EP0375572B1 - Aluminium alloy for cupping, containing silicon, magnesium and copper - Google Patents
Aluminium alloy for cupping, containing silicon, magnesium and copper Download PDFInfo
- Publication number
- EP0375572B1 EP0375572B1 EP89420499A EP89420499A EP0375572B1 EP 0375572 B1 EP0375572 B1 EP 0375572B1 EP 89420499 A EP89420499 A EP 89420499A EP 89420499 A EP89420499 A EP 89420499A EP 0375572 B1 EP0375572 B1 EP 0375572B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- alloy
- content
- less
- elements
- solution treatment
- 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.)
- Expired - Lifetime
Links
- 229910052710 silicon Inorganic materials 0.000 title claims abstract description 9
- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 7
- 229910052749 magnesium Inorganic materials 0.000 title claims abstract description 7
- 229910052802 copper Inorganic materials 0.000 title abstract description 4
- 239000010949 copper Substances 0.000 title abstract 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 title abstract 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 title 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 title 1
- 239000011777 magnesium Substances 0.000 title 1
- 239000010703 silicon Substances 0.000 title 1
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 13
- 239000000956 alloy Substances 0.000 claims abstract description 13
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 8
- 238000000265 homogenisation Methods 0.000 claims abstract description 7
- 229910052726 zirconium Inorganic materials 0.000 claims abstract description 6
- 238000004519 manufacturing process Methods 0.000 claims abstract description 5
- 238000000034 method Methods 0.000 claims abstract 6
- 239000000203 mixture Substances 0.000 claims description 8
- 238000011282 treatment Methods 0.000 claims description 5
- 238000005452 bending Methods 0.000 claims description 3
- 238000010791 quenching Methods 0.000 claims description 3
- 230000000171 quenching effect Effects 0.000 claims description 3
- 238000009749 continuous casting Methods 0.000 claims description 2
- 230000032683 aging Effects 0.000 claims 1
- 238000005482 strain hardening Methods 0.000 claims 1
- 230000009466 transformation Effects 0.000 abstract description 7
- 238000004090 dissolution Methods 0.000 abstract description 4
- 238000007493 shaping process Methods 0.000 abstract description 3
- 238000000137 annealing Methods 0.000 abstract 1
- 238000005266 casting Methods 0.000 abstract 1
- 238000013000 roll bending Methods 0.000 abstract 1
- 229910052748 manganese Inorganic materials 0.000 description 5
- 230000007797 corrosion Effects 0.000 description 3
- 238000005260 corrosion Methods 0.000 description 3
- 229910052742 iron Inorganic materials 0.000 description 3
- 238000001556 precipitation Methods 0.000 description 3
- 238000001953 recrystallisation Methods 0.000 description 3
- 238000007711 solidification Methods 0.000 description 3
- 230000008023 solidification Effects 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 2
- 238000005496 tempering Methods 0.000 description 2
- 229910019064 Mg-Si Inorganic materials 0.000 description 1
- 229910019752 Mg2Si Inorganic materials 0.000 description 1
- 229910019406 Mg—Si Inorganic materials 0.000 description 1
- 241001080024 Telles Species 0.000 description 1
- 210000004027 cell Anatomy 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005496 eutectics Effects 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 229910000765 intermetallic Inorganic materials 0.000 description 1
- 239000003595 mist Substances 0.000 description 1
- 239000003973 paint Substances 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 230000008685 targeting Effects 0.000 description 1
- 239000002966 varnish Substances 0.000 description 1
- 230000002747 voluntary effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
- C22C21/08—Alloys based on aluminium with magnesium as the next major constituent with silicon
-
- 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
- C22C21/12—Alloys based on aluminium with copper as the next major constituent
- C22C21/14—Alloys based on aluminium with copper as the next major constituent with silicon
Definitions
- the invention relates to an Al alloy essentially containing Si, Mg and Cu intended for the manufacture of stampable sheets or strips, in particular sheets used in automobile bodywork.
- US-A-4,614,552 describes an Al alloy for stamping containing essentially from 0.65 to 0.79% (by weight) Cu; from 0.62 to 0.82% Mg; from 0.6 to 1.0% Si; 0.1 to 0.5% Mn; up to 0.4% Fe; up to 0.10% Ti; remains Al.
- anti-recrystallizing elements such as Mn, Cr and / or Zr, however in limited quantities.
- a preferred composition of the alloy according to the invention therefore comprises an Mn content of less than or equal to 0.2% and contents of Cr and Zr ⁇ 0.05% each.
- the manufacturing range used generally includes the following operations: . continuous or semi-continuous casting of blanks, possible homogenization, hot transformation, possible cold transformation, dissolution and tempering.
- homogenization at high temperature between 520 ° C and 560 ° C with a holding time of 6 to 24 hours is desirable. Homogenization is preferably preceded by a slow rise in temperature.
- the temperature at the end of hot transformation to avoid these recrystallizations, must imperatively be between 270 ° and 320 ° C.
- the alloy After possible cold transformation, the alloy is put into a complete solution. This takes place in the temperature range between 520 and 560 ° C, and preferably between 530 ° and 550 ° C by targeting the temperature of 550 ° C.
- the rise in temperature before dissolving must be rapid (V ⁇ 10 ° C / sec) and dissolving preferably performed either in a pass-through oven or in a sheet-to-sheet processing oven.
- the processing time varies from a few seconds to a few minutes, without being able to exceed one hour.
- the sheets and strips thus obtained have good isotropy and an average grain size generally not exceeding 60 ⁇ m.
- the quenching must be rapid and depends on the thickness of the product. For sheets and strips, it is generally carried out in calm or pulsed air.
- the parts undergo hardening income, under the usual conditions; the hardening is due to the precipitation of the Mg2Si phase and of AlCuMgSi complex phases. Tempering is typically carried out between 8 and 12 hrs around 165 ° C.
- FIG. 1 giving the field of composition of alloys in the Mg-Si plane and is illustrated by the following example: - A 1100x300x2850 mm3 plate of the following weight composition was poured semi-continuously:
- This plate was homogenized at 530 ° C-8h and immediately hot rolled; up to 4 mm thick, the final rolling temperature was 300 ° C; the strip thus obtained has been cold rolled until 1.2 mm thick, then dissolved in a passing oven at 550 ° C (about 1 min at temperature) at a speed of 20 m / min and quenched in a mist (air + water).
- an alloy with the following weight composition If: 1%; Mg: 0.4%; Cu: 0.15%; Mn: 0.1%; rest Al and usual impurities having followed the same range of transformation and heat treatment as above, has the following characteristics in state T4:
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Cookers (AREA)
- Continuous Casting (AREA)
- Conductive Materials (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
- Lead Frames For Integrated Circuits (AREA)
Abstract
Description
L'invention concerne un alliage d'Al contenant essentiellement du Si, du Mg et du Cu destiné à la fabrication de tôles ou bandes emboutissables, en particulier des tôles utilisées en carrosserie automobile.The invention relates to an Al alloy essentially containing Si, Mg and Cu intended for the manufacture of stampable sheets or strips, in particular sheets used in automobile bodywork.
Dans le brevet français FR-2 601 040 est divulguée une composition d'alliages d'Al chaudronnable et soudable, utilisable à l'état traité (trempé/revenu) après mise en forme entre l'état trempé et l'état revenu. Cependant, pour certaines applications telles que celle indiquée ci-dessus, les caractéristiques de résistance de cet alliage à l'état trempé-mûri restent insuffisantes (R 0,2 100 MPa, Rm 200 MPa, R 0,2 étant la limite élastique à 0,2% de déformation résiduelle et Rm la charge de rupture).In French patent FR-2 601 040, a composition of boilable and weldable Al alloys is disclosed, usable in the treated state (quenched / tempered) after shaping between the quenched state and the tempered state. However, for certain applications such as that indicated above, the strength characteristics of this alloy in the quenched-cured state remain insufficient (R 0.2 100 MPa, Rm 200 MPa, R 0.2 being the elastic limit at 0.2% of residual deformation and Rm the breaking load).
Il a été trouvé que l'augmentation modérée de la teneur en Cu permet de façon surprenante d'améliorer les caractéristiques de résistance, sans perte sur les caractéristiques de ductilité.It has been found that the moderate increase in the Cu content makes it possible, surprisingly, to improve the strength characteristics, without loss of the ductility characteristics.
Le brevet US-A-4 614 552 décrit un alliage d'Al pour emboutissage contenant essentiellement de 0,65 à 0,79 % (en poids) Cu; de 0,62 à 0,82% Mg; de 0,6 à 1,0 % Si; de 0,1 à 0,5 % Mn; jusqu'à 0,4 % Fe; jusqu'à 0,10 % Ti; reste Al.US-A-4,614,552 describes an Al alloy for stamping containing essentially from 0.65 to 0.79% (by weight) Cu; from 0.62 to 0.82% Mg; from 0.6 to 1.0% Si; 0.1 to 0.5% Mn; up to 0.4% Fe; up to 0.10% Ti; remains Al.
Selon l'invention, l'alliage répondant au problème posé ci-dessus a la composition pondérale suivante :
- . les teneurs en Si et Mg sont comprises dans un rectangle dont les sommets sont :
- . la teneur en Cu étant comprise entre 0,5 et 0,8
- . la teneur en Mn inférieure ou égale à 0,3%
- . la teneur en Fe inférieure ou égale à 0,35%
- . les teneurs en Cr et Zr inférieures à 0,2% chacune
- . autres éléments
chacun ≦ 0,05%
total ≦ 0,15% - . reste Al
- . the Si and Mg contents are included in a rectangle whose vertices are:
- . the Cu content being between 0.5 and 0.8
- . the Mn content less than or equal to 0.3%
- . Fe content less than or equal to 0.35%
- . Cr and Zr contents of less than 0.2% each
- . other elements
each ≦ 0.05%
total ≦ 0.15% - . stay Al
Pour les valeurs minimales en éléments principaux les caractéristiques mécaniques minimales indiquées ci-dessus ne sont pas atteintes.For the minimum values in main elements the minimum mechanical characteristics indicated above are not reached.
Pour Si supérieur à la limite DE, les risques de précipitation de Si élémentaire submicroscopique existent si la mise en solution est conduite à une température trop basse.For Si greater than the DE limit, the risks of precipitation of submicroscopic elementary Si exist if the dissolution is carried out at too low a temperature.
Pour Mg supérieur à la ligne BC, (soit Si/Mg<2 environ) des précipitations grossières de Mg₂Si sont possibles lors de la solidification et nuisent, de ce fait, aux propriétés de ductilité et d'aptitude à l'emboutissage.For Mg greater than the line BC, (ie Si / Mg <2 approximately) coarse precipitations of Mg sontSi are possible during solidification and therefore harm the ductility and drawing properties.
Pour Cu ≧ 0,8 %, le gain de résistance en caractéristiques mécaniques devient négligeable; de plus, la résistance à la corrosion et l'emboutissabilité diminuent.For Cu ≧ 0.8%, the gain in strength in mechanical characteristics becomes negligible; moreover, the corrosion resistance and the drawability decrease.
Il est possible d'ajouter à la composition des éléments anti-recristallisants tels que le Mn, le Cr et/ou le Zr cependant en quantité limitée.It is possible to add anti-recrystallizing elements to the composition such as Mn, Cr and / or Zr, however in limited quantities.
La teneur en Mn est limitée supérieurement car cet élément présente en quantité plus élevée les inconvénients suivants :
- . il donne naissance à la solidification des composés intermétalliques à base de Fe, Mn, Si qui réduisent la capacité de déformation de l'alliage et peuvent initier des décohésions et ruptures, lors des opérations de mise en forme;
- . il augmente la vitesse critique de trempe et limite donc les possibilités de traitements thermiques pour les produits épais;
- . il confère à l'alliage un comportement à la corrosion assez médiocre;
- . il n'est pas adapté aux homogénéisations de courte durée, telles que celles généralement obtenues dans des fours à passage.
- . it gives rise to the solidification of intermetallic compounds based on Fe, Mn, Si which reduce the deformation capacity of the alloy and can initiate decohesions and ruptures, during shaping operations;
- . it increases the critical quenching speed and therefore limits the possibilities of heat treatments for thick products;
- . it gives the alloy a fairly poor corrosion behavior;
- . it is not suitable for short-term homogenizations, such as those generally obtained in passage ovens.
Le Cr et le Zr ont des effets similaires à ceux du Mn, et sont donc aussi limités supérieurement.Cr and Zr have similar effects to those of Mn, and are therefore also superiorly limited.
Une composition préférentielle de l'alliage selon l'invention comporte donc une teneur en Mn inférieure ou égale à 0,2 % et des teneurs en Cr et Zr ≦ 0,05 % chacun.A preferred composition of the alloy according to the invention therefore comprises an Mn content of less than or equal to 0.2% and contents of Cr and Zr ≦ 0.05% each.
La gamme de fabrication utilisée comporte généralement les opérations suivantes:
. la coulée continue ou semi-continue d'ébauches, une homogénéisation éventuelle, une transformation à chaud, une transformation à froid éventuelle, une mise en solution et un revenu.The manufacturing range used generally includes the following operations:
. continuous or semi-continuous casting of blanks, possible homogenization, hot transformation, possible cold transformation, dissolution and tempering.
Cependant, pour obtenir de bonnes propriétés de l'alliage, ces opérations doivent être conduites dans des conditions assez étroites.However, to obtain good properties of the alloy, these operations must be carried out under fairly narrow conditions.
Ainsi, pour limiter le temps de mise en solution ultérieure, il est préférable de bien homogénéiser l'alliage en évitant de le brûler par fusion des phases eutectiques. Une homogénéisation à haute température entre 520°C et 560°C avec un temps de maintien de 6 à 24 h est souhaitable. L'homogénéisation est, de préférence précédée d'une montée lente en température.Thus, to limit the time for subsequent dissolution, it is preferable to homogenize the alloy well, avoiding burning it by fusion of the eutectic phases. Homogenization at high temperature between 520 ° C and 560 ° C with a holding time of 6 to 24 hours is desirable. Homogenization is preferably preceded by a slow rise in temperature.
Dans le cas des tôles et bandes, les recristallisations à chaud grossières (taille de grain supérieure à 80 µm) sont la source de lignes de déformations macroscopiques, visibles après emboutissage, donc rédhibitoires pour cette application.In the case of sheets and strips, coarse hot recrystallizations (grain size greater than 80 μm) are the source of macroscopic deformation lines, visible after stamping, therefore unacceptable for this application.
De ce fait, la température de fin de transformation à chaud, pour éviter ces recristallisations, doit être impérativement entre 270° et 320°C.Therefore, the temperature at the end of hot transformation, to avoid these recrystallizations, must imperatively be between 270 ° and 320 ° C.
Après transformation à froid éventuelle l'alliage est mis en solution complète. Celle-ci a lieu dans le domaine de température compris entre 520 et 560°C, et de préférence entre 530° et 550°C en visant la température de 550°C.After possible cold transformation, the alloy is put into a complete solution. This takes place in the temperature range between 520 and 560 ° C, and preferably between 530 ° and 550 ° C by targeting the temperature of 550 ° C.
En l'absence volontaire d'éléments inhibiteurs de recristallisation (Mn, Cr, Zr ≦ 0,05% chacun), la montée en température avant mise en solution doit être rapide (V ≧ 10°C/sec) et la mise en solution de préférence exécutée soit dans un four à passage, soit dans un four de traitement tôle à tôle.In the voluntary absence of recrystallization inhibiting elements (Mn, Cr, Zr ≦ 0.05% each), the rise in temperature before dissolving must be rapid (V ≧ 10 ° C / sec) and dissolving preferably performed either in a pass-through oven or in a sheet-to-sheet processing oven.
Le temps de traitement varie de quelques secondes à quelques minutes, sans pouvoir dépasser une heure. Les tôles et bandes ainsi obtenues présentent une bonne isotropie et une grosseur de grain moyenne ne dépassant pas en général 60 µm.The processing time varies from a few seconds to a few minutes, without being able to exceed one hour. The sheets and strips thus obtained have good isotropy and an average grain size generally not exceeding 60 μm.
La trempe doit être rapide et dépend de l'épaisseur du produit. Pour les tôles et bandes, elle est généralement effectuée à l'air calme ou pulsé.The quenching must be rapid and depends on the thickness of the product. For sheets and strips, it is generally carried out in calm or pulsed air.
Après les opérations de mise en forme à froid telles que emboutissage, pliage, cintrage etc...et/ou d'assemblage telle que le soudage par points, les pièces subissent un revenu de durcissement, dans les conditions habituelles; le durcissement est dû à la précipitation de la phase Mg₂Si et de phases complexes AlCuMgSi. Le revenu est typiquement effectué entre 8 et 12 h vers 165°C.After the cold forming operations such as stamping, bending, bending, etc. and / or assembly such as spot welding, the parts undergo hardening income, under the usual conditions; the hardening is due to the precipitation of the Mg₂Si phase and of AlCuMgSi complex phases. Tempering is typically carried out between 8 and 12 hrs around 165 ° C.
Il est à remarquer que dans certains cas, la cuisson de revêtements de surface tels que des vernis ou peintures, bien que plus courte, et généralement à plus haute température, réalise ipso facto ce traitement.It should be noted that in certain cases, the baking of surface coatings such as varnishes or paints, although shorter, and generally at higher temperature, ipso facto performs this treatment.
L'invention sera mieux comprise à l'aide de la figure 1 donnant le domaine de composition des alliages dans le plan Mg-Si et est illustrée par l'exemple suivant:
- on a coulé en semi-continu une plaque 1100x300x2850 mm3 de la composition pondérale suivante:
- A 1100x300x2850 mm3 plate of the following weight composition was poured semi-continuously:
Cette plaque a été homogénéisée à 530°C-8h et immédiatement laminée à chaud; jusqu'à 4 mm d'épaisseur,la température finale du laminage était de 300°C; la bande ainsi obtenue a été relaminée à froid jusqu'a 1,2 mm d'épaisseur, puis mise en solution en four à passage à 550°C (de l'ordre de 1 min à température) à la vitesse de 20 m/min et trempée au brouillard (air+eau).This plate was homogenized at 530 ° C-8h and immediately hot rolled; up to 4 mm thick, the final rolling temperature was 300 ° C; the strip thus obtained has been cold rolled until 1.2 mm thick, then dissolved in a passing oven at 550 ° C (about 1 min at temperature) at a speed of 20 m / min and quenched in a mist (air + water).
Les résultats obtenus sur tôle de 1,2 mm d'épaisseur aux états T4 et T6, dans le sens travers long, sont les suivants:
A titre de comparaison, un alliage de composition pondérale suivante :
Si: 1%; Mg: 0,4%; Cu: 0,15%; Mn: 0,1%; reste Al et impuretés habituelles ayant suivi la même gamme de transformation et de traitement thermique que ci-dessus, présente à l'état T4 les caractéristiques suivantes :
If: 1%; Mg: 0.4%; Cu: 0.15%; Mn: 0.1%; rest Al and usual impurities having followed the same range of transformation and heat treatment as above, has the following characteristics in state T4:
Claims (7)
- An aluminium alloy for the production of drawable sheets characterized in that it has the following composition (% by weight):. the Cu is comprised between 0.5 and 0.8%. the elements Cr and Zr less than 0.2% each. Mn ≦ 0.3%. Fe ≦ 0.35%. other elements: each ≦ 0.05%, total ≦ 0.15%. the balance being Al
- Alloy according to claim 1, characterized in that the Mn content is less than or equal to 0.2% and Cr & Zr < 0.05% each.
- Alloy according to one of claims 1 or 2, characterized in that the average grain size is less than 80 µm and preferably less than 60 µm.
- Process for obtaining products according to one of claims 1 to 3, comprising the continuous or semi-continuous casting of ingots, optional homogenization, hot working, optional cold working, solution treatment, quenching operation forming operation, for example by drawing, folding, bending, and finally artificial aging characterized in that the final hot working takes place between 270 and 320°C.
- Process according to claim 4, characterized in that the homogneization or complete solution treatment takes place between 520 and 560°C.
- Process according to claim 5, characterized in that the homogenization or solution treatment takes place between 530 and 550°C.
- Process according to one of claims 5 or 6, characterized in that the solution treatment is preceded by a rise in temperature at a speed which is greater than 10°C/sec.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT89420499T ATE90978T1 (en) | 1988-12-21 | 1989-12-19 | DRAWING ALUMINUM ALLOY CONTAINING SILICON, MAGNESIUM AND COPPER. |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8817621A FR2642436B1 (en) | 1988-12-21 | 1988-12-21 | A1 ALLOY CONTAINING ESSENTIALLY SI, MG AND CU FOR STAMPING |
FR8817621 | 1988-12-21 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0375572A1 EP0375572A1 (en) | 1990-06-27 |
EP0375572B1 true EP0375572B1 (en) | 1993-06-23 |
Family
ID=9373742
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP89420499A Expired - Lifetime EP0375572B1 (en) | 1988-12-21 | 1989-12-19 | Aluminium alloy for cupping, containing silicon, magnesium and copper |
Country Status (5)
Country | Link |
---|---|
EP (1) | EP0375572B1 (en) |
AT (1) | ATE90978T1 (en) |
DE (1) | DE68907332T2 (en) |
ES (1) | ES2041438T3 (en) |
FR (1) | FR2642436B1 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2713664B1 (en) * | 1993-11-17 | 1996-05-24 | Pechiney Rhenalu | Al-Si-Mg alloy with improved ductility and stampability and process for obtaining it. |
CH688379A5 (en) * | 1994-11-29 | 1997-08-29 | Alusuisse Lonza Services Ag | Thermaformed and weldable aluminum alloy of the AlMgSi type |
FR2748035B1 (en) * | 1996-04-29 | 1998-07-03 | Pechiney Rhenalu | ALUMINUM-SILICON-MAGNESIUM ALLOY FOR AUTOMOTIVE BODYWORK |
WO1997047779A1 (en) * | 1996-06-14 | 1997-12-18 | Aluminum Company Of America | Highly formable aluminum alloy rolled sheet |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4082578A (en) * | 1976-08-05 | 1978-04-04 | Aluminum Company Of America | Aluminum structural members for vehicles |
US4424084A (en) * | 1980-08-22 | 1984-01-03 | Reynolds Metals Company | Aluminum alloy |
JPS6055586B2 (en) * | 1982-11-30 | 1985-12-05 | 株式会社神戸製鋼所 | High strength corrosion resistant aluminum alloy for brazing |
US4614552A (en) * | 1983-10-06 | 1986-09-30 | Alcan International Limited | Aluminum alloy sheet product |
ATE68529T1 (en) * | 1985-11-04 | 1991-11-15 | Aluminum Co Of America | VEHICLE PART MADE OF ALUMINUM ALLOY. |
-
1988
- 1988-12-21 FR FR8817621A patent/FR2642436B1/en not_active Expired - Fee Related
-
1989
- 1989-12-19 EP EP89420499A patent/EP0375572B1/en not_active Expired - Lifetime
- 1989-12-19 AT AT89420499T patent/ATE90978T1/en active
- 1989-12-19 ES ES198989420499T patent/ES2041438T3/en not_active Expired - Lifetime
- 1989-12-19 DE DE89420499T patent/DE68907332T2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP0375572A1 (en) | 1990-06-27 |
ES2041438T3 (en) | 1993-11-16 |
FR2642436B1 (en) | 1991-06-14 |
DE68907332T2 (en) | 1993-11-11 |
DE68907332D1 (en) | 1993-07-29 |
FR2642436A1 (en) | 1990-08-03 |
ATE90978T1 (en) | 1993-07-15 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0717784B1 (en) | Aluminium-silicon alloy sheet for mechanical, aircraft and space applications | |
EP0949344B1 (en) | Process for making aluminium alloy sheet | |
EP0259232B2 (en) | Easily workable and weldable aluminium alloy, and process for its manufacture | |
FR2843754A1 (en) | Balanced aluminum-copper-magnesium-silicon alloy product for fuselage sheet or lower-wing sheet of aircraft, contains copper, silicon, magnesium, manganese, zirconium, chromium, iron, and aluminum and incidental elements and impurities | |
EP0162096B1 (en) | Aluminium alloys containing lithium, magnesium and copper | |
FR2584094A1 (en) | HIGH STRENGTH TITANIUM ALLOY MATERIAL HAVING IMPROVED OUVABILITY AND PROCESS FOR PRODUCING THE SAME | |
JPH11507102A (en) | Aluminum or magnesium alloy plate or extruded product | |
EP0686208B1 (en) | Process for making high formability aluminium alloy sheets | |
EP0679199B1 (en) | Aluminium-silicon-magnesium alloy having improved ductility and deep-drawing properties, and method for producing same | |
EP0756017B1 (en) | Aluminium-copper-magnesium alloy with high creep resistance | |
WO2015011346A1 (en) | Extrados structural element made from an aluminium copper lithium alloy | |
EP0157711B1 (en) | Process for the manufacture of objects from al-li-mg-cu alloys with high ductibility and isotropy properties | |
JP3022922B2 (en) | Method for producing plate or strip material with improved cold rolling characteristics | |
EP0375572B1 (en) | Aluminium alloy for cupping, containing silicon, magnesium and copper | |
EP0227563B1 (en) | Process od desensitization to exfoliating corrosion of lithium-containing aluminium alloys, resulting simultaneously in a high mechanical resistance and in good damage limitation | |
EP0388283B1 (en) | Stainless ferritic steel and process for manufacturing this steel | |
CA1333232C (en) | Alloy product containing li, which is resistant to corrosion under stress, and process for its preparation | |
JPS6283445A (en) | High strength aluminum alloy for casting | |
EP0300927B1 (en) | Aluminium based alloy for cans and process of manufacturing | |
JPH11350058A (en) | Aluminum alloy sheet excellent in formability and baking hardenability and its production | |
JPH10259464A (en) | Production of aluminum alloy sheet for forming | |
JP3557953B2 (en) | Aluminum alloy sheet for precision machining and method of manufacturing the same | |
JPH08165539A (en) | Heat treated type thin aluminum extruded shape and its production | |
JPS63277744A (en) | Can end part made of aluminum alloy and its production | |
JP2613522B2 (en) | Aluminum alloy plate for stay tub |
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 DE ES GB GR IT LI LU NL SE |
|
17P | Request for examination filed |
Effective date: 19900803 |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: PECHINEY RHENALU |
|
17Q | First examination report despatched |
Effective date: 19920717 |
|
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 DE ES GB GR IT LI LU NL SE |
|
REF | Corresponds to: |
Ref document number: 90978 Country of ref document: AT Date of ref document: 19930715 Kind code of ref document: T |
|
ITF | It: translation for a ep patent filed | ||
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 19930630 |
|
REF | Corresponds to: |
Ref document number: 68907332 Country of ref document: DE Date of ref document: 19930729 |
|
REG | Reference to a national code |
Ref country code: GR Ref legal event code: FG4A Free format text: 3008253 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2041438 Country of ref document: ES Kind code of ref document: T3 |
|
EPTA | Lu: last paid annual fee | ||
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 |
|
26N | No opposition filed | ||
EAL | Se: european patent in force in sweden |
Ref document number: 89420499.9 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: AT Payment date: 19951116 Year of fee payment: 7 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GR Payment date: 19951130 Year of fee payment: 7 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: BE Payment date: 19951201 Year of fee payment: 7 Ref country code: LU Payment date: 19951201 Year of fee payment: 7 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: ES Payment date: 19951212 Year of fee payment: 7 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: NL Payment date: 19951230 Year of fee payment: 7 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: SE Payment date: 19961118 Year of fee payment: 8 |
|
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: 19961219 Ref country code: AT Effective date: 19961219 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Effective date: 19961231 |
|
BERE | Be: lapsed |
Owner name: PECHINEY RHENALU Effective date: 19961231 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GR Free format text: THE PATENT HAS BEEN ANNULLED BY A DECISION OF A NATIONAL AUTHORITY Effective date: 19970630 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Effective date: 19970701 |
|
REG | Reference to a national code |
Ref country code: GR Ref legal event code: MM2A Free format text: 3008253 |
|
NLV4 | Nl: lapsed or anulled due to non-payment of the annual fee |
Effective date: 19970701 |
|
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: 19971220 Ref country code: ES Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 19971220 |
|
EUG | Se: european patent has lapsed |
Ref document number: 89420499.9 |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: IF02 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FD2A Effective date: 19980113 |
|
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;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED. Effective date: 20051219 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: CH Payment date: 20081229 Year of fee payment: 20 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20090202 Year of fee payment: 20 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20081229 Year of fee payment: 20 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: PE20 Expiry date: 20091218 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20091218 |