| GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
| RTI1 | Title (correction) |
Free format text: USE OF ALUMINUM ALLOY SHEET FOR HEAT SHIELDING |
|
| GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
| RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: HYDRO ALUMINIUM DEUTSCHLAND GMBH |
|
| GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
| AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE |
|
| 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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20050323 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: 20050323 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: 20050323 |
|
| 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: GERMAN |
|
| REF | Corresponds to: |
Ref document number: 50009840 Country of ref document: DE Date of ref document: 20050428 Kind code of ref document: P |
|
| REG | Reference to a national code |
Ref country code: SE Ref legal event code: TRGR |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
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: 20050623 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: 20050623 |
|
| GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 20050616 |
|
| REG | Reference to a national code |
Ref country code: PT Ref legal event code: SC4A Effective date: 20050607 |
|
| 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: 20050801 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: 20050801 |
|
| 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: 20050831 Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20050831 Ref country code: MC Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20050831 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20050831 |
|
| NLV1 | Nl: lapsed or annulled due to failure to fulfill the requirements of art. 29p and 29m of the patents act | ||
| REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2238955 Country of ref document: ES Kind code of ref document: T3 |
|
| REG | Reference to a national code |
Ref country code: IE Ref legal event code: FD4D |
|
| PLBI | Opposition filed |
Free format text: ORIGINAL CODE: 0009260 |
|
| PLAX | Notice of opposition and request to file observation + time limit sent |
Free format text: ORIGINAL CODE: EPIDOSNOBS2 |
|
| 26 | Opposition filed |
Opponent name: CORUS ALUMINIUM NV Effective date: 20051213 |
|
| ET | Fr: translation filed | ||
| REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
| PLAF | Information modified related to communication of a notice of opposition and request to file observations + time limit |
Free format text: ORIGINAL CODE: EPIDOSCOBS2 |
|
| PLBB | Reply of patent proprietor to notice(s) of opposition received |
Free format text: ORIGINAL CODE: EPIDOSNOBS3 |
|
| PLAB | Opposition data, opponent's data or that of the opponent's representative modified |
Free format text: ORIGINAL CODE: 0009299OPPO |
|
| R26 | Opposition filed (corrected) |
Opponent name: CORUS ALUMINIUM NV Effective date: 20051213 |
|
| BERE | Be: lapsed |
Owner name: HYDRO ALUMINIUM DEUTSCHLAND G.M.B.H. Effective date: 20050831 |
|
| PLCK | Communication despatched that opposition was rejected |
Free format text: ORIGINAL CODE: EPIDOSNREJ1 |
|
| APBP | Date of receipt of notice of appeal recorded |
Free format text: ORIGINAL CODE: EPIDOSNNOA2O |
|
| APAH | Appeal reference modified |
Free format text: ORIGINAL CODE: EPIDOSCREFNO |
|
| APBQ | Date of receipt of statement of grounds of appeal recorded |
Free format text: ORIGINAL CODE: EPIDOSNNOA3O |
|
| PLAB | Opposition data, opponent's data or that of the opponent's representative modified |
Free format text: ORIGINAL CODE: 0009299OPPO |
|
| R26 | Opposition filed (corrected) |
Opponent name: ALERIS ALUMINUM DUFFEL BVBA Effective date: 20051213 |
|
| APAH | Appeal reference modified |
Free format text: ORIGINAL CODE: EPIDOSCREFNO |
|
| APBU | Appeal procedure closed |
Free format text: ORIGINAL CODE: EPIDOSNNOA9O |
|
| PLBN | Opposition rejected |
Free format text: ORIGINAL CODE: 0009273 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: OPPOSITION REJECTED |
|
| 27O | Opposition rejected |
Effective date: 20091112 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: AT Payment date: 20110812 Year of fee payment: 12 Ref country code: FR Payment date: 20110901 Year of fee payment: 12 Ref country code: ES Payment date: 20110825 Year of fee payment: 12 Ref country code: GB Payment date: 20110819 Year of fee payment: 12 Ref country code: DE Payment date: 20110823 Year of fee payment: 12 Ref country code: SE Payment date: 20110824 Year of fee payment: 12 Ref country code: PT Payment date: 20110729 Year of fee payment: 12 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: IT Payment date: 20110825 Year of fee payment: 12 |
|
| 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: 20130201 |
|
| REG | Reference to a national code |
Ref country code: SE Ref legal event code: EUG |
|
| REG | Reference to a national code |
Ref country code: AT Ref legal event code: MM01 Ref document number: 291646 Country of ref document: AT Kind code of ref document: T Effective date: 20120801 |
|
| GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20120801 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20120802 |
|
| REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST Effective date: 20130430 |
|
| 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: 20120801 Ref country code: PT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20130201 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20120801 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20130301 Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20120801 |
|
| 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: 20120831 |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 50009840 Country of ref document: DE Effective date: 20130301 |
|
| REG | Reference to a national code |
Ref country code: ES Ref legal event code: FD2A Effective date: 20131030 |
|
| 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: 20120802 |