EP0142405A1 - Work pieces made from aluminium alby powder, and process for manufacturing it - Google Patents

Work pieces made from aluminium alby powder, and process for manufacturing it Download PDF

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Publication number
EP0142405A1
EP0142405A1 EP84401982A EP84401982A EP0142405A1 EP 0142405 A1 EP0142405 A1 EP 0142405A1 EP 84401982 A EP84401982 A EP 84401982A EP 84401982 A EP84401982 A EP 84401982A EP 0142405 A1 EP0142405 A1 EP 0142405A1
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Prior art keywords
powder
blank
aluminum alloy
density
aluminium
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EP84401982A
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German (de)
French (fr)
Inventor
Christian De Beaulieu
Claude Castellani
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Renault SAS
Regie Nationale des Usines Renault
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Renault SAS
Regie Nationale des Usines Renault
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Publication of EP0142405A1 publication Critical patent/EP0142405A1/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/17Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces by forging
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/0408Light metal alloys
    • C22C1/0416Aluminium-based alloys

Definitions

  • the present invention relates to a process for obtaining mechanical parts produced from aluminum alloy powders and undergoing a forging operation.
  • Aluminum alloys are of interest in mechanical parts for their low density, their better machinability, their better thermal conductivity; compared to the usual techniques of forging and foundry, powder metallurgy is likely to bring about a reduction in material losses between the raw part f and the finished part (reduction in the weight per thousand of material) and a reduction in costs machining.
  • This process thus has the drawback of obtaining a mechanical part with low characteristics and a low final density.
  • this process requires heat treatment with extremely precise temperature control.
  • Another method consists in starting with a pre-alloyed powder, that is to say in which each grain of powder is homogeneous in composition of the alloy; the alumina film then remains and cannot be removed since it is no longer possible to sinter in the presence of a liquid phase; we are then obliged to encapsulate the powder before forging, then to eliminate the capsule; a strong wrought breaks the alumina films and allows the powder grains to weld; it is then possible to achieve properties close to that of rolled and forged metal; this technique remains relatively complex, expensive and applicable only in small series.
  • the purpose of the process according to the invention is to obtain mechanical parts with high characteristics, by a simple and inexpensive route, capable of mass production.
  • the mechanical part in powder of pre-alloyed aluminum alloy is characterized by the presence of a homogeneous matrix of aluminum alloy with a very fine structure whose grain size is the same order of magnitude as that of the initial powder grains, and the interfaces of which are marked by a very fine network of precipitates, said part having a density equal to 100% of the theoretical density, without residual porosity, and without coarse precipitation.
  • the method according to the invention thus has the advantage of obtaining mechanical parts with high characteristics and a correct density.
  • the method used according to the invention offers the additional advantage of being inexpensive and applicable for mass production.
  • the most homogeneous structure is obtained with a pre-alloyed powder; it also has the advantage by compared to mixed powders to avoid mixing and to limit the handling of powders to the possible addition of a compacting lubricant.
  • the following operation, cold compaction, is carried out on an industrial press to obtain a blank of moderate density 2.0 to 2.5 of simple shape, therefore of economical realization the mass of powder must be precise to within 1% (i.e. at + 0.5% of the correct weight of the blank), the weighing of the blank is carried out automatically on a balance at the press outlet.
  • the blank is brought to temperature in an oven in a neutral atmosphere (for example pure nitrogen) with dew point ⁇ - 30 ° C; the forging temperature is between 470 and 500 ° C (for an alloy 2214); it does not need to be specific.
  • a neutral atmosphere for example pure nitrogen
  • the blank is finally quickly removed from the oven and forged in a period of less than ten seconds in a closed die, without thick burrs, which is made possible by the weight precision of the blank; this absence of burrs is an advantage of the process, since they constitute a loss of metal and their formation imposes a high forging pressure which places a heavy load on the press and constitutes an important wear factor of the tool.
  • the final densification at 100% without porosity takes place at the same time as the flow in the solid state of the metal in the cavity; moreover, a resistance to deformation of the pieces forged by the method of the invention from powder was measured, lower than that of the pieces forged from rolled metal.
  • the product obtained is at 100% of the theoretical density without residual porosity. It is characterized by a structure with a very fine homogeneous matrix whose grain size is of the same order of magnitude as that of the initial powder grains, in which there remains a fine network of intergranular precipitates.
  • FIG. 1 relates to a part obtained with a pre-alloyed powder 2214 (AU 4 SG), forged at 500 ° C. and followed by a T6 treatment (quenching at 1 water at 500 ° C and returned for 20 hours at 160 ° C).
  • the intergranular network is very fine and apparent.
  • a characteristic of the rupture of a tensile test piece shown in FIG. 3 is the absence of necking; the reduction in section being distributed over the entire length of the test piece (dotted lines of the test piece), unlike a conventional tensile test piece shown in FIG. 2 with a necking. This unexpected phenomenon characterizes the product obtained according to the process of the invention.

Abstract

Mechanical component made of prealloyed aluminium alloy characterised by the presence of a homogeneous matrix of aluminium alloy of very fine structure in which the grain size is of the same order of magnitude as that of the initial powder grains and whose interfaces are marked by a very fine network of precipitates, the said component having a density of 100% of the theoretical density, without residual porosity and without coarse precipitation. Main application: all mechanical components obtained by powder metallurgy.

Description

La présente invention se rapporte à un procédé d'obtention de pièces mécaniques réalisées à partir de poudres d'alliage d'aluminium et subissant une opération de forgeage.The present invention relates to a process for obtaining mechanical parts produced from aluminum alloy powders and undergoing a forging operation.

Les alliages d'aluminium présentent un intérêt en pièces mécaniques pour leur faible densité, leur meilleure usinabilité, leur meilleure conductivité thermique ; par rapport aux techniques usuelles de forge et de fonderie, la métallurgie des poudres est susceptible d'apporter une réduction des pertes de matière entre la pièce brutefet la pièce finie (réduction de la mise au mille de matière) et une diminution des frais d'usinage.Aluminum alloys are of interest in mechanical parts for their low density, their better machinability, their better thermal conductivity; compared to the usual techniques of forging and foundry, powder metallurgy is likely to bring about a reduction in material losses between the raw part f and the finished part (reduction in the weight per thousand of material) and a reduction in costs machining.

Plusieurs voies sont possibles pour passer de la poudre à la pièce mécanique ; la plus simple jusqu'à maintenant consiste à utiliser les alliages sous forme de poudre d'aluminium mélangée à des poudres des éléments d'alliages par exemple cuivre, magnésium, silicium, zinc ; ce procédé impose une étape de frittage, c'est-à-dire un traitement à chaud qui donne sa cohésion à la pièce comprimée à froid.Several ways are possible to pass from the powder to the mechanical part; the simplest until now consists in using the alloys in the form of aluminum powder mixed with powders of the elements of alloys for example copper, magnesium, silicon, zinc; this process requires a sintering step, that is to say a hot treatment which gives its cohesion to the cold pressed part.

Le traitement est nécessaire car les particules d'aluminium sont recouvertes d'un film d'alumine d'environ 0,1 à 0,01 µm adhérent, stable et difficilement réductible, donc inhibiteur de diffusion, et qui rend impossible le frittage en phase solide à l'air en four industriel ; le frittage a pour rôle de former une phase liquide à partir des éléments métalliques ; ainsi dans le cas des alliages de la famille 2 000 (famille des alliages aluminium cuivre), la phase liquide eutectique se forme vers 550 °C ; le liquide mouille et dissout le film d'alumine, pénètre dans les fissures formées lors de la compression de la poudre et diffuse dans les particules métalliques ; ce procédé impose une température précise de traitement à + 3 °C près, les alliages ainsi obtenus ont une densité de 90 à 96 % de la densité théorique, avec des porosités et une hétérogénéité de la struc- ture. Les propriétés mécaniques obtenues pour un alliage 2014 d'après les fabricants de poudres sont les suivantes

  • - Résistance à la rupture R = 330 M Pa
  • - limite élastique à 0,2 % RE 0,2 = 320 M Pa
  • - Allongement en % A % = 2 %
  • - limite d'endurance 55 M Pa

pour l'état traité T6 (trempe à l'eau à 500 °C et revenu pendant 20 heures à 160°C).The treatment is necessary because the aluminum particles are covered with an alumina film of approximately 0.1 to 0.01 μm adherent, stable and difficult to reduce, therefore inhibiting diffusion, and which makes phase sintering impossible. air solid in an industrial oven; the role of sintering is to form a liquid phase from the metallic elements; thus in the case of alloys of the family 2000 (family of alloys aluminum copper), the eutectic liquid phase forms around 550 ° C; the liquid wets and dissolves the alumina film, penetrates into the cracks formed during the compression of the powder and diffuses into the metallic particles; this method requires a precise processing temperature at + 3 ° C of the resulting alloys have a density of 90 to 96% of theoretical density, with porosity and heterogeneity of the struc - ture. The mechanical properties obtained for a 2014 alloy according to the powder manufacturers are as follows
  • - Tensile strength R = 330 M Pa
  • - elastic limit at 0.2% R E 0.2 = 320 MP a
  • - Elongation in% A% = 2%
  • - endurance limit 55 M Pa

for the treated state T6 (water quenching at 500 ° C and tempered for 20 hours at 160 ° C).

L'atmosphère de frittage est un important paramètre du procédé, Messieurs AMATO, CORSO et SGAMBETTERRA ont montré que le frittage dans l'azote pur était meilleur que dans l'air ; le frittage sous vide n'améliore pas les résultats par rapport à l'azote (revue "POWER METALLURGY" n° 3 de 1976 page 171).The sintering atmosphere is an important parameter of the process, Messrs. AMATO, CORSO and SGAMBETTERRA have shown that sintering in pure nitrogen is better than in air; vacuum sintering does not improve the results compared to nitrogen (review "POWER METALLURGY" n ° 3 of 1976 page 171).

Ce procédé présente ainsi l'inconvénient d'obtenir une pièce mécanique avec des caractéristiques peu élevées et une densité finale faible. De plus ce procédé nécessite un traitement thermique avec un réglage de température extrêmement précis.This process thus has the drawback of obtaining a mechanical part with low characteristics and a low final density. In addition, this process requires heat treatment with extremely precise temperature control.

Une amélioration importante des caractéristiques passe par la suppression des porosités ; ceci peut être obtenu par forgeage à chaud des comprimés. Messieurs K.E. BUCHOVECKY et M.R. REARICK ont utilisé la gamme suivante : compression à froid de poudres mélangées, frittage avec azote, forgeage à différents taux de corroyage (ouvrage "FORGING OF POWDER METALLURGY PREFORM" de HAUSNER - 1973 éditeur M. P. I. F.). Les résultats sont alors très améliorés et pour un taux de corroyage moyen on atteint des résistances de 460 M Pa avec 4 % d'allongement. Ce procédé présente l'inconvénient de nécessiter encore un traitement thermique avec un réglage de température extrêmement précis.A significant improvement in the characteristics requires the elimination of the porosities; this can be achieved by hot forging the tablets. Messrs. K.E. BUCHOVECKY and M.R. REARICK used the following range: cold compression of mixed powders, sintering with nitrogen, forging at different rates of wrought (work "FORGING OF POWDER METALLURGY PREFORM" by HAUSNER - 1973 editor M. P. I. F.). The results are then very improved and for an average rate of wrought we reach resistances of 460 M Pa with 4% elongation. This process has the drawback of still requiring heat treatment with extremely precise temperature control.

Un autre procédé consiste à partir d'une poudre préalliée, c'est-à-dire dans laquelle chaque grain de poudre est homogène en composition de l'alliage ; la pellicule d'alumine subsiste alors et ne peut être éliminée puisqu'il n'est plus possible de fritter en présence d'une phase liquide ; on est alors obligé de procéder à un encapsulage de la poudre avant le forgeage, puis ensuite d'éliminer la capsule ; un fort corroyage brise les films d'alumine et permet aux grains de poudre de se souder ; il est alors possible d'atteindre des propriétés voisines de celle du métal laminé et forgé ; cette technique reste relativement complexe, coûteuse et applicable seulement en petite série.Another method consists in starting with a pre-alloyed powder, that is to say in which each grain of powder is homogeneous in composition of the alloy; the alumina film then remains and cannot be removed since it is no longer possible to sinter in the presence of a liquid phase; we are then obliged to encapsulate the powder before forging, then to eliminate the capsule; a strong wrought breaks the alumina films and allows the powder grains to weld; it is then possible to achieve properties close to that of rolled and forged metal; this technique remains relatively complex, expensive and applicable only in small series.

Le procédé selon l'invention a pour but d'obtenir des pièces mécaniques de caractéristiques élevées, par une voie simple et peu coûteuse, susceptible de fabrication en grande série.The purpose of the process according to the invention is to obtain mechanical parts with high characteristics, by a simple and inexpensive route, capable of mass production.

Selon un mode de réalisation de l'invention, le procédé d'obtention de pièces mécaniques est réalisé à partir de poudres d'alliage d'aluminium. Ledit procédé comprend les étapes ci-après :

  • - utilisation d'une poudre préalliée ;
  • - compactage à froid d'une ébauche de forme simple ;
  • - pesée de l'ébauche automatique afin de contrôler que le poids de l'ébauche est à + 0,5 % ;
  • - mise en température de ladite ébauche en atmosphère d'azote pur ;
  • - forgeage en température en matrice fermée.
According to one embodiment of the invention, the process for obtaining mechanical parts is carried out from aluminum alloy powders. Said method comprises the following steps:
  • - use of a pre-alloyed powder;
  • - cold compaction of a blank of simple shape;
  • - weighing the automatic blank to check that the weight of the blank is + 0.5%;
  • - temperature setting said blank in an atmosphere of pure nitrogen;
  • - temperature forging in a closed matrix.

Selon un mode de réalisation de l'invention, la pièce mécanique en poudre d'alliage d'aluminium préalliée est caractérisée par la présence d'une matrice homogène d'alliage d'aluminium à très fine structure dont la taille des grains est du même ordre de grandeur que celle des grains de poudre initiaux, et dont les interfaces sont marqués par un très fin réseau de précipités, ladite pièce ayant une densité égale à 100 % de la densité théorique, sans porosité résiduelle, et sans précipitation grossière.According to one embodiment of the invention, the mechanical part in powder of pre-alloyed aluminum alloy is characterized by the presence of a homogeneous matrix of aluminum alloy with a very fine structure whose grain size is the same order of magnitude as that of the initial powder grains, and the interfaces of which are marked by a very fine network of precipitates, said part having a density equal to 100% of the theoretical density, without residual porosity, and without coarse precipitation.

Le procédé selon l'invention présente ainsi l'avantage d'obtenir des pièces mécaniques avec des caractéristiques élevées et une densité correcte. De plus, le procédé mis en oeuvre selon l'invention offre l'avantage supplémentaire d'être peu coûteux et applicable pour la fabrication en très grande série.The method according to the invention thus has the advantage of obtaining mechanical parts with high characteristics and a correct density. In addition, the method used according to the invention offers the additional advantage of being inexpensive and applicable for mass production.

La structure la plus homogène est obtenue avec une poudre préalliée ; elle a aussi pour avantage par rapport aux poudres mélangées d'éviter le mélangeage et de limiter la manipulation de poudres à l'addition éventuelle d'un lubrifiant de compactage. L'opération suivante, le compactage à froid, est effectué sur presse industrielle pour obtenir une ébauche de densité modérée 2,0 à 2,5 de forme simple, donc de réalisation économique la masse de poudre doit être précise à moins de 1 % près (c'est-à-dire à + 0,5 % du poids correct de l'ébauche), la pesée de l'ébauche est effectuée automatiquement sur une balance en sortie de presse.The most homogeneous structure is obtained with a pre-alloyed powder; it also has the advantage by compared to mixed powders to avoid mixing and to limit the handling of powders to the possible addition of a compacting lubricant. The following operation, cold compaction, is carried out on an industrial press to obtain a blank of moderate density 2.0 to 2.5 of simple shape, therefore of economical realization the mass of powder must be precise to within 1% (i.e. at + 0.5% of the correct weight of the blank), the weighing of the blank is carried out automatically on a balance at the press outlet.

La mise à température de l'ébauche est effectuée dans un four en atmosphère neutre (par exemple azote pur) à point de rosée < - 30 °C ; la température de forgeage est comprise entre 470 et 500 °C (pour un alliage 2214); elle n'a pas besoin d'être précise.The blank is brought to temperature in an oven in a neutral atmosphere (for example pure nitrogen) with dew point <- 30 ° C; the forging temperature is between 470 and 500 ° C (for an alloy 2214); it does not need to be specific.

L'ébauche est enfin sortie rapidement du four et forgée dans un délai inférieur à une dizaine de secondes en matrice fermée, sans bavure épaisse, ce qui est rendu possible par la précision de poids de l'ébauche ; cette absence de bavures est un avantage du procédé, car elles constituent une perte de métal et leur formation impose une pression de forgeage élevée sollicitant fortement la presse et constitue un facteur d'usure important de l'outillage. La densification finale à 100 % sans porosité s'effectue en même temps que l'écoulement à l'état solide du métal dans l'empreinte ; par ailleurs, on a mesuré une résistance à la déformation des lopins forgés par le procédé de l'invention à partir de poudre, inférieure à celle des lopins forgés à partir de métal laminé.The blank is finally quickly removed from the oven and forged in a period of less than ten seconds in a closed die, without thick burrs, which is made possible by the weight precision of the blank; this absence of burrs is an advantage of the process, since they constitute a loss of metal and their formation imposes a high forging pressure which places a heavy load on the press and constitutes an important wear factor of the tool. The final densification at 100% without porosity takes place at the same time as the flow in the solid state of the metal in the cavity; moreover, a resistance to deformation of the pieces forged by the method of the invention from powder was measured, lower than that of the pieces forged from rolled metal.

Le produit obtenu est à 100 % de la densité théorique sans porosité résiduelle. Il est caractérisé par une structure à matrice homogène très fine dont la taille des grains est du même ordre de grandeur que celle des grains de poudre initiaux, dans laquelle subsiste un fin réseau de précipités intergranulaires.The product obtained is at 100% of the theoretical density without residual porosity. It is characterized by a structure with a very fine homogeneous matrix whose grain size is of the same order of magnitude as that of the initial powder grains, in which there remains a fine network of intergranular precipitates.

Cette structure est présentée sur la reproduction microgrâphique au grossissement 500 de la figure 1. Cette figure 1 concerne une pièce obtenue avec une poudre préalliée 2214 (AU 4 S G), forgée à 500 °C et suivie d'un traitement T6 (trempe à l'eau à 500 °C et revenu pendant 20 heures à 160 °C). Le réseau inter- granulaire est très fin et apparent.This structure is presented on the micrographic reproduction at magnification 500 of FIG. 1. This FIG. 1 relates to a part obtained with a pre-alloyed powder 2214 (AU 4 SG), forged at 500 ° C. and followed by a T6 treatment (quenching at 1 water at 500 ° C and returned for 20 hours at 160 ° C). The intergranular network is very fine and apparent.

Les caractéristiques mécaniques des produits obtenus pour un taux de corroyage faible sont élevées (voir tableau ci-après) et on atteint même des tenues en fatigue en flexion rotative de 160 M Pa pour 108 cycles à là température ambiante.The mechanical characteristics of the products obtained for a low degree of working are high (see table below) and even fatigue strengths in rotary bending of 160 M Pa for 10 8 cycles at room temperature are reached.

Caractéristiques mécaniques de produit obtenues selon le procédé de l'invention pour l'alliage A U 4 S G :

Figure imgb0001
Mechanical product characteristics obtained according to the process of the invention for the AU 4 SG alloy:
Figure imgb0001

Les traitements thermiques T4 et T6 consistent :

  • - pour T4 : trempe à l'eau à 500 °C et maturation pendant 4 jours ;
  • - pour T6 : trempe à l'eau à 500 °C et revenu. pendant 20 heures à 160 °C.
The T4 and T6 heat treatments consist of:
  • - for T4: water quenching at 500 ° C and maturation for 4 days;
  • - for T6: water quenching at 500 ° C and tempered. for 20 hours at 160 ° C.

Une caractéristique de la rupture d'une éprouvette de traction représentée sur la figure 3 est l'absence de striction ; la diminution de section étant répartie sur toute la longueur de l'éprouvette (traits en pointillés de l'éprouvette), contrairement à une éprouvette de traction classique représentée sur la figure 2 avec une striction. Ce phénomène inattendu caractérise le produit obtenu selon le procédé de l'invention.A characteristic of the rupture of a tensile test piece shown in FIG. 3 is the absence of necking; the reduction in section being distributed over the entire length of the test piece (dotted lines of the test piece), unlike a conventional tensile test piece shown in FIG. 2 with a necking. This unexpected phenomenon characterizes the product obtained according to the process of the invention.

Claims (2)

1. Procédé d'obtention de pièces mécaniques réalisées à partir de poudres d'alliage d'aluminium, caractérisé en ce que ledit procédé comprend les étapes ci-après : - utilisation d'une poudre préalliée ; - compactage à froid d'une ébauche de forme simple ; - pesée de l'ébauche automatique afin de contrôler que le poids de l'ébauche est à + 0,5 % ; - mise en température de ladite ébauche en atmosphère d'azote pur ; - forgeage en température en matrice fermée. 1. Method for obtaining mechanical parts produced from aluminum alloy powders, characterized in that said method comprises the following steps: - use of a pre-alloyed powder; - cold compaction of a blank of simple shape; - weighing the automatic blank to check that the weight of the blank is + 0.5%; - temperature setting said blank in an atmosphere of pure nitrogen; - temperature forging in a closed matrix. 2. Pièce mécanique en poudre d'alliage d'aluminium préalliée obtenue par le procédé de la revendication 1, caractérisée par la présence d'une matrice homogène d'alliage d'aluminium à très fine structure dont la taille des grains est du même ordre de grandeur que celle des grains de poudre initiaux, et dont les interfaces sont marqués par un très fin réseau de précipités, ladite pièce ayant une densité égale à 100 % de la densité théorique, sans porosité résiduelle, et sans précipitation grossière.2. Mechanical part made of pre-alloyed aluminum alloy powder obtained by the process of claim 1, characterized by the presence of a homogeneous matrix of aluminum alloy with a very fine structure whose grain size is of the same order larger than that of the initial powder grains, and the interfaces of which are marked by a very fine network of precipitates, said part having a density equal to 100% of the theoretical density, without residual porosity, and without coarse precipitation.
EP84401982A 1983-10-11 1984-10-04 Work pieces made from aluminium alby powder, and process for manufacturing it Withdrawn EP0142405A1 (en)

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FR8316125A FR2553015B1 (en) 1983-10-11 1983-10-11 ALUMINUM ALLOY POWDER MECHANICAL PART AND PROCESS FOR OBTAINING
FR8316125 1983-10-11

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2997325A1 (en) * 2012-10-25 2014-05-02 Peugeot Citroen Automobiles Sa Manufacturing e.g. spacers in motor vehicle comprises selecting powder from powders of aluminum particles, compressing powder for producing preform, sintering preform, quenching continuous material, and hardening material

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2963780A (en) * 1957-05-08 1960-12-13 Aluminum Co Of America Aluminum alloy powder product
FR2374428A1 (en) * 1976-12-17 1978-07-13 Aluminum Co Of America METAL ARTICLE, POWDER ALLOY AND METHOD FOR MANUFACTURING THE METAL ARTICLE FROM AN ALUMINUM-BASED POWDERED ALLOY CONTAINING SILICON AND MANGANESE
US4104061A (en) * 1976-10-21 1978-08-01 Kaiser Aluminum & Chemical Corporation Powder metallurgy
US4270951A (en) * 1978-12-08 1981-06-02 Ford Motor Company Sintering of coated briquette

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2963780A (en) * 1957-05-08 1960-12-13 Aluminum Co Of America Aluminum alloy powder product
US4104061A (en) * 1976-10-21 1978-08-01 Kaiser Aluminum & Chemical Corporation Powder metallurgy
FR2374428A1 (en) * 1976-12-17 1978-07-13 Aluminum Co Of America METAL ARTICLE, POWDER ALLOY AND METHOD FOR MANUFACTURING THE METAL ARTICLE FROM AN ALUMINUM-BASED POWDERED ALLOY CONTAINING SILICON AND MANGANESE
US4270951A (en) * 1978-12-08 1981-06-02 Ford Motor Company Sintering of coated briquette

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2997325A1 (en) * 2012-10-25 2014-05-02 Peugeot Citroen Automobiles Sa Manufacturing e.g. spacers in motor vehicle comprises selecting powder from powders of aluminum particles, compressing powder for producing preform, sintering preform, quenching continuous material, and hardening material

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FR2553015A1 (en) 1985-04-12
NO844055L (en) 1985-04-12

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