EP1250204B1 - Method for making light alloy components - Google Patents
Method for making light alloy components Download PDFInfo
- Publication number
- EP1250204B1 EP1250204B1 EP00993697A EP00993697A EP1250204B1 EP 1250204 B1 EP1250204 B1 EP 1250204B1 EP 00993697 A EP00993697 A EP 00993697A EP 00993697 A EP00993697 A EP 00993697A EP 1250204 B1 EP1250204 B1 EP 1250204B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- preform
- graphite
- forging
- casting
- container
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D31/00—Cutting-off surplus material, e.g. gates; Cleaning and working on castings
- B22D31/002—Cleaning, working on castings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J1/00—Preparing metal stock or similar ancillary operations prior, during or post forging, e.g. heating or cooling
- B21J1/06—Heating or cooling methods or arrangements specially adapted for performing forging or pressing operations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
- B21J5/002—Hybrid process, e.g. forging following casting
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
- B21J5/02—Die forging; Trimming by making use of special dies ; Punching during forging
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
Definitions
- the invention relates to the technical sector of the manufacture of light alloy parts, in particular aluminum, obtained in foundry, forging and similar processes.
- EP 119.365 discloses a specific process called COBAPRESS which combines the techniques of foundry and forging of aluminum or aluminum alloy parts.
- this process consists of casting aluminum or aluminum alloy in a mold and after casting, to release the part still hot called preform at a temperature of the order of 400 ° C at 500 ° C, we place it between two matrices or parts of a matrix defining a footprint of dimensions slightly smaller than those of the mold, which correspond to those of the final piece, the two shells or parts being strongly pressed against each other to exert on the casting preform put between the parts of the dies a combined effect of core pressing and surface dressing.
- COBAPRESS 2 therefore makes it possible to reduce production time and manufacturing cost so significant parts, while obtaining the same characteristics of the parts compared to the teaching of the COBAPRESS process described in the EP patent 119,365.
- the aim sought after according to the invention was therefore to ensure optimization of the initial COBAPRESS process of cast-forged light alloy.
- the applicant has attempted to optimize the COBAPRESS process as defined by the aforementioned prior patents.
- a first step was to focus on improving the conditions for depositing graphite in the forging matrix by spraying the graphite solution on the forging matrix, with better control of the distribution using robots. In practice, this solution is not very satisfactory, because it still requires human intervention, and the costs and environmental problems are still there.
- the process for manufacturing the light alloy parts according to the invention requires installation with five successive specific zones covering the different stages of the process.
- the first zone (Z1) corresponds to the casting of the light alloy in a mold (1) enabling a preform (2) to be obtained under the conditions previously recalled.
- the second zone (Z2) corresponds to the transfer of the preform (2) heated in a tank (3) for immersion and graphitation by coating the preform (2).
- the bath is a solution of graphite and water.
- a phase (Z3) of drying the preformed part is provided out of the bath.
- the following zone (Z4) corresponds to the transfer of the preform dried graphite in the tunnel oven (4) for homogenization in temperature.
- the following zone (Z5) corresponds to the exit of the tunnel oven from the preform to be then forged in a matrix (5) which is the object less and faster lubrication limited to the burr bead depending on the conditions mentioned above, then cooled to temperature ambient or accelerated or drenched.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Forging (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Mold Materials And Core Materials (AREA)
Abstract
Description
L'invention se rattache au secteur technique de la fabrication de pièces en alliage léger, notamment en aluminium, obtenues en fonderie, forgeage et procédés similaires.The invention relates to the technical sector of the manufacture of light alloy parts, in particular aluminum, obtained in foundry, forging and similar processes.
On connaít, par le brevet EP 119.365, un procédé spécifique dénommé COBAPRESS qui combine les techniques de fonderie et de forgeage de pièces en aluminium ou alliages d'aluminium.EP 119.365 discloses a specific process called COBAPRESS which combines the techniques of foundry and forging of aluminum or aluminum alloy parts.
On rappelle que ce procédé consiste à couler de l'aluminium ou alliage d'aluminium dans un moule et après la coulée, à démouler la pièce encore chaude dénommée préforme à une température de l'ordre de 400°C à 500°C, on la place entre deux matrices ou parties d'une matrice définissant une empreinte de dimensions légèrement inférieures à celles du moule, qui correspondent à celles de la pièce finale, les deux coquilles ou parties étant fortement pressées l'une contre l'autre pour exercer sur la préforme coulée mise entre les parties de matrices un effet combiné de pressage à coeur et de corroyage superficiel.Remember that this process consists of casting aluminum or aluminum alloy in a mold and after casting, to release the part still hot called preform at a temperature of the order of 400 ° C at 500 ° C, we place it between two matrices or parts of a matrix defining a footprint of dimensions slightly smaller than those of the mold, which correspond to those of the final piece, the two shells or parts being strongly pressed against each other to exert on the casting preform put between the parts of the dies a combined effect of core pressing and surface dressing.
On connaít par ailleurs, par le brevet FR 2.778.125, un procédé du type précité amélioré qui vise à profiter de l'opération de préchauffe pour réaliser en même temps l'opération de traitement thermique économisant ainsi sur l'opération de traitement thermique classique postérieure à l'opération de frappe. Entre la coulée de la préforme et le forgeage, on transfère ladite préforme coulée dans un four assurant la mise en solution de ladite préforme coulée à la température de mise en solution du matériau constitutif et placée ensuite entre les deux parties de la matrice de frappe pour l'opération de forgeage avec refroidissement ambiant, en accéléré ou trempé.We also know, from patent FR 2,778,125, a method of aforementioned improved type which aims to take advantage of the preheating operation for simultaneously perform the heat treatment operation saving thus on the conventional heat treatment operation after the typing operation. Between the casting of the preform and the forging, we transfers said preform poured into an oven ensuring the dissolution of said preform poured at the dissolution temperature of the material component and then placed between the two parts of the striking matrix for the forging operation with ambient, accelerated or tempered.
Ce procédé amélioré dénommé COBAPRESS 2 permet donc de réduire le temps de production et le coût de fabrication de manière significative des pièces, tout en obtenant les mêmes caractéristiques des pièces par rapport à l'enseignement du procédé COBAPRESS décrit dans le brevet EP 119.365.This improved process called COBAPRESS 2 therefore makes it possible to reduce production time and manufacturing cost so significant parts, while obtaining the same characteristics of the parts compared to the teaching of the COBAPRESS process described in the EP patent 119,365.
La mise en oeuvre du procédé précité dans les deux versions requiert de manière courante dans l'activité de forgeage de pulvériser sur la matrice de forge une solution eau plus graphite à l'état liquide, qui a pour but de faciliter le fluage de la matière ainsi forgée et le démoulage de la pièce finale.The implementation of the above method in both versions requires commonly in forging activity to spray on the die forging a water solution plus graphite in the liquid state, which aims to facilitate the flow of the material thus forged and the release of the part final.
En pratique, la pulvérisation de la solution graphite sur la matrice de
forge est une opération qui, en fonction de la complexité des formes de la
pièce finale brute, est relativement longue et coûteuse, qui ne permet pas
systématiquement d'avoir une homogénéité de pulvérisation dans les parties
d'accès difficile de la pièce, et enfin qui est très salissante pour le poste de
travail.
On connaít par ailleurs le brevet US 4683742 qui prévoit le
préchauffage des billettes avant de leur appliquer un revêtement de type
graphite puis les billettes étant forgées ensuite après passage dans une
installation de séchage. In practice, the spraying of the graphite solution on the forging die is an operation which, depending on the complexity of the shapes of the raw final part, is relatively long and costly, which does not systematically allow uniformity of spraying. in the parts of difficult access of the part, and finally which is very messy for the work station.
We also know US Patent 4683742 which provides preheating of the billets before applying a coating of graphite type and then the billets being forged after passing through a drying installation.
Le but recherché selon l'invention était donc d'assurer une
optimisation du procédé COBAPRESS initial de coulé-forgé en alliage
léger.
On connaít aussi par le brevet JP 6005433 le forgeage de billettes
avec utilisation d'un revêtement graphite.
Face à l'ensemble de l'art antérieur précité, le demandeur a tenté
d'optimiser le procédé du COBAPRESS tel que défini par les brevets
antérieurs précités.
Une première démarche a été de s'orienter sur une amélioration des
conditions de dépose du graphite dans la matrice de forgeage par
pulvérisation de la solution de graphite sur la matrice de forge, avec un
meilleur contrôle de la distribution à l'aide de robots. En pratique, cette
solution est peu satisfaisante, car elle nécessite tout de même l'intervention
de l'homme, et les coûts et problèmes environnementaux sont toujours là.The aim sought after according to the invention was therefore to ensure optimization of the initial COBAPRESS process of cast-forged light alloy.
We also know from JP 6005433 the forging of billets with the use of a graphite coating.
Faced with all of the aforementioned prior art, the applicant has attempted to optimize the COBAPRESS process as defined by the aforementioned prior patents.
A first step was to focus on improving the conditions for depositing graphite in the forging matrix by spraying the graphite solution on the forging matrix, with better control of the distribution using robots. In practice, this solution is not very satisfactory, because it still requires human intervention, and the costs and environmental problems are still there.
La démarche du demandeur s'est donc orientée de manière inattendue sur une autre possibilité qui s'intercale entre les deux phases principales de coulée et de forgeage, possibilité qui offre toutes les garanties dans une répartition homogène de la solution graphite sur la préforme, et qui au surplus apporte des caractéristiques particulières intéressantes, en améliorant la productivité du procédé.The applicant's approach was therefore unexpectedly oriented on another possibility which is inserted between the two main phases of casting and forging, possibility which offers all the guarantees in a homogeneous distribution of the graphite solution on the preform, and which at surplus brings interesting particular characteristics, in improving the productivity of the process.
Selon une première caractéristique, le procédé de fabrication des pièces en alliage léger est du type mettant en oeuvre les phases suivantes :
- coulage de la préforme à une température de l'ordre de 250° à 500°C,
- transfert de la préforme chauffée dans une matrice définissant une empreinte de dimensions légèrement inférieures à celle du moule, les deux parties de la matrice étant pressées l'une contre l'autre pour exercer l'effort de forgeage, de matriçage de la pièce brute finale,
- refroidissement de la pièce brute à la température ambiante, le procédé étant caractérisé en ce que après coulage de la préforme chauffée et avant le transfert de la préforme dans une matrice de forge, ladite préforme, à température de fin de coulée est transférée et immergée totalement dans un bac pour graphitage par enduction, pour autoriser le dépôt de la solution graphite sur la préforme, puis en sortie de bac, la température de la préforme permettant l'évaporation naturelle de l'eau de sorte que la préforme est recouverte d'une manière homogène de graphite.
- pouring the preform at a temperature of the order of 250 ° to 500 ° C,
- transfer of the heated preform into a matrix defining an imprint of dimensions slightly smaller than that of the mold, the two parts of the matrix being pressed one against the other to exert the forging effort, forging the final blank ,
- cooling of the blank to ambient temperature, the process being characterized in that after casting the heated preform and before transferring the preform into a forging die, said preform, at end of casting temperature, is transferred and completely immersed in a graphitation tank by coating, to allow the graphite solution to be deposited on the preform, then at the tank outlet, the temperature of the preform allowing the natural evaporation of water so that the preform is covered with a homogeneous graphite.
Ainsi on a plus besoin de remettre la pièce en chauffe pour la tenue
du produit de revêtement ni d'avoir un système pour faire évaporer l'eau,
celle-ci étant naturelle.
Selon une autre caractéristique, le procédé perfectionné de
fabrication des pièces en alliage léger est du type mettant en oeuvre les
phases suivantes :
- coulage de préforme à une température de l'ordre de 250° à 500°C ;
- transfert de la préforme coulée obtenue dans un four assurant la mise en solution de ladite préforme coulée à la température de mise en solution du matériau constitutif ;
- transfert de la préforme mise en solution en sortie du four dans une matrice définissant une empreinte de dimensions légèrement inférieures à celles du moule, les parties de la matrice étant pressées l'une contre l'autre pour exercer l'effort de forgeage, de matriçage de la pièce brute finale ;
- refroidissement de la pièce brute obtenue à la température ambiante, en accéléré ou trempé, le procédé étant caractérisé en ce que, après coulage de la préforme chauffée et avant le transfert dans le four tunnel, ladite préforme, à température de fin de coulée, est transférée et immergée totalement dans un bac pour graphitage par enduction, pour autoriser le dépôt de la solution graphite sur la préforme, puis en sortie de bac, à ce stade, la température de la préforme et celle du procédé en amont permettant l'évaporation naturelle de l'eau, de sorte que la préforme est recouverte d'une manière homogène de graphite, ladite préforme étant ensuite remise en température dans le four tunnel assurant l'homogénéisation en température de la préforme graphitée.
According to another characteristic, the improved process for manufacturing light alloy parts is of the type implementing the following phases:
- casting of preform at a temperature of the order of 250 ° to 500 ° C;
- transfer of the casting preform obtained in an oven ensuring the dissolution of said casting preform at the dissolution temperature of the constituent material;
- transfer of the preform dissolved in the outlet of the furnace in a matrix defining an imprint of dimensions slightly smaller than those of the mold, the parts of the matrix being pressed one against the other to exert the effort of forging, forging of the final blank;
- cooling of the blank obtained at room temperature, accelerated or quenched, the process being characterized in that, after pouring the heated preform and before transferring it to the tunnel oven, said preform, at the end of casting temperature, is transferred and completely immersed in a tray for graphitation by coating, to authorize the deposition of the graphite solution on the preform, then at the exit of the tray, at this stage, the temperature of the preform and that of the upstream process allowing natural evaporation water, so that the preform is homogeneously covered with graphite, said preform then being brought back to temperature in the tunnel oven ensuring the temperature homogenization of the graphite preform.
Ces caractéristiques et d'autres encore ressortiront bien de la suite de la description.These and other characteristics will become apparent from the following the description.
Pour fixer l'objet de l'invention illustré d'une manière non limitative aux figures du dessin où la figure 1 représente le schéma de mise en oeuvre du procédé selon l'invention.To fix the object of the invention illustrated in a nonlimiting manner to the drawing figures where Figure 1 shows the implementation diagram of the process according to the invention.
Le procédé de fabrication des pièces en alliage léger selon l'invention requiert une installation avec cinq zones spécifiques successives couvrant les différentes étapes du procédé.The process for manufacturing the light alloy parts according to the invention requires installation with five successive specific zones covering the different stages of the process.
La première zone (Z1) correspond à la coulée de l'alliage léger dans un moule (1) permettant l'obtention d'une préforme (2) dans les conditions de température rappelées précédemment. The first zone (Z1) corresponds to the casting of the light alloy in a mold (1) enabling a preform (2) to be obtained under the conditions previously recalled.
La seconde zone (Z2) correspond au transfert de la préforme (2) chauffée dans un bac (3) pour immersion et graphitage par enduction de la préforme (2). Le bain est une solution de graphite et eau.The second zone (Z2) corresponds to the transfer of the preform (2) heated in a tank (3) for immersion and graphitation by coating the preform (2). The bath is a solution of graphite and water.
Adjacent au bac permettant le graphitage par enduction, ou dans son plan supérieur, est prévue une phase (Z3) de séchage de la pièce préformée hors du bain.Adjacent to the tray for graphitation by coating, or in its upper plane, a phase (Z3) of drying the preformed part is provided out of the bath.
La zone (Z4) suivante correspond au transfert de la préforme graphitée séchée dans le four tunnel (4) pour homogénéisation en température. La zone (Z5) suivante correspond à la sortie du four tunnel de la préforme pour être ensuite forgée dans une matrice (5) qui fait l'objet d'une lubrification moindre et plus rapide limitée au cordon de bavure selon les conditions évoquées précédemment, puis refroidie à température ambiante ou accélérée ou trempée.The following zone (Z4) corresponds to the transfer of the preform dried graphite in the tunnel oven (4) for homogenization in temperature. The following zone (Z5) corresponds to the exit of the tunnel oven from the preform to be then forged in a matrix (5) which is the object less and faster lubrication limited to the burr bead depending on the conditions mentioned above, then cooled to temperature ambient or accelerated or drenched.
Le procédé optimisé selon l'invention apparaít donner aux pièces ainsi traitées des avantages spécifiques.The optimized process according to the invention appears to give the parts thus treated specific benefits.
Les avantages du procédé optimisé de l'invention sont nombreux .
On profite de la température de la préforme pour permettre au
graphite d'accrocher sur la préforme puis à l'eau de s'évaporer avant les
opérations suivantes
- une qualité d'état de surface plus affiné de la pièce grâce à une homogénisation du dépôt de solution graphite qui a une influence sur les conditions d'essai de rupture ;
- une meilleure tenue en essai de fatigue ;
- une longévité accrue de l'outillage de frappe
- une amélioration de l'environnement ;
- un gain de productivité ;
- une formation humaine moindre et moins complexe, ce qui est important en regard du recrutement de main d'oeuvre qualifié, ce qui est toujours difficile ou une automatisation plus simple ;
- au moment de l'homogénisation en température dans le four tunnel pour homogénéisation en température, la couleur noire issue du bain graphité permet de mieux emmagasiner les calories et donc d'améliorer les caractéristiques de structure et mécaniques de la pièce ;
- De plus, une nuance de couleur pourrait répondre à un besoin d'esthétique et de coloris. Une plus grande discrétion pour des éléments de sécurité et plus particulièrement de suspension - châssis pour éviter l'effet de brillance sous carrosserie visible par les conducteurs voisins au véhicule concerné.
We take advantage of the temperature of the preform to allow the graphite to hang on the preform and then the water to evaporate before the following operations
- a more refined surface finish quality of the part thanks to a homogenization of the graphite solution deposit which has an influence on the failure test conditions;
- better resistance in fatigue test;
- increased longevity of impact tools
- improvement of the environment;
- increased productivity;
- less and less complex human training, which is important with regard to the recruitment of qualified labor, which is always difficult or simpler automation;
- at the time of temperature homogenization in the tunnel oven for temperature homogenization, the black color resulting from the graphite bath makes it possible to better store calories and therefore to improve the structural and mechanical characteristics of the part;
- In addition, a shade of color could meet a need for aesthetics and colors. Greater discretion for safety elements and more particularly suspension - chassis to avoid the shine effect under the body visible by drivers next to the vehicle concerned.
Les avantages sont donc nombreux. Le procédé est optimisé selon l'invention et apporte des améliorations inattendues et récentes qui justifient son développement.The advantages are therefore numerous. The process is optimized according to the invention and makes unexpected and recent improvements that justify His development.
Claims (4)
- Process for manufacturing light alloys parts involves the following operations :Having a casting preform at about 250°C to 500°Ctransferring the cast preform in a furnace to solution heat treat the preform material.transferring the cast preform thus obtained from the preheat furnace directly to the forging press between two halves of a die that defines a cavity having dimensions that are slightly less than those of the mould, the two halves being forced together in order to exert an impact forging forcecooling the rough forging thus obtained at room temperature or accelerated cooling or cooling by quench
- Process for manufacturing light alloys parts involves the following operations :Having a casting preform at about 250°C to 500°Ctransferring the cast preform in a furnace to solution heat treat the preform material.transferring the cast preform thus obtained from the preheat furnace directly to the forging press between two halves of a die that defines a cavity having dimensions that are slightly less than those of the mould, the two halves being forced together in order to exert an impact forging forcecooling the rough forging thus obtained at room temperature or accelerated cooling or cooling by quench
What makes the invention specific is that after the casting of the as said preform and before the forging operation, the as said hot preform is transferred and dipped in a graphite solution container for lubrication.. Outside of the container, the preform temperature allows the water to evaporate and the graphite to stick to the preform creating an homogeneous graphite skin all around it.The as said preform is after transferred in a tunnel furnace for temperature homogenization. - Process as claimed in claim 1 and 2, characterized in that we can introduce color in the lubrication container.
- The process of this invention needs an installation of five successive specific areas .The first zone (Z1) corresponds to the casting of the alloy in a mold in order to obtain a preform in hot temperature conditions.The second zone (Z2) corresponds to the transfer of the hot preform (2) in a container (3) for a graphite solution dipping for lubrication. The bath is a graphite and water solution.On the side of the lubrication container, or above it, is the drying sequence (Z3) of the preform out of the bath.lubrication,The next (Z4) area corresponds to the transfer of the graphite lubricated preform in the tunnel furnace (4) for temperature homogenization. The (Z5) area is the exit of the preform from the tunnel furnace then brought to the forging die which is only slightly and therefore quicker lubricated and this only inside the cavity limited to the rib around it according to the above conditions. The part is then cooled naturally, or in an accelerated process or quenched.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9916831A FR2803232B1 (en) | 1999-12-29 | 1999-12-29 | IMPROVED PROCESS FOR MANUFACTURING LIGHT ALLOY PARTS |
FR9916831 | 1999-12-29 | ||
PCT/FR2000/003703 WO2001049435A1 (en) | 1999-12-29 | 2000-12-27 | Improved method for making light alloy components |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1250204A1 EP1250204A1 (en) | 2002-10-23 |
EP1250204B1 true EP1250204B1 (en) | 2003-07-30 |
Family
ID=9554133
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP00993697A Expired - Lifetime EP1250204B1 (en) | 1999-12-29 | 2000-12-27 | Method for making light alloy components |
Country Status (12)
Country | Link |
---|---|
US (1) | US20020166357A1 (en) |
EP (1) | EP1250204B1 (en) |
JP (1) | JP5025870B2 (en) |
KR (1) | KR100730711B1 (en) |
CN (1) | CN1221348C (en) |
AT (1) | ATE246063T1 (en) |
AU (1) | AU771366B2 (en) |
CA (1) | CA2396043C (en) |
DE (1) | DE60004271T2 (en) |
ES (1) | ES2204753T3 (en) |
FR (1) | FR2803232B1 (en) |
WO (1) | WO2001049435A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2164999A1 (en) * | 2007-07-09 | 2010-03-24 | Bharat Forge Aluminiumtechnik GMBH & CO. KG | Casting-forging of wrought alloys |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20040221931A1 (en) * | 2002-09-09 | 2004-11-11 | Asahi Tec Corporation | Aluminum cast -forged product and method for manufacturing aluminum cast-forged product |
JP4712040B2 (en) * | 2004-08-04 | 2011-06-29 | エルジー エレクトロニクス インコーポレイティド | Broadcast / multicast service system and method for providing roaming between networks |
DE102006036369B4 (en) * | 2006-08-02 | 2009-04-09 | Kahn, Friedhelm, Prof. Dr. Ing. | Method and device for producing components by integrated melting, casting and forming |
FR2958193B1 (en) * | 2010-04-06 | 2012-06-29 | Saint Jean Ind | PROCESS FOR MANUFACTURING LIGHT ALLOY FORGED PARTS INCORPORATING FULL OR DRAWN THICKNESS SECTIONS |
FR2985205B1 (en) | 2011-12-29 | 2014-01-10 | Saint Jean Ind | METHOD OF POTEYING OF FORGE MATRIX IN THE IMPLEMENTATION OF PIECES OBTAINED BY TWO SUCCESSIVE FOUNDRY CASTING AND THEN FORGING PROCEDURES |
DE102012100458A1 (en) * | 2012-01-20 | 2013-07-25 | Martinrea Honsel Germany Gmbh | Method for producing a light metal component provided with at least one cavity |
WO2014159153A1 (en) * | 2013-03-13 | 2014-10-02 | Consolidated Engineering Company, Inc. | System and method for formation and processing of high pressure die cast metal articles |
DE102014101609A1 (en) * | 2014-02-10 | 2015-08-13 | Ertl Automation Gmbh & Co. Kg | Method for cooling a cast component |
KR20160123766A (en) | 2015-04-17 | 2016-10-26 | 주식회사 엘지에스 | Apparatus for cleaning wafer |
CN112404411A (en) * | 2020-11-21 | 2021-02-26 | 冯柏松 | Aluminum alloy casting method and aluminum alloy casting system |
CN113751639A (en) * | 2021-07-28 | 2021-12-07 | 韩有良 | Forging equipment for high-pressure shell of deep-sea exploration submarine |
Family Cites Families (44)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1711000A (en) * | 1925-07-02 | 1929-04-30 | Gen Motors Res Corp | Method of making wrought-metal articles |
US2588625A (en) * | 1945-03-15 | 1952-03-11 | Aluminum Co Of America | Forging lubricant and method of using same |
US2821016A (en) * | 1955-03-03 | 1958-01-28 | William M Dickson | Method of hot forging or extruding metal shapes and lubricant for use in hot forging and extruding operations |
GB1078781A (en) * | 1963-04-26 | 1967-08-09 | Julius Friedrich Werner Schleg | Hot working of metal castings |
US3339271A (en) * | 1964-07-01 | 1967-09-05 | Wyman Gordon Co | Method of hot working titanium and titanium base alloys |
GB1172093A (en) * | 1965-10-23 | 1969-11-26 | Federal Mogul Corp | Improvements in Forging Parts from Workpieces |
US3637498A (en) * | 1968-04-29 | 1972-01-25 | Aluminum Co Of America | Extrusion lubricant |
US3843529A (en) * | 1972-08-10 | 1974-10-22 | Dow Corning | Metal working lubricant compositions |
US3895968A (en) * | 1974-01-07 | 1975-07-22 | Paul L Mcculloch | Method of making finished steel castings |
US4284670A (en) * | 1976-08-06 | 1981-08-18 | Aluminum Company Of America | Method for applying lubricants onto metal working surfaces |
US4291927A (en) * | 1976-10-18 | 1981-09-29 | Skf Industries, Inc. | Integral foamed plastic sliding bearings |
US4055975A (en) * | 1977-04-01 | 1977-11-01 | Lockheed Aircraft Corporation | Precision forging of titanium |
US4269053A (en) * | 1979-07-25 | 1981-05-26 | Rockwell International Corporation | Method of superplastic forming using release coatings with different coefficients of friction |
DE3373281D1 (en) * | 1983-03-14 | 1987-10-08 | Serio Thomas Di | Method of producing pieces of aluminium or aluminium alloy |
JPS6056433A (en) * | 1983-09-07 | 1985-04-02 | Mitsubishi Electric Corp | Induction heating device |
GB8507093D0 (en) * | 1985-03-19 | 1985-04-24 | Radyne Ltd | Coating billets for forging |
US4621399A (en) * | 1985-12-18 | 1986-11-11 | Allied Tube & Conduit Corporation | Tube-coating method and apparatus therefor |
US4683747A (en) * | 1986-03-14 | 1987-08-04 | Hall James W | Timing device |
US4775426A (en) * | 1986-04-03 | 1988-10-04 | Richards Medical Company | Method of manufacturing surgical implants from cast stainless steel and product |
FR2614814B3 (en) * | 1987-05-04 | 1989-06-30 | Serio Thomas Di | PROCESS FOR MANUFACTURING ALUMINUM PARTS, VARIOUS ALLOYS AND ALL ALLOYS IN GENERAL |
JPH02294454A (en) * | 1989-05-09 | 1990-12-05 | Hiroshima Alum Kogyo Kk | Manufacture of forging made of al alloy |
JPH05311454A (en) * | 1992-04-03 | 1993-11-22 | Nkk Corp | Composite coated aluminum plate or aluminum alloy plate excellent in press moldability, scratch resistance, filiform erosion resistance and image clarity |
JPH06158250A (en) * | 1992-11-17 | 1994-06-07 | Furukawa Alum Co Ltd | Manufacture of aluminum alloy cast product having excellent mechanical characteristic |
US5456953A (en) * | 1993-02-26 | 1995-10-10 | Armco Steel Company, L.P. | Method for coating bake hardenable steel with a water based chromium bearing organic resin |
US5493886A (en) * | 1993-08-23 | 1996-02-27 | Cleveland State University | Elevated temperature metal forming lubrication method |
US5484541A (en) * | 1994-05-17 | 1996-01-16 | Century Chemical Corporation | Process and product for lubricating metal prior to cold forming |
US5495737A (en) * | 1994-07-15 | 1996-03-05 | Cleveland State University | Elevated temperature metal forming lubrication |
JPH08311468A (en) * | 1995-05-15 | 1996-11-26 | Daido Steel Co Ltd | Lubricating coating agent for hot forging |
US5658383A (en) * | 1995-05-16 | 1997-08-19 | Cutshall; Taylor K. | Liquid coating apparatus |
US5584201A (en) * | 1995-11-20 | 1996-12-17 | Cleveland State University | Elevated temperature metal forming lubrication method |
JP3755174B2 (en) * | 1995-11-27 | 2006-03-15 | 大同特殊鋼株式会社 | Method for forging Ti alloy |
FR2749851B1 (en) * | 1996-06-13 | 2000-02-25 | Valeo Systemes Dessuyage | METHOD FOR MANUFACTURING A PROFILE HAVING A SURFACE LAYER REDUCING THE COEFFICIENT OF FRICTION WITH A GLASS SURFACE TO BE WIPED AND WIPING BLADE OBTAINED BY SUCH A PROCESS |
DE19626175C2 (en) * | 1996-06-29 | 2000-01-13 | Honsel Ag | Method and device for producing a brake drum or a brake disc |
EP0816042A1 (en) * | 1996-07-03 | 1998-01-07 | GUIDO BAGGIOLI S.N.C. DI BAGGIOLI GIUSEPPE & PELLEGRINI CLEMENTINA | A process for manufacturing alloy castings |
JP3812035B2 (en) * | 1997-02-10 | 2006-08-23 | オイレス工業株式会社 | Sphere-shaped sealing body and method for manufacturing the same |
US6129362A (en) * | 1997-02-10 | 2000-10-10 | Oiles Corporation | Spherical annular seal member and method of manufacturing the same |
JP4010381B2 (en) * | 1997-10-24 | 2007-11-21 | 本田技研工業株式会社 | Forging method |
FR2778125B1 (en) * | 1998-05-04 | 2000-07-07 | Serio Emile Di | PROCESS FOR MANUFACTURING PARTS OF CAST ALLOYS, PARTICULARLY ALUMINUM |
US6376433B1 (en) * | 1999-07-13 | 2002-04-23 | Century Chemical Corporation | Process and product for lubricating metal prior to cold forming |
AU4686801A (en) * | 2000-04-10 | 2001-10-23 | Showa Denko Kabushiki Kaisha | Forged scroll part and production method therefor |
US6702907B2 (en) * | 2000-04-10 | 2004-03-09 | Showa Denko K.K. | Forged scroll part and production process thereof |
JP2003103330A (en) * | 2001-09-27 | 2003-04-08 | Asahi Tec Corp | Manufacturing method for forging, manufacturing device for forging, and preform forging material |
US7105472B2 (en) * | 2002-04-04 | 2006-09-12 | Walter Zepf | Coating solution for metals and metal alloys |
US20080078225A1 (en) * | 2006-09-28 | 2008-04-03 | Gm Global Technology Operations, Inc. | Lubricant formulation for high temperature metal forming processes |
-
1999
- 1999-12-29 FR FR9916831A patent/FR2803232B1/en not_active Expired - Lifetime
-
2000
- 2000-12-27 DE DE60004271T patent/DE60004271T2/en not_active Expired - Lifetime
- 2000-12-27 JP JP2001549791A patent/JP5025870B2/en not_active Expired - Lifetime
- 2000-12-27 ES ES00993697T patent/ES2204753T3/en not_active Expired - Lifetime
- 2000-12-27 WO PCT/FR2000/003703 patent/WO2001049435A1/en active IP Right Grant
- 2000-12-27 CA CA002396043A patent/CA2396043C/en not_active Expired - Lifetime
- 2000-12-27 KR KR1020027008421A patent/KR100730711B1/en active IP Right Grant
- 2000-12-27 AT AT00993697T patent/ATE246063T1/en active
- 2000-12-27 AU AU28605/01A patent/AU771366B2/en not_active Expired
- 2000-12-27 CN CNB008178380A patent/CN1221348C/en not_active Expired - Lifetime
- 2000-12-27 EP EP00993697A patent/EP1250204B1/en not_active Expired - Lifetime
-
2002
- 2002-06-26 US US10/180,878 patent/US20020166357A1/en not_active Abandoned
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2164999A1 (en) * | 2007-07-09 | 2010-03-24 | Bharat Forge Aluminiumtechnik GMBH & CO. KG | Casting-forging of wrought alloys |
Also Published As
Publication number | Publication date |
---|---|
KR20020086877A (en) | 2002-11-20 |
EP1250204A1 (en) | 2002-10-23 |
FR2803232A1 (en) | 2001-07-06 |
CN1414890A (en) | 2003-04-30 |
DE60004271D1 (en) | 2003-09-04 |
JP5025870B2 (en) | 2012-09-12 |
KR100730711B1 (en) | 2007-06-21 |
FR2803232B1 (en) | 2002-04-26 |
CA2396043A1 (en) | 2001-07-12 |
JP2003527966A (en) | 2003-09-24 |
CA2396043C (en) | 2009-04-21 |
ATE246063T1 (en) | 2003-08-15 |
ES2204753T3 (en) | 2004-05-01 |
WO2001049435A1 (en) | 2001-07-12 |
DE60004271T2 (en) | 2004-04-22 |
AU2860501A (en) | 2001-07-16 |
US20020166357A1 (en) | 2002-11-14 |
AU771366B2 (en) | 2004-03-18 |
CN1221348C (en) | 2005-10-05 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1250204B1 (en) | Method for making light alloy components | |
CN107952948A (en) | As-cast aluminum alloy wheel hub low-pressure casting preparation method | |
CN104259438A (en) | Copper-steel bimetal casting improved technology | |
CN109014038A (en) | A method of reducing shell spalling in precision-investment casting dewaxing process | |
JP2000053058A (en) | Body frame for two-wheeled vehicle and manufacture thereof | |
CN103266325A (en) | Spotted copper ware manufacturing technology | |
EP1530651B1 (en) | Method and apparatus for simplified production of heat treatable aluminum alloy castings with artificial self-aging | |
CA2270751A1 (en) | Production process for cast alloy workpieces, especially aluminum parts | |
US20010009170A1 (en) | Apparatus for simplified production of heat treatable aluminum alloy castings with artificial self-aging | |
JPH1136035A (en) | Magnesium alloy formed part and its production | |
CN1425792A (en) | Composite heat processing and forming method for reinforced aluminium alloy | |
US7494554B1 (en) | Method for continuous manufacturing of cast articles utilizing one or more fluidized beds for heat treating and aging purposes | |
CH568747A5 (en) | ||
KR20170006324A (en) | Aluminum alloy archery handle and manufacturing method thereof | |
FR2814096A1 (en) | Light alloy casting fabrication method for internal combustion engine cylinder block manufacture, involves coating outer surface of liner with lampblack | |
JPS61119668A (en) | Manufacture of portable watch case made of zinc alloy | |
CN107755632A (en) | The method that manufacture has the high strength light alloy product of hot cracking tendency | |
JP2554496B2 (en) | Hand casting molding method | |
CN114559007A (en) | Novel ultra-high temperature die casting process for stainless steel | |
CN109092982A (en) | A method of forming metal alloy parts | |
RU2278906C1 (en) | Method of manufacture of art articles by sputtering | |
JPH03243211A (en) | Indirectly extruding method | |
JP2005169926A (en) | Matting method of gold ornament | |
Cocks et al. | Modern technology ensures zinc die castings meet market needs | |
BE486076A (en) |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 20020618 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE TR |
|
AX | Request for extension of the european patent |
Free format text: AL;LT;LV;MK;RO;SI |
|
GRAH | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOS IGRA |
|
RTI1 | Title (correction) |
Free format text: METHOD FOR MAKING LIGHT ALLOY COMPONENTS |
|
RTI1 | Title (correction) |
Free format text: METHOD FOR MAKING LIGHT ALLOY COMPONENTS |
|
GRAH | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOS IGRA |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE TR |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20030730 Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20030730 Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20030730 |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: FRENCH |
|
REF | Corresponds to: |
Ref document number: 60004271 Country of ref document: DE Date of ref document: 20030904 Kind code of ref document: P |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20031030 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20031030 |
|
REG | Reference to a national code |
Ref country code: SE Ref legal event code: TRGR |
|
NLV1 | Nl: lapsed or annulled due to failure to fulfill the requirements of art. 29p and 29m of the patents act | ||
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 20031111 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20031227 Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20031227 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20031230 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20031231 |
|
LTIE | Lt: invalidation of european patent or patent extension |
Effective date: 20030730 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2204753 Country of ref document: ES Kind code of ref document: T3 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed |
Effective date: 20040504 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: CH Payment date: 20141126 Year of fee payment: 15 Ref country code: IE Payment date: 20141124 Year of fee payment: 15 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: AT Payment date: 20141124 Year of fee payment: 15 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: BE Payment date: 20141120 Year of fee payment: 15 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: GC Effective date: 20150325 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 16 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151231 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MM01 Ref document number: 246063 Country of ref document: AT Kind code of ref document: T Effective date: 20151227 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: MM4A |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151231 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151231 Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151227 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 17 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151227 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 18 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: SE Payment date: 20191125 Year of fee payment: 20 Ref country code: DE Payment date: 20191119 Year of fee payment: 20 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20191120 Year of fee payment: 20 Ref country code: IT Payment date: 20191121 Year of fee payment: 20 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: ES Payment date: 20200102 Year of fee payment: 20 Ref country code: GB Payment date: 20191122 Year of fee payment: 20 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R071 Ref document number: 60004271 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: PE20 Expiry date: 20201226 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20201226 |
|
REG | Reference to a national code |
Ref country code: SE Ref legal event code: EUG |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FD2A Effective date: 20211229 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: ES Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20201228 |