EP0259232A1 - Easily workable and weldable aluminium alloy, and process for its manufacture - Google Patents
Easily workable and weldable aluminium alloy, and process for its manufacture Download PDFInfo
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- EP0259232A1 EP0259232A1 EP87420190A EP87420190A EP0259232A1 EP 0259232 A1 EP0259232 A1 EP 0259232A1 EP 87420190 A EP87420190 A EP 87420190A EP 87420190 A EP87420190 A EP 87420190A EP 0259232 A1 EP0259232 A1 EP 0259232A1
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- C22C21/08—Alloys based on aluminium with magnesium as the next major constituent with silicon
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- the invention relates to a weldable boilermaking aluminum alloy containing essentially Si, Mg and Cu and to its manufacturing process.
- alloys of the 6000 series according to the nomenclature of the Aluminum Association have been developed essentially in the form of profiles, although some of these alloys such as 6061 or 6082, are commonly found in the form of sheets or strips, intended for the stamping.
- Patent application FR 2 375 332 describes a process in which an alloy rich in Si is treated so as to obtain a fine sub-micron precipitation (0.1 to 0.5 ⁇ m) of Si in supersaturation; this size is intermediate between the eutectic phases present in the alloy and that of the hardening phases usually observed in Al-Si-Mg-Cu alloys.
- French patent application FR 2 360 684 describes an Al-Si-Mg-Cu alloy containing at least one of the recrystallization inhibiting elements from the group Mn, Cr, Zr.
- Mn in particular has several drawbacks: . 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.
- the alloy comprises (in% by weight) contents of Si and Mg defined by the trapezoid of coordinates: Cu 0.1 - 0.5 Mn 0 - 0.2 Ti 0 - 0.1 Fe 0 - 0.35 others each ⁇ 0.05 total ⁇ 0.15 remains Al.
- the maximum Si / Mg ratio (BC side of the trapezoid) remains equal to or greater than 2.6 approximately so as to limit the precipitation of Mg2Si during solidification as much as possible.
- the fine precipitation Mg2Si present in the alloy results only from the heat treatments undergone.
- the secondary elements are limited for the following reasons: As explained above, the presence of Mn is not desirable; however, it has been admitted up to 0.2% maximum due to possible contamination in this element, due to the recycling of waste. It should be noted that the alloy does not contain intentional additions of Cr and / or Zr.
- the Ti associated with B controls, as is known, the fineness of the primary crystallization of the raw casting products (plates, strips, billets, etc.) and allows shorter homogenizations and solutions, in particular in which concerns the processing of flat products (sheets, strips).
- the effective contents are Ti ⁇ 0.1% and B ⁇ 0.05%.
- the Fe content is limited to 0.35% to avoid the formation of coarse primary compounds containing Fe (AlMnFeSi type).
- the range of manufacturing of the alloys according to the invention generally comprises the continuous or semi-continuous casting of blanks, possible homogenization, hot transformation, possible cold transformation, dissolution and tempering.
- homogenization at high temperature between 550 ° C and 570 ° C with a holding time of 6 to 24 hours is desirable. Homogenization is preferably preceded by a slow rise in temperature.
- the hot transformation is carried out by any known means (rolling, spinning, forging, etc.). However, this must then be carried out so as to avoid coarse recrystallizations during operation. In the case of sheets and strips, these coarse hot recrystallizations are the source of macroscopic deformation lines, visible after stamping, therefore unacceptable for this application.
- the temperature at the end of hot transformation to avoid these recrystallizations, must imperatively be between 270 ° and 340 ° C.
- the alloy After possible cold transformation, the alloy is put into a complete solution. This takes place in the temperature range between 540 and 580 ° C, preferably between 550 and 570 ° C, targeting the temperature of 560 ° C.
- the temperature rise before dissolving must be rapid (V ⁇ 10 ° C / sec) and dissolving preferably carried out either in a 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 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 the complex AlCuMg, AlCuMg Si phases. Tempering is typically carried out between 8 to 12 h at 165 ° C.
- FIG. 1 represents the field of composition of the elements Si and Mg of the alloy
- FIG. 2 represents the field of dissolution or homogenization of an alloy according to the invention, on a vertical section of the state diagram Al, Mg, Si at 0.2% Mg.
- Dissolution (or homogenization) must be carried out in the single-phase field and in particular under the temperature conditions represented by the rectangle FGHI for the general range and F'G'H'I 'for the preferred range.
- This heat treatment therefore requires a precise industrial tool.
- the dissolution of these was carried out in a passage oven at a speed of 20 m / min, the time for keeping at temperature of 560 ° C. being of the order of 1 minute and the speed of temperature rise about 25 ° C / sec.
- the anisotropy was estimated by making buckets and measuring the rate of the horns according to the AFNOR NF-A-50-301 standard. This value is equal to 7%.
- the grain size measured by metallography is 40 ⁇ m.
- Sheets cut from the dissolved metal were finished by shaping parts of the automobile body, in this case a front cover.
- Example 1 A sheet of the same composition as that of Example 1 was welded to another sheet of the same composition by spot welding, under the following conditions: "Mallory 328" tapered electrode with apex angle 60 ° and pellet diameter ⁇ 5.5 mm. Support force: 400 kg Intensity: 27,000 A Frequency: 2 Hz.
- the assembly was then brought, in an oven, to 165 ° C for 10 h.
- the shear strength of the welded joints thus obtained is of the order of 280 MPa. We can see the good properties obtained after welding and tempering.
- the alloy according to the invention has the following advantages: This alloy is delivered in T4 state to transformers. In this state, the alloy is ductile and lends itself well to deformation, its maturation at ambient temperature being very low. The cold deformed part acquires better resistance characteristics by work hardening, at least locally in the most deformed zones; the softening due to annealing during the welding operation is partially offset by the structural hardening during the final tempering (T6).
- the metal undergoes after quenching only the finishing operations (such as dressing, leveling, etc.) which are strictly necessary.
- the alloys according to the invention are mainly used in the fields of automobile bodywork and casing.
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Abstract
L'invention se rapporte à un alliage d'aluminium de chaudronnerie, soudable, contenant essentiellement du Si, du Mg et du Cu et son procédé de fabrication. Cet alliage comprent (en poids %) des teneurs en Si et Mg définies par le trapèze de coordonnées : <IMAGE> Cu : 0,1 - 0,5 Mn : 0 - 0,2 Ti : 0 - 0,1 Fe : 0 - 0,35 Autres chacun : <= 0,05 Total <= 0,15 Reste Al. La gamme de fabrication comporte la coulée semi-continue ou continue d'ébauches, une homogénéisation éventuelle, une transformation à chaud terminée dans le domaine 270°C-340°C, une transformation à froid éventuelle, une mise en solution complète, une mise en forme par emboutissage, pliage, cintrage, etc...et un revenu.The invention relates to a weldable boilermaking aluminum alloy containing essentially Si, Mg and Cu and its manufacturing process. This alloy includes (by weight%) Si and Mg contents defined by the trapezoid of coordinates: <IMAGE> Cu: 0.1 - 0.5 Mn: 0 - 0.2 Ti: 0 - 0.1 Fe: 0 - 0.35 Others each: <= 0.05 Total <= 0.15 Rest Al. The manufacturing range includes semi-continuous or continuous casting of blanks, possible homogenization, hot transformation completed in the field 270 ° C-340 ° C, a possible cold transformation, a complete solution, a shaping by stamping, bending, bending, etc ... and an income.
Description
L'invention se rapporte à un alliage d'aluminium de chaudronnerie, soudable, contenant essentiellement du Si, du Mg et du Cu et à son procédé de fabrication.The invention relates to a weldable boilermaking aluminum alloy containing essentially Si, Mg and Cu and to its manufacturing process.
Les alliages de la série 6000 selon la nomenclature de l'Aluminium Association ont été développés essentiellement sous forme de profilés, bien que certains de ces alliages tel que le 6061 ou le 6082, se trouvent couramment sous forme de tôles ou bandes, destinées à l'emboutissage.The alloys of the 6000 series according to the nomenclature of the Aluminum Association have been developed essentially in the form of profiles, although some of these alloys such as 6061 or 6082, are commonly found in the form of sheets or strips, intended for the stamping.
Des alliages entrant dans cette famille ont été décrits dans les brevets français FR-A-2 375 332 et FR-A-2 360 684.
Ces alliages, moins chargés en magnésium que les alliages 6000 classiques, peu éloignées de la stoéchiométrie Mg₂Si, sont par contre beaucoup plus riches en silicium.Alloys belonging to this family have been described in French patents FR-A-2,375,332 and FR-A-2,360,684.
These alloys, less loaded with magnesium than the conventional 6000 alloys, not far from the Mg₂Si stoichiometry, are on the other hand much richer in silicon.
La demande de brevet FR 2 375 332 décrit un procédé dans lequel un alliage riche en Si est traité de façon à obtenir une fine précipitation sub-micronique (0,1 à 0,5 µm) de Si en sursaturation; cette taille est intermédiaire entre le phases eutectiques présentes dans l'alliage et celle des phases durcissantes habituellement observées dans les alliages Al-Si-Mg-Cu.
Cette précipitation de Si, si elle présente selon les auteurs un certain nombre d'avantages, a également quelques inconvénients.This precipitation of Si, if it presents according to the authors a certain number of advantages, also has some disadvantages.
En effet, les précipités au silicium trop importants réduisent les capacités de déformation du matériau et de plus la résistance à la corrosion de l'alliage dans ses conditions d'emploi est affaiblie par leur présence.In fact, excessively large silicon precipitates reduce the deformation capacities of the material and, moreover, the corrosion resistance of the alloy under its conditions of use is weakened by their presence.
La demande de brevet français FR 2 360 684 décrit un alliage Al-Si- Mg-Cu contenant au moins l'un des éléments inhibiteurs de recristallisation du groupe Mn, Cr, Zr.French
Cependant, la présence de ces derniers éléments n'est pas favorable. Le Mn en particulier présente plusieurs inconvénients :
. 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 le 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.However, the presence of these latter elements is not favorable. Mn in particular has several drawbacks:
. 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.Cr and Zr have effects similar to those of Mn.
Le problème qui se pose à l'homme de l'art est donc l'obtention d'un alliage Al-Si-Mg-Cu emboutissable et soudable, exempt des inconvénients signalés ci-dessus et qui présente des propriétés mécaniques satisfaisantes à l'état durci, une bonne aptitude à la déformation à froid à l'état trempé, une bonne résistance à la corrosion et ce à la suite d'un traitement thermique simple, qui exclut la présence de toute précipitation de phase submicronique essentiellement constituée de Si.The problem which presents itself to a person skilled in the art is therefore obtaining a stampable and weldable Al-Si-Mg-Cu alloy, free from the drawbacks mentioned above and which has satisfactory mechanical properties when hardened state, good capacity for cold deformation in the quenched state, good resistance to corrosion and this following a simple heat treatment, which excludes the presence of any precipitation of submicron phase essentially consisting of Si.
Selon l'invention, l'alliage comprend (en % en poids) des teneurs en Si et Mg définies par le trapèze de coordonnées :
Mn 0 - 0,2
Ti 0 - 0,1
Fe 0 - 0,35
autres chacun ≦ 0,05
total ≦ 0,15
reste Al.According to the invention, the alloy comprises (in% by weight) contents of Si and Mg defined by the trapezoid of coordinates:
Mn 0 - 0.2
Ti 0 - 0.1
Fe 0 - 0.35
others each ≦ 0.05
total ≦ 0.15
remains Al.
Au-dessous des valeurs minimales des éléments principaux (Si, Mg, Cu) les caractéristiques mécaniques désirées à l'état traité ne sont pas atteintes.Below the minimum values of the main elements (Si, Mg, Cu) the desired mechanical characteristics in the treated state are not reached.
Pour Si ≧ 1,3 % le traitement thermique de mise en solution complète est difficile à appliquer industriellement, comme cela sera exposé ci-après.For Si ≧ 1.3%, the heat treatment for complete solution is difficult to apply industrially, as will be explained below.
Pour Mg ≧ 0,5 %, des difficultés lors de la transformation à chaud apparaissent (fragilisation) et l'aptitude à l'emboutissage est réduite.For Mg ≧ 0.5%, difficulties during hot processing appear (embrittlement) and the ability to stamp is reduced.
On peut aussi observer que le rapport Si/Mg maximum (côté BC du trapèze) reste égal ou supérieur à 2,6 environ de manière à limiter au maximum la précipitation de Mg₂Si en cours de solidification. Ainsi, les fines précipitations Mg₂Si présentes dans l'alliage ne résultent que des traitements thermiques subis.It can also be observed that the maximum Si / Mg ratio (BC side of the trapezoid) remains equal to or greater than 2.6 approximately so as to limit the precipitation of Mg₂Si during solidification as much as possible. Thus, the fine precipitation Mg₂Si present in the alloy results only from the heat treatments undergone.
Pour Cu ≧ 0,5 %, la résistance à la corrosion ainsi que l'aptitude à l'emboutissage sont réduites.For Cu ≧ 0.5%, the corrosion resistance as well as the drawing ability are reduced.
Les éléments secondaires sont limités pour les raisons suivantes : Comme explicité ci-dessus, la présence de Mn n'est pas souhaitable; cependant, elle a été admise jusqu'à 0,2 % maximum en raison des contaminations éventuelles en cet élément, dues au recyclage des déchets. Il est à noter que l'alliage ne comporte pas d'additions intentionnelles de Cr et/ou Zr.The secondary elements are limited for the following reasons: As explained above, the presence of Mn is not desirable; however, it has been admitted up to 0.2% maximum due to possible contamination in this element, due to the recycling of waste. It should be noted that the alloy does not contain intentional additions of Cr and / or Zr.
Le Ti associé au B contrôle, comme cela est connu, la finesse de la cristallisation primaire des produits bruts de coulée (plaques, bandes, billettes, etc...) et permet des homogénéisations et mises en solution plus courtes, en particulier en ce qui concerne le traitement des produits plats (tôles, bandes). Les teneurs efficaces sont Ti < 0,1 % et B < 0,05 %. La teneur en Fe est limitée à 0,35 % pour éviter la formation de composés primaires grossiers contenant de Fe (type AlMnFeSi).The Ti associated with B controls, as is known, the fineness of the primary crystallization of the raw casting products (plates, strips, billets, etc.) and allows shorter homogenizations and solutions, in particular in which concerns the processing of flat products (sheets, strips). The effective contents are Ti <0.1% and B <0.05%. The Fe content is limited to 0.35% to avoid the formation of coarse primary compounds containing Fe (AlMnFeSi type).
Une composition préférentielle de l'alliage suivant l'invention (% en poids) est la suivante, teneur en Si et Mg comprises dans le trapèze ayant pour sommet :
Mn = 0-0,15
Ti = 0 - 0,1
Fe 0 - 0,3
autres chacun ≦ 0,05
total ≦ 0,15
rest Al.A preferred composition of the alloy according to the invention (% by weight) is as follows, content of Si and Mg included in the trapezium having for apex:
Mn = 0-0.15
Ti = 0 - 0.1
Fe 0 - 0.3
others each ≦ 0.05
total ≦ 0.15
rest Al.
La gamme de fabrication des alliages suivant l'invention comporte généralement 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 range of manufacturing of the alloys according to the invention generally comprises the 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, en particulier une finesse de grain inférieure à 80 um en moyenne, ces opérations doivent être conduites dans des conditions assez étroites.However, to obtain good properties of the alloy, in particular a fineness of grain of less than 80 µm on average, 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 de phases eutectiques. Une homogénéisation à haute température entre 550°C et 570°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 eutectic phases. Homogenization at high temperature between 550 ° C and 570 ° C with a holding time of 6 to 24 hours is desirable. Homogenization is preferably preceded by a slow rise in temperature.
La transformation à chaud est effectuée par tout moyen connu (laminage, filage, forgeage, etc...). Cependant, celle-ci doit ensuite être conduite de façon à éviter des recristallisations grossières en cours d'opération. Dans le cas des tôles et bandes, ces recristallisations à chaud grossières sont la source de lignes de déformations macroscopiques, visibles après emboutissage, donc rédhibitoires pour cette application.The hot transformation is carried out by any known means (rolling, spinning, forging, etc.). However, this must then be carried out so as to avoid coarse recrystallizations during operation. In the case of sheets and strips, these coarse hot recrystallizations 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 340°C.Therefore, the temperature at the end of hot transformation, to avoid these recrystallizations, must imperatively be between 270 ° and 340 ° C.
Après transformation à froid éventuelle l'alliage est mis en solution complète. Celle-ci a lieu dans le domaine de température compris entre 540 et 580°C, de préférence entre 550 et 570°C, en visant la température de 560°C.After possible cold transformation, the alloy is put into a complete solution. This takes place in the temperature range between 540 and 580 ° C, preferably between 550 and 570 ° C, targeting the temperature of 560 ° C.
Compte tenu de l'absence volontaire d'éléments inhibiteurs de recristallisation (Mn,Cr,Zr), 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.Taking into account the voluntary absence of recrystallization inhibiting elements (Mn, Cr, Zr), the temperature rise before dissolving must be rapid (V ≧ 10 ° C / sec) and dissolving preferably carried out either in a 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 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 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, les pièces subissent un revenu de durcissement, dans les conditons habituelles; le durcissement est dû à la précipitation de la phase Mg₂Si et de phases complexes AlCuMg, AlCuMg Si. Le revenu est typiquement effectué entre 8 à 12 h vers 165°C.After the cold forming operations such as stamping, bending, bending, etc. and / or assembly such as welding, the parts undergo hardening income, under the usual conditions; the hardening is due to the precipitation of the Mg₂Si phase and of the complex AlCuMg, AlCuMg Si phases. Tempering is typically carried out between 8 to 12 h at 165 ° C.
Il est à remarquer que dans certains cas, la cuisson de revêtements de surface tels que des vernis, bien que plus courte, réalise ipso facto ce traitement.It should be noted that in certain cases, the baking of surface coatings such as varnishes, although shorter, ipso facto performs this treatment.
L'invention sera mieux comprise à l'aide des exemples suivants illustrés par la figure 1 que représente le domaine de composition des éléments Si et Mg de l'alliage, et la figure 2 qui représente le domaine de mise en solution ou d'homogénéisation d'un alliage suivant l'invention, sur une coupe verticale du diagramme d'état Al, Mg, Si à 0,2 % Mg.The invention will be better understood with the aid of the following examples illustrated by FIG. 1 which represents the field of composition of the elements Si and Mg of the alloy, and FIG. 2 which represents the field of dissolution or homogenization of an alloy according to the invention, on a vertical section of the state diagram Al, Mg, Si at 0.2% Mg.
Sur la figure 2, on trouve en (1) la courbe solvus, en (2) la courbe solidus et en (3) le palier eutectique, qui se regroupent au point E.In Figure 2, we find in (1) the solvus curve, in (2) the solidus curve and in (3) the eutectic plateau, which are grouped at point E.
La mise en solution (ou homogénéisation) doit être effectuée dans le domaine monophasé et en particulier dans les conditions de température représentées par le rectangle FGHI pour la plage générale et F'G'H'I' pour la plage préférentielle.Dissolution (or homogenization) must be carried out in the single-phase field and in particular under the temperature conditions represented by the rectangle FGHI for the general range and F'G'H'I 'for the preferred range.
Il est évident, d'après ces courbes, que pour les teneurs en Si élevées, le traitement est délicat, puisqu'une faible variation par rapport à la température de consigne conduit soit à une précipitation de Si si la température baisse, soit à une "brûlure" du métal si la température monte.It is obvious from these curves that for high Si contents, the treatment is delicate, since a slight variation with respect to the set temperature leads either to a precipitation of Si if the temperature drops, or to a "burning" of the metal if the temperature rises.
Ce traitement thermique exige donc un outil industriel précis.This heat treatment therefore requires a precise industrial tool.
Une plaque (1500x400 mm²) de composition suivante (% en poids ) : Si 0,90; Mg 0,30; Cu 0,20; Fe 0,25; Ti 0,03, a été coulée par le procédé classique en semi-continu. Cette plaque a été homogénéisée 10 h à 555°C (scalpée à 1500 x 420 mm²) puis laminée à chaud jusqu'à 4 mm d'épaisseur avec finition entre 320 et 300°C. Les bobines ainsi obtenues ont été laminées à froid jusqu'à 1,25 mm d'épaisseur.A plate (1500x400 mm²) of the following composition (% by weight): Si 0.90; Mg 0.30; Cu 0.20; Fe 0.25; Ti 0.03, was cast by the conventional semi-continuous process. This plate was homogenized for 10 h at 555 ° C (scalped to 1500 x 420 mm²) then hot rolled to 4 mm thick with finishing between 320 and 300 ° C. The coils thus obtained were cold rolled to 1.25 mm thick.
La mise en solution de celles-ci a été effectuée dans un four à passage à la vitesse de 20 m/mn, le temps de maintien à température de 560°C étant de l'ordre de 1 minute et la vitesse de montée en température de l'ordre de 25°C/sec.The dissolution of these was carried out in a passage oven at a speed of 20 m / min, the time for keeping at temperature of 560 ° C. being of the order of 1 minute and the speed of temperature rise about 25 ° C / sec.
Les caractéristiques mécaniques mesurées dans la direction du laminage, dans le sens travers et suivant la direction à 45° de la direction du laminage sont rassemblées dans le Tableau suivant :
Ces mesures montrent que le produit obtenu est relativement homogène et isotrope.These measurements show that the product obtained is relatively homogeneous and isotropic.
L'anisotropie a été estimée en réalisant des godets et en mesurant le taux des cornes suivant la norme AFNOR NF-A-50-301. Cette valeur est égale à 7 %. La grosseur de grain mesurée par métallographie est de 40 µm.The anisotropy was estimated by making buckets and measuring the rate of the horns according to the AFNOR NF-A-50-301 standard. This value is equal to 7%. The grain size measured by metallography is 40 µm.
De tôles découpées dans le métal mis en solution ont été parachevées par mise en forme de parties de carrosserie automobile, dans ce cas un capot avant.Sheets cut from the dissolved metal were finished by shaping parts of the automobile body, in this case a front cover.
Après emboutissage, celui-ci a été revêtu d'un revêtement protection (peinture) avant de subir une cuisson de 1,5 h à 180°C.After stamping, it was coated with a protective coating (paint) before being baked for 1.5 h at 180 ° C.
Les caractéristiques mécaniques obtenues en fonction du taux d'écrouissage local sont les suivantes :
Une tôle de même composition que celle de l'exemple 1 a été soudée à une autre tôle de même composition par soudure par point, dans les conditions suivantes :
Electrode en "Mallory 328" de forme tronconique avec angle au sommet de 60° et diamètre de pastille ⌀ 5,5 mm.
Force d'appui : 400 kg
Intensité : 27 000 A
Fréquence : 2 Hz.A sheet of the same composition as that of Example 1 was welded to another sheet of the same composition by spot welding, under the following conditions:
"Mallory 328" tapered electrode with apex angle 60 ° and pellet diameter ⌀ 5.5 mm.
Support force: 400 kg
Intensity: 27,000 A
Frequency: 2 Hz.
L'assemblage a été ensuite porté, en étuve, à 165°C pendant 10 h.
La résistance au cisaillement des joints soudés ainsi obtenus est de l'ordre de 280 MPa.
On peut constater les bonnes propriétés obtenues après soudage et revenu.The assembly was then brought, in an oven, to 165 ° C for 10 h.
The shear strength of the welded joints thus obtained is of the order of 280 MPa.
We can see the good properties obtained after welding and tempering.
L'alliage suivant l'invention présente les avantages suivants :
Cet alliage est livré à l'état T4 aux transformateurs.
A cet état, l'alliage est ductile et se prête bien à la déformation, sa maturation à la température ambiante étant très faible.
La pièce déformée à froid acquiert de meilleures caractéristiques de résistance par écrouissage, au moins localement dans les zones les plus déformées; l'adoucissement dû au recuit lors de l'opération de soudage est partiellement compensé par le durcissement structural lor du revenu final (T6).The alloy according to the invention has the following advantages:
This alloy is delivered in T4 state to transformers.
In this state, the alloy is ductile and lends itself well to deformation, its maturation at ambient temperature being very low.
The cold deformed part acquires better resistance characteristics by work hardening, at least locally in the most deformed zones; the softening due to annealing during the welding operation is partially offset by the structural hardening during the final tempering (T6).
Pour obtenir l'état le plus ductile, le métal ne subit après trempe que les opérations de finition (telles que dressage, planage, etc...) strictement nécessaires.To obtain the most ductile state, the metal undergoes after quenching only the finishing operations (such as dressing, leveling, etc.) which are strictly necessary.
Les alliages selon l'invention sont principalement utilisés dans les domaines de la carrosserie automobile et du boîtage.The alloys according to the invention are mainly used in the fields of automobile bodywork and casing.
Claims (9)
Mn 0-0,2
Fe 0-0,35
autres chacun ≦ 0,05
Total ≦ 0,15
reste Al.1. A cauldronable and weldable aluminum alloy characterized in that it contains (by weight%) Si and Mg contents delimited by the trapezoid ABCD whose coordinates are: Cu 0.1 -0.5
Mn 0-0.2
Fe 0-0.35
others each ≦ 0.05
Total ≦ 0.15
remains Al.
Mn ≦ 0,15.2. Alloy according to claim 1, characterized in that it contains (in% by weight) contents of Si and Mg delimited by the trapezoid A'B'C'D 'whose coordinates are: Cu 0.1-0.25
Mn ≦ 0.15.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT87420190T ATE64763T1 (en) | 1986-07-07 | 1987-07-02 | WELL MACHINABLE AND WELDABLE ALUMINUM ALLOY AND PROCESS FOR THEIR PRODUCTION. |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8610028A FR2601040B1 (en) | 1986-07-07 | 1986-07-07 | SOLDERABLE AND WELDABLE ALUMINUM ALLOY AND MANUFACTURING METHOD THEREOF |
FR8610028 | 1986-07-07 | ||
CA000552025A CA1340260C (en) | 1986-07-07 | 1987-11-17 | Formable and weldable aluminum alloy, process for producing the same |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0259232A1 true EP0259232A1 (en) | 1988-03-09 |
EP0259232B1 EP0259232B1 (en) | 1991-06-26 |
EP0259232B2 EP0259232B2 (en) | 1998-01-28 |
Family
ID=25671592
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP87420190A Expired - Lifetime EP0259232B2 (en) | 1986-07-07 | 1987-07-02 | Easily workable and weldable aluminium alloy, and process for its manufacture |
Country Status (7)
Country | Link |
---|---|
US (1) | US4814022A (en) |
EP (1) | EP0259232B2 (en) |
CA (1) | CA1340260C (en) |
DE (1) | DE3771017D1 (en) |
ES (1) | ES2022918T5 (en) |
FR (1) | FR2601040B1 (en) |
GR (2) | GR3002191T3 (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1995014113A1 (en) * | 1993-11-17 | 1995-05-26 | Pechiney Rhenalu | Aluminium-silicon-magnesium alloy having improved ductility and deep-drawing properties, and method for producing same |
WO1995031580A1 (en) * | 1994-05-11 | 1995-11-23 | Aluminum Company Of America | Corrosion resistant aluminum alloy rolled sheet |
EP0714993A1 (en) * | 1994-11-29 | 1996-06-05 | Alusuisse-Lonza Services AG | Deep drawable and weldable AlMgSi type aluminium alloy |
EP0811700A1 (en) * | 1996-06-04 | 1997-12-10 | Alusuisse Technology & Management AG | Deep drawable and weldable AlMgSi type aluminium alloy |
WO1998014626A1 (en) * | 1996-09-30 | 1998-04-09 | Alcan International Limited | Aluminium alloy for rolled product process |
WO2013030469A1 (en) | 2011-09-02 | 2013-03-07 | Constellium France | Clad sheet for motor vehicle body |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB9318041D0 (en) * | 1993-08-31 | 1993-10-20 | Alcan Int Ltd | Extrudable a1-mg-si alloys |
US5919323A (en) * | 1994-05-11 | 1999-07-06 | Aluminum Company Of America | Corrosion resistant aluminum alloy rolled sheet |
US5582660A (en) * | 1994-12-22 | 1996-12-10 | Aluminum Company Of America | Highly formable aluminum alloy rolled sheet |
DE69620771T3 (en) * | 1995-09-19 | 2006-04-27 | Alcan International Ltd., Montreal | Use of rolled aluminum alloys for structural parts of vehicles |
FR2748035B1 (en) * | 1996-04-29 | 1998-07-03 | Pechiney Rhenalu | ALUMINUM-SILICON-MAGNESIUM ALLOY FOR AUTOMOTIVE BODYWORK |
US6780259B2 (en) * | 2001-05-03 | 2004-08-24 | Alcan International Limited | Process for making aluminum alloy sheet having excellent bendability |
FR2835533B1 (en) * | 2002-02-05 | 2004-10-08 | Pechiney Rhenalu | AL-Si-Mg ALLOY SHEET FOR AUTOMOTIVE BODY SKIN |
US6959476B2 (en) * | 2003-10-27 | 2005-11-01 | Commonwealth Industries, Inc. | Aluminum automotive drive shaft |
DE202011110888U1 (en) | 2011-11-11 | 2017-01-24 | Novelis Inc. | aluminum alloy |
EP2592165B2 (en) | 2011-11-11 | 2018-09-19 | Novelis, Inc. | Aluminium alloy |
RU2596509C2 (en) | 2011-11-11 | 2016-09-10 | Новелис Инк. | Aluminium alloy |
WO2020185920A1 (en) | 2019-03-13 | 2020-09-17 | Novelis Inc. | Age-hardenable and highly formable aluminum alloys, monolithic sheet made therof and clad aluminum alloy product comprising it |
Citations (5)
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US3149001A (en) * | 1962-04-05 | 1964-09-15 | Aluminum Co Of America | Enameled aluminous metal product |
US3370943A (en) * | 1965-11-04 | 1968-02-27 | Kaiser Aluminium Chem Corp | Aluminum alloy |
FR2360684A1 (en) * | 1976-08-05 | 1978-03-03 | Aluminum Co Of America | IMPROVED ALUMINUM STRUCTURAL ELEMENTS, FOR MOTOR VEHICLES |
FR2375332A1 (en) * | 1976-12-24 | 1978-07-21 | Alusuisse | MANUFACTURING PROCESS OF WELL TRANSFORMABLE ALUMINUM SHEETS, POOR IN HORNS AND OF HIGH MECHANICAL STRENGTH |
FR2446865A1 (en) * | 1979-01-16 | 1980-08-14 | Pechiney Aluminium | Wrought aluminium alloy with high tensile strength - where amts. of minor elements are controlled to obtain very high notch toughness |
-
1986
- 1986-07-07 FR FR8610028A patent/FR2601040B1/en not_active Expired
-
1987
- 1987-06-30 US US07/068,118 patent/US4814022A/en not_active Expired - Lifetime
- 1987-07-02 DE DE8787420190T patent/DE3771017D1/en not_active Expired - Lifetime
- 1987-07-02 ES ES87420190T patent/ES2022918T5/en not_active Expired - Lifetime
- 1987-07-02 EP EP87420190A patent/EP0259232B2/en not_active Expired - Lifetime
- 1987-11-17 CA CA000552025A patent/CA1340260C/en not_active Expired - Fee Related
-
1991
- 1991-06-27 GR GR90401165T patent/GR3002191T3/en unknown
-
1998
- 1998-02-12 GR GR980400273T patent/GR3026104T3/en unknown
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3149001A (en) * | 1962-04-05 | 1964-09-15 | Aluminum Co Of America | Enameled aluminous metal product |
US3370943A (en) * | 1965-11-04 | 1968-02-27 | Kaiser Aluminium Chem Corp | Aluminum alloy |
FR2360684A1 (en) * | 1976-08-05 | 1978-03-03 | Aluminum Co Of America | IMPROVED ALUMINUM STRUCTURAL ELEMENTS, FOR MOTOR VEHICLES |
FR2375332A1 (en) * | 1976-12-24 | 1978-07-21 | Alusuisse | MANUFACTURING PROCESS OF WELL TRANSFORMABLE ALUMINUM SHEETS, POOR IN HORNS AND OF HIGH MECHANICAL STRENGTH |
FR2446865A1 (en) * | 1979-01-16 | 1980-08-14 | Pechiney Aluminium | Wrought aluminium alloy with high tensile strength - where amts. of minor elements are controlled to obtain very high notch toughness |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1995014113A1 (en) * | 1993-11-17 | 1995-05-26 | Pechiney Rhenalu | Aluminium-silicon-magnesium alloy having improved ductility and deep-drawing properties, and method for producing same |
FR2713664A1 (en) * | 1993-11-17 | 1995-06-16 | Pechiney Rhenalu | Al-Si-Mg type alloy with improved ductility and drawability and method of production. |
WO1995031580A1 (en) * | 1994-05-11 | 1995-11-23 | Aluminum Company Of America | Corrosion resistant aluminum alloy rolled sheet |
EP0714993A1 (en) * | 1994-11-29 | 1996-06-05 | Alusuisse-Lonza Services AG | Deep drawable and weldable AlMgSi type aluminium alloy |
CH688379A5 (en) * | 1994-11-29 | 1997-08-29 | Alusuisse Lonza Services Ag | Thermaformed and weldable aluminum alloy of the AlMgSi type |
EP0811700A1 (en) * | 1996-06-04 | 1997-12-10 | Alusuisse Technology & Management AG | Deep drawable and weldable AlMgSi type aluminium alloy |
CH690916A5 (en) * | 1996-06-04 | 2001-02-28 | Alusuisse Tech & Man Ag | Thermaformed and weldable aluminum alloy of the AlMgSi type. |
WO1998014626A1 (en) * | 1996-09-30 | 1998-04-09 | Alcan International Limited | Aluminium alloy for rolled product process |
WO2013030469A1 (en) | 2011-09-02 | 2013-03-07 | Constellium France | Clad sheet for motor vehicle body |
Also Published As
Publication number | Publication date |
---|---|
ES2022918B3 (en) | 1991-12-16 |
EP0259232B2 (en) | 1998-01-28 |
FR2601040B1 (en) | 1988-09-02 |
GR3002191T3 (en) | 1992-12-30 |
FR2601040A1 (en) | 1988-01-08 |
GR3026104T3 (en) | 1998-05-29 |
DE3771017D1 (en) | 1991-08-01 |
ES2022918T5 (en) | 1998-03-16 |
US4814022A (en) | 1989-03-21 |
EP0259232B1 (en) | 1991-06-26 |
CA1340260C (en) | 1998-12-15 |
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