EP0020282A1 - Process for the manufacture of hollow bodies of an aluminium alloy, and products thus obtained - Google Patents
Process for the manufacture of hollow bodies of an aluminium alloy, and products thus obtained Download PDFInfo
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- EP0020282A1 EP0020282A1 EP80420064A EP80420064A EP0020282A1 EP 0020282 A1 EP0020282 A1 EP 0020282A1 EP 80420064 A EP80420064 A EP 80420064A EP 80420064 A EP80420064 A EP 80420064A EP 0020282 A1 EP0020282 A1 EP 0020282A1
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- 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
- C22C21/10—Alloys based on aluminium with zinc as the next major constituent
Definitions
- This invention relates to a method for manufacturing hollow bodies of aluminum alloy and to the products thus obtained, which have high ductility (in the long direction) and high toughness (in the cross direction) when they are treated with resistance levels higher than 660 MPa.
- alloys A-Z8GU (or 7049 A) according to the AFNOR 50-411 standard, the analysis of which is given in Table 1, are particularly used in the manufacture of hollow bodies under pressure, due to the high mechanical characteristics which '' they acquire in the quenched-income state (state T6).
- the aim of this invention is therefore to solve this problem by a suitable choice partially covering the field of alloy 7049 A, which makes it possible to obtain, according to the process, products having high ductility and toughness characteristics, and, therefore, great job security.
- the general composition of the alloys according to the invention is as follows (by weight):
- the V content is limited to a content of less than 0.01%.
- the products are transformed in the following way: - homogenization between 460 and 490 ° C of the cast billets, hot deformation between 320 and 420 ° C, including possibly the shrinking of one (or both) end ( s) in the case of the production of hollow bodies, dissolving between 460 and 480 ° C. and tempering suitable for obtaining a breaking load (long direction) and a limit burst stress (transverse direction) greater than or equal to 660 MPa .
- the hot deformation is preferably carried out by reverse spinning; homogenization, dissolution and tempering conditions may be different from those indicated above without departing from the scope of the invention.
- Particles are considered to be part of a cluster when the interparticle distance is less than or equal to the largest dimension of the particle considered.
- the length taken into account is the cumulative length of the maximum dimensions of each particle in the cluster.
- the alloys marked 1 to 12 were vertically semi-continuously cast in 0 185 mm billets, which were homogenized 24 h at 450 ° C. These billets were machined at 0 170 mm and drilled with a central hole 0 70 mm for reverse spinning of tubes 0 82 x 67.5 mm at a temperature of 365 ° C.
- alloys 1 to 8 the composition of which is outside the scope of the invention, while alloys 9 to 12, according to the invention, achieve them.
- the micrographic structure of the ingot in its lower 1/3 is represented by FIG. 1 at 200 magnification. No compound larger than 35 microns in its largest dimension is observed. In addition, all the compounds out of solution are observed in the interdendritic spaces. A good part of them is moreover resolved by subsequent heat treatments.
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Abstract
L'invention est relative à un procédé d'obtention de corps creux en alliage d'aluminium, présentant une grande résistance à l'éclatement et aux produits ainsi obtenus. L'alliage contient (en poids: 7,6 à 9,5% Zn, 1 à 2% Cu; 2,4 à 3,5% Mg; 0,07 à 0,17% Cr; 0,15 à 0,25% Mn; 0,08 à 0,14% Zr; moins de 0,2% Fe, de 0,15% Si, de 0,10% Ti, et éventuellement moins de 0,01% V. Il présente une charge de rupture (sens long) et une résistance à l'éclatement (sens travers) supérieures ou égales à 660 MPa. Sa structure est caractérisée par l'absence de gros composés intermétalliques (>= 35 µm) après un test de solidification spécifique. Il peut être utilisé dans toutes les applications de sécurité comportant une enceinte sous pression (bouteilles de gaz comprimés, etc ...)The invention relates to a process for obtaining hollow bodies made of aluminum alloy, having high resistance to bursting and to the products thus obtained. The alloy contains (by weight: 7.6 to 9.5% Zn, 1 to 2% Cu; 2.4 to 3.5% Mg; 0.07 to 0.17% Cr; 0.15 to 0, 25% Mn; 0.08 to 0.14% Zr; less than 0.2% Fe, 0.15% Si, 0.10% Ti, and possibly less than 0.01% V. It has a charge breaking strength (long direction) and burst strength (cross direction) greater than or equal to 660 MPa. Its structure is characterized by the absence of large intermetallic compounds (> = 35 µm) after a specific solidification test. can be used in all security applications including a pressure vessel (compressed gas cylinders, etc.)
Description
Cette invention se rapporte à un procédé de fabrication de corps creux en alliage d'aluminium et aux produits ainsi obtenus, qui possèdent une grande ductilité (dans le sens long) et une grande ténacité (dans le sens travers) lorsqu'ils sont traités à des niveaux de résistance supérieurs à 660 MPa.This invention relates to a method for manufacturing hollow bodies of aluminum alloy and to the products thus obtained, which have high ductility (in the long direction) and high toughness (in the cross direction) when they are treated with resistance levels higher than 660 MPa.
On sait que les alliages A-Z8GU (ou 7049 A) selon la norme AFNOR 50-411, dont l'analyse est reportée au tableau 1, sont particulièrement utilisés dans la fabrication de corps creux sous pression, en raison des hautes caractéristiques mécaniques qu'ils acquièrent à l'état trempe-revenu (état T6).It is known that the alloys A-Z8GU (or 7049 A) according to the AFNOR 50-411 standard, the analysis of which is given in Table 1, are particularly used in the manufacture of hollow bodies under pressure, due to the high mechanical characteristics which '' they acquire in the quenched-income state (state T6).
Or, ces alliages ne sont pas toujours fiables en ce sens que des ruptures ou éclatements prématurés sont parfois observés lors des épreuves hydrauliques de contrôle de tels corps creux soumis à une pression interne.However, these alloys are not always reliable in the sense that premature ruptures or bursts are sometimes observed during hydraulic tests to control such hollow bodies subjected to internal pressure.
Le but de cette invention est donc de résoudre ce problème par un choix convenable couvrant partiellement le domaine de l'alliage 7049 A, qui permet d'obtenir, selon le procédé, des produits présentant des caractéristiques de ductilité et de ténacité élevées, et, par conséquent, une grande sécurité d'emploi.The aim of this invention is therefore to solve this problem by a suitable choice partially covering the field of alloy 7049 A, which makes it possible to obtain, according to the process, products having high ductility and toughness characteristics, and, therefore, great job security.
Ce but est atteint de façon surprenante :
- 1°) Essentiellement en diminuant les teneurs des éléments Cr, Mn et Zr, qui sont connus pour être des inhibiteurs de recristallisation dans les alliages d'Al (voir ALTENPOHL, "Un regard à l'intérieur de l'aluminium", éd. française, 1976, p. 148).
Or, en vue d'obtenir les très hautes caractéristiques mécaniques recherchées, l'alliage est, en effet, utilisé à l'état non recristallisé avec effet de presse, même après les traitements de mise en solution, trempe et revenu. - 2°) En augmentant au-delà des limites habituelles les teneurs en éléments principaux tels que Zn, Cu, Mg.
- 3°) En limitant à des niveaux bas ou très bas les teneurs des éléments mineurs (Fe, Si, Ti) ou même des impuretés telles que le V.
- 1 °) Essentially by reducing the contents of the elements Cr, Mn and Zr, which are known to be inhibitors of recrystallization in the alloys of Al (see ALTENPOHL, "A look inside aluminum", ed. French, 1976, p. 148).
However, in order to obtain the very high mechanical properties sought, the alloy is, in fact, used in the non-recrystallized state with press effect, even after the dissolution, quenching and tempering treatments. - 2 °) By increasing beyond the usual limits the contents of main elements such as Zn, Cu, Mg.
- 3 °) By limiting the contents of minor elements (Fe, Si, Ti) or even impurities such as V. to low or very low levels.
La composition générale des alliages suivant l'invention est la suivante (en poids) :
Dans une composition préférentielle, la teneur en V est limitée à une teneur inférieure à 0,01 %.In a preferred composition, the V content is limited to a content of less than 0.01%.
Dans le procédé, les produits sont transformés de la façon suivante : - homogénéisation entre 460 et 490° C des billettes coulées, déformation à chaud entre 320 et 420° C, y compris éventuellement le rétreint d'une ( ou des deux) extrémité(s) dans le cas de fabrication de corps creux, mise en solution entre 460 et 480° C et revenu adapté pour obtenir une charge de rupture (sens long) et une contrainte limite d'éclatement (sens travers) supérieures ou égales à 660 MPa.In the process, the products are transformed in the following way: - homogenization between 460 and 490 ° C of the cast billets, hot deformation between 320 and 420 ° C, including possibly the shrinking of one (or both) end ( s) in the case of the production of hollow bodies, dissolving between 460 and 480 ° C. and tempering suitable for obtaining a breaking load (long direction) and a limit burst stress (transverse direction) greater than or equal to 660 MPa .
Dans ces conditions et, pour une charge de rupture égale à 660 MPa, l'allongement dans le sens long est supérieur à 9 cet allongement est mesuré sur une longueur de base lo = 5,65 √S, S étant la section de l'éprouvette. La déformation à chaud est réalisée, de préférence, par filage inverse ; des conditions d'homogénéisation, de mise en solution et de revenu peuvent être différentes de celles indiquées ci-dessus sans sortir du domaine de l'invention.Under these conditions and, for a breaking load equal to 660 MPa, the elongation in the long direction is greater than 9 this elongation is measured over a basic length lo = 5.65 √S, S being the section of the test tube. The hot deformation is preferably carried out by reverse spinning; homogenization, dissolution and tempering conditions may be different from those indicated above without departing from the scope of the invention.
La contrainte d'éclatement (RE) lors de l'épreuve hydraulique est donnée par la formule classique:
- e : est l'épaisseur minimum du tube ou du corps creux (supposé sensiblement cylindrique circulaire).
- D : est le diamètre moyen du cylindre , soit
- p : est la pression d'éclatement
- e: is the minimum thickness of the tube or hollow body (assumed to be substantially circular cylindrical).
- D: is the mean diameter of the cylinder,
- p: is the burst pressure
Il a été constaté que les éléments Cr, Mn, Zr ortun effet synergétique imprévisible, c'est-à-dire que leur action globale sur les caractéristiques mécaniques est très largement supérieure à la somme des actions inviduelles de chacun d'eux. Cet effet est nettement mis en évidence dans les exemples donnés ci-après. Il n'était donc pas du tout évident de choisir cette combinaison particulière de teneurs en ces éléments pour obtenir les propriétés recherchées.It has been found that the elements Cr, Mn, Zr have an unpredictable synergistic effect, that is to say that their overall action on the mechanical characteristics is very much greater than the sum of the individual actions of each of them. This effect is clearly demonstrated in the examples given below. It was therefore not at all obvious to choose this particular combination of contents of these elements to obtain the desired properties.
Les alliages suivant l'invention répondent au test de contrôle suivant :
- - 200 g d'alliage environ sont refondus à 735° C ± 5° C dans un creuset de graphite poteyé d'alumine
- - on soumet ensuite l'ensemble à un refroidissement lent en four, à raison de 0,5 à 1° C/min. suivi d'un palier de 2 h à une température supérieure à 2 à 4°C à celle du début de solidification de l'alliage (liquidus), puis on sort le creuset à l'air pour assurer une solidification rapide.
- - l'examen en micrographie optique au grossissement x 100 à 500 d'un échantillon poli prélevé dans la moitié inférieure du lingotin ainsi obtenu, ne révèle aucun amas de constituants intermétalliques primaires ou de particules intermétalliques individuelles massives, non dendritiques, de forme générale polygonale, de longueur supérieure à 35 ym dans leur plus grande dimension.
- - about 200 g of alloy are melted at 735 ° C ± 5 ° C in a crucible of alumina-containing graphite
- - The assembly is then subjected to slow cooling in the oven, at a rate of 0.5 to 1 ° C / min. followed by a 2-hour plateau at a temperature greater than 2 to 4 ° C than that of the beginning of solidification of the alloy (liquidus), then the crucible is removed in the air to ensure rapid solidification.
- - examination in optical micrography at 100 × 500 magnification of a polished sample taken from the lower half of the ingot thus obtained, does not reveal any mass of primary intermetallic constituents or of individual massive non-dendritic intermetallic particles, of general polygonal shape , of length greater than 35 μm in their largest dimension.
Les particules sont considérées comme faisant partie d'un amas lorsque la distance interparticulaire est inférieure ou égale à la plus grande dimension de la particule considérée. Dans ce cas, la longueur prise en compte est la longueur cumulée des dimensions maximales de chaque particule de l'amas.Particles are considered to be part of a cluster when the interparticle distance is less than or equal to the largest dimension of the particle considered. In this case, the length taken into account is the cumulative length of the maximum dimensions of each particle in the cluster.
L'invention sera mieux comprise et illustrée par les exemples suivants :The invention will be better understood and illustrated by the following examples:
Les alliages repérés 1 à 12 dont les compositions (% en poids) sont reportées au tableau II ont été coulés en semi-continu verticalement, en billettes 0 185 mm, qui ont été homogénéisées 24 h à 450° C. Ces billettes ont été usinées à 0 170 mm et forées d'un trou central 0 70 mm pour filage inverse de tubes 0 82 x 67,5 mm à une température de 365° C.The alloys marked 1 to 12, the compositions of which (% by weight) are given in Table II, were vertically semi-continuously cast in 0 185 mm billets, which were homogenized 24 h at 450 ° C. These billets were machined at 0 170 mm and drilled with a central hole 0 70 mm for reverse spinning of tubes 0 82 x 67.5 mm at a temperature of 365 ° C.
Les tubes ont été ensuite traités de la façon suivante :
- - mise en solution à 460° C pendant 45 minutes
- - trempe à l'eau froide (10-15°C)
- - revenu à 125° C pendant 20 h
Les tubes ainsi obtenus ont été soumis à des essais de traction suivant une direction parallèle aux génératrices du tube et à des essais d'éclatement sous pression hydraulique (déchirure longitudinale).The tubes were then treated as follows:
- - dissolved at 460 ° C for 45 minutes
- - quenching in cold water (10-15 ° C)
- - returned to 125 ° C for 20 h
The tubes thus obtained were subjected to tensile tests in a direction parallel to the generatrices of the tube and to bursting tests under hydraulic pressure (longitudinal tear).
On a relevé la charge de rupture (Rm), la limité élastique (R 0,2), l'allongement (A %) et la contrainte d'éclatement (RE).The breaking load (Rm), the elastic limit (R 0.2), the elongation (A%) and the bursting stress (RE) were noted.
Les résultats obtenus sont reportés dans le tableau III.The results obtained are reported in Table III.
Les effets individuels des additions de 0,07 % Cr (rep. A), de 0,08 % Zr (rep. B) et de 0,15 % Mn (rep. C) sont reportés au tableau IV. On constate que la somme des effets individuels (lignes A + B + C) est largement inférieure à celle des additions conjointes (ligne D suivant l'invention) de l'ensemble de ces éléments sur.les caractéristiques de traction et de façon particulièrement spectaculaire sur la limite élastique et les allongements. Elle reste cependant sans effet notable sur la résistance à l'éclatement.The individual effects of the additions of 0.07% Cr (rep. A), 0.08% Zr (rep. B) and 0.15% Mn (rep. C) are shown in Table IV. It can be seen that the sum of the individual effects (lines A + B + C) is much lower than that of the joint additions (line D according to the invention) of all of these elements on the traction characteristics and in a particularly spectacular manner. on the elastic limit and the elongations. However, it has no significant effect on the burst strength.
Ainsi, l'effet synergétique de ces éléments, imprévisible a priori, est bien démontré.Thus, the synergistic effect of these elements, unpredictable a priori, is well demonstrated.
Par ailleurs, on constate bien que les caractéristiques visées ne sont pas atteintes pour les alliages 1 à 8 dont la composition est hors du domaine de l'invention alors que les alliages 9 à 12, selon l'invention, les atteignent.Furthermore, it can be seen that the characteristics targeted are not achieved for alloys 1 to 8, the composition of which is outside the scope of the invention, while alloys 9 to 12, according to the invention, achieve them.
Trois coulées en semi-continu d'alliage 7049 A, sortant des limites de composition de la présente invention, ont été effectuées.Les analyses obtenues sont reportées au tableau V.Three semi-continuous castings of alloy 7049 A, outside the composition limits of the present invention, were carried out. The analyzes obtained are given in Table V.
Celles-ci ont été transformées en tubes dans les conditions de l'exemple 1 par filage inverse, et ceux-ci ont été rétreints et traités à l'état T6 par mise en solution à 465° ± 5° C, 45 mn, trempe eau et revenu 125° C, 20 h. Les contraintes de rupture sous épreuve hydraulique, calculées comme indiqué ci-dessus, sont également données au tableau V. On peut constater qu'elles sont nettement inférieures à la valeur limite visée (660 MPa).These were transformed into tubes under the conditions of Example 1 by reverse spinning, and these were shrunk and treated in the T6 state by dissolving at 465 ° ± 5 ° C, 45 min, quenching water and tempering 125 ° C, 20 h. The breaking stresses under hydraulic test, calculated as indicated above, are also given in Table V. It can be seen that they are much lower than the target limit value (660 MPa).
Sur du métal conforme à l'invention (Rep. 12, tableau II) et non conforme à l'invention (Rep. E, tableau V), nous avons procédé au test de solidification suivant :
- - prélèvement de 200 g de métal dans les billettes coulées en série continue,
- - fusion du prélèvement à 735° C t 5° C,
- - refroidissement à 632° C à raison de 0,5 à 1°C/minute,
- - maintien 2 h à 632° C (début de solidification de l'alliage à 628° C),
- - sortie du four et refroidissement rapide.
- - removal of 200 g of metal from the billet cast in continuous series,
- - fusion of the sample at 735 ° C t 5 ° C,
- - cooling to 632 ° C at a rate of 0.5 to 1 ° C / minute,
- - 2 h hold at 632 ° C (start of solidification of the alloy at 628 ° C),
- - exit from the oven and rapid cooling.
Sur l'alliage conforme à l'invention, la structure micrographique du lingot dans son 1/3 inférieur est représentée par la figure 1 au grossissement 200. On n'observe aucun composé de taille supérieure à 35 microns dans sa plus grande dimension. De plus, tous les composés hors solution sont observés dans les espaces interdendritiques. Une bonne partie d'entre eux est d'ailleurs résolue par traitements thermiques ultérieurs.On the alloy in accordance with the invention, the micrographic structure of the ingot in its lower 1/3 is represented by FIG. 1 at 200 magnification. No compound larger than 35 microns in its largest dimension is observed. In addition, all the compounds out of solution are observed in the interdendritic spaces. A good part of them is moreover resolved by subsequent heat treatments.
Au contraire, dans le cas de l'alliage sortant du domaine de l'invention ; (Cr 0,22 %, Mn 0,27 %, Zr 0,13 %), il est possible d' observer des composés intermétalliques primaire de forme polyédrique, de dimension supérieure à 100 microns et groupés en colonies (figure 2). Ces cristaux ne peuvent être confondus avec ceux de la figure 1, ni par leur dimension, ni par leur situation, ni enfin par leur évolution en cours de transformation. Ils ne subissent, en effet, aucune modification par l'effet des traitements thermiques. Ils se fragmentent et s'alignent, en restant contigus, dans la direction principale de la déformation, avec toutes les conséquences qu'implique cette configuration sur la fragilité du produit.
Claims (3)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7915054A FR2457908A1 (en) | 1979-06-01 | 1979-06-01 | PROCESS FOR PRODUCING HOLLOW BODIES OF ALUMINUM ALLOY AND PRODUCTS THUS OBTAINED |
FR7915054 | 1979-06-01 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0020282A1 true EP0020282A1 (en) | 1980-12-10 |
EP0020282B1 EP0020282B1 (en) | 1982-12-29 |
Family
ID=9226502
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP80420064A Expired EP0020282B1 (en) | 1979-06-01 | 1980-05-28 | Process for the manufacture of hollow bodies of an aluminium alloy, and products thus obtained |
Country Status (11)
Country | Link |
---|---|
US (1) | US4345951A (en) |
EP (1) | EP0020282B1 (en) |
BE (1) | BE883565A (en) |
CA (1) | CA1118190A (en) |
CH (1) | CH644402A5 (en) |
DE (1) | DE3061495D1 (en) |
ES (1) | ES8102198A1 (en) |
FR (1) | FR2457908A1 (en) |
IT (1) | IT1130700B (en) |
NO (1) | NO153184C (en) |
ZA (1) | ZA803235B (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2640644A1 (en) * | 1988-12-19 | 1990-06-22 | Pechiney Recherche | PROCESS FOR THE "SPRAY-DEPOSITION" PRODUCTION OF 7000 SER AL ALLOYS AND DISCONTINUOUS REINFORCED COMPOSITE MATERIALS HAVING HIGH MECHANICAL RESISTANCE AND GOOD DUCTILITY AS MATRIX |
WO1994024326A1 (en) * | 1993-04-15 | 1994-10-27 | Alcan International Limited | Method of making hollow bodies |
EP0670377A1 (en) * | 1994-03-02 | 1995-09-06 | Pechiney Recherche (Gie) | High-strength aluminium alloy 7000 and manufacturing process |
WO2003085146A1 (en) | 2002-04-05 | 2003-10-16 | Pechiney Rhenalu | Al-zn-mg-cu alloys welded products with high mechanical properties, and aircraft structural elements |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
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US4863528A (en) * | 1973-10-26 | 1989-09-05 | Aluminum Company Of America | Aluminum alloy product having improved combinations of strength and corrosion resistance properties and method for producing the same |
FR2517702B1 (en) * | 1981-12-03 | 1985-11-15 | Gerzat Metallurg | |
US5221377A (en) * | 1987-09-21 | 1993-06-22 | Aluminum Company Of America | Aluminum alloy product having improved combinations of properties |
US5496426A (en) * | 1994-07-20 | 1996-03-05 | Aluminum Company Of America | Aluminum alloy product having good combinations of mechanical and corrosion resistance properties and formability and process for producing such product |
IL156386A0 (en) | 2000-12-21 | 2004-01-04 | Alcoa Inc | Aluminum alloy products and artificial aging method |
FR2838136B1 (en) * | 2002-04-05 | 2005-01-28 | Pechiney Rhenalu | ALLOY PRODUCTS A1-Zn-Mg-Cu HAS COMPROMISED STATISTICAL CHARACTERISTICS / DAMAGE TOLERANCE IMPROVED |
DE502005001724D1 (en) | 2005-01-19 | 2007-11-29 | Fuchs Kg Otto | Quench-resistant aluminum alloy and method for producing a semifinished product from this alloy |
US8083871B2 (en) | 2005-10-28 | 2011-12-27 | Automotive Casting Technology, Inc. | High crashworthiness Al-Si-Mg alloy and methods for producing automotive casting |
US8840737B2 (en) * | 2007-05-14 | 2014-09-23 | Alcoa Inc. | Aluminum alloy products having improved property combinations and method for artificially aging same |
US8673209B2 (en) * | 2007-05-14 | 2014-03-18 | Alcoa Inc. | Aluminum alloy products having improved property combinations and method for artificially aging same |
US8206517B1 (en) | 2009-01-20 | 2012-06-26 | Alcoa Inc. | Aluminum alloys having improved ballistics and armor protection performance |
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GB552972A (en) * | 1942-06-12 | 1943-05-03 | Nat Smelting Co | Improvements in or relating to aluminium base alloys |
FR1322510A (en) * | 1962-05-02 | 1963-03-29 | Aluminum Co Of America | Improvement of articles in aluminum-based alloy obtained by heat treatment |
FR2113037A5 (en) * | 1970-10-23 | 1972-06-23 | Fuchs Otto |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
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US4305763A (en) * | 1978-09-29 | 1981-12-15 | The Boeing Company | Method of producing an aluminum alloy product |
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1979
- 1979-06-01 FR FR7915054A patent/FR2457908A1/en active Granted
-
1980
- 1980-05-28 DE DE8080420064T patent/DE3061495D1/en not_active Expired
- 1980-05-28 EP EP80420064A patent/EP0020282B1/en not_active Expired
- 1980-05-29 IT IT22416/80A patent/IT1130700B/en active
- 1980-05-30 BE BE0/200831A patent/BE883565A/en not_active IP Right Cessation
- 1980-05-30 CA CA000353060A patent/CA1118190A/en not_active Expired
- 1980-05-30 CH CH421480A patent/CH644402A5/en not_active IP Right Cessation
- 1980-05-30 ES ES491989A patent/ES8102198A1/en not_active Expired
- 1980-05-30 NO NO801611A patent/NO153184C/en unknown
- 1980-05-30 US US06/155,116 patent/US4345951A/en not_active Expired - Lifetime
- 1980-05-30 ZA ZA00803235A patent/ZA803235B/en unknown
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB552972A (en) * | 1942-06-12 | 1943-05-03 | Nat Smelting Co | Improvements in or relating to aluminium base alloys |
FR1322510A (en) * | 1962-05-02 | 1963-03-29 | Aluminum Co Of America | Improvement of articles in aluminum-based alloy obtained by heat treatment |
FR2113037A5 (en) * | 1970-10-23 | 1972-06-23 | Fuchs Otto |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2640644A1 (en) * | 1988-12-19 | 1990-06-22 | Pechiney Recherche | PROCESS FOR THE "SPRAY-DEPOSITION" PRODUCTION OF 7000 SER AL ALLOYS AND DISCONTINUOUS REINFORCED COMPOSITE MATERIALS HAVING HIGH MECHANICAL RESISTANCE AND GOOD DUCTILITY AS MATRIX |
EP0375571A1 (en) * | 1988-12-19 | 1990-06-27 | PECHINEY RECHERCHE (Groupement d'Intérêt Economique régi par l'ordonnance du 23 Septembre 1967) | Process for the preparation by spray deposits of aluminium alloys of the 7000 series, and discontinuously reinforced composite materials having these high strength, highly ductile alloys as a matrix |
WO1994024326A1 (en) * | 1993-04-15 | 1994-10-27 | Alcan International Limited | Method of making hollow bodies |
US5932037A (en) * | 1993-04-15 | 1999-08-03 | Luxfer Group Limited | Method of making hollow bodies |
EP0670377A1 (en) * | 1994-03-02 | 1995-09-06 | Pechiney Recherche (Gie) | High-strength aluminium alloy 7000 and manufacturing process |
FR2716896A1 (en) * | 1994-03-02 | 1995-09-08 | Pechiney Recherche | 7000 alloy with high mechanical strength and process of obtaining. |
EP1464719A1 (en) * | 1994-03-02 | 2004-10-06 | Pechiney Rhenalu | High strength aluminium 7000 alloy and process for production |
WO2003085146A1 (en) | 2002-04-05 | 2003-10-16 | Pechiney Rhenalu | Al-zn-mg-cu alloys welded products with high mechanical properties, and aircraft structural elements |
Also Published As
Publication number | Publication date |
---|---|
NO801611L (en) | 1980-12-02 |
CA1118190A (en) | 1982-02-16 |
EP0020282B1 (en) | 1982-12-29 |
US4345951A (en) | 1982-08-24 |
FR2457908B1 (en) | 1984-03-02 |
DE3061495D1 (en) | 1983-02-03 |
ES491989A0 (en) | 1980-12-16 |
NO153184C (en) | 1986-01-29 |
IT8022416A0 (en) | 1980-05-29 |
FR2457908A1 (en) | 1980-12-26 |
IT1130700B (en) | 1986-06-18 |
BE883565A (en) | 1980-12-01 |
CH644402A5 (en) | 1984-07-31 |
NO153184B (en) | 1985-10-21 |
ES8102198A1 (en) | 1980-12-16 |
ZA803235B (en) | 1981-05-27 |
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