EP1301298B1 - Equipment for moulding foundry parts with improved means for positioning sand cores, and related positioning method - Google Patents
Equipment for moulding foundry parts with improved means for positioning sand cores, and related positioning method Download PDFInfo
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- EP1301298B1 EP1301298B1 EP01956609A EP01956609A EP1301298B1 EP 1301298 B1 EP1301298 B1 EP 1301298B1 EP 01956609 A EP01956609 A EP 01956609A EP 01956609 A EP01956609 A EP 01956609A EP 1301298 B1 EP1301298 B1 EP 1301298B1
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- Prior art keywords
- core
- insert
- mold
- positioning
- cores
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C21/00—Flasks; Accessories therefor
- B22C21/12—Accessories
- B22C21/14—Accessories for reinforcing or securing moulding materials or cores, e.g. gaggers, chaplets, pins, bars
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/10—Cores; Manufacture or installation of cores
- B22C9/108—Installation of cores
Definitions
- the present invention relates generally to a system for positioning cores in aluminum casting in metal molds
- the positioning accuracy of the sand cores contributes to the dimensional accuracy of the molded metal moldings in a decisive way, since it affects most of the inner forms of the molded part and some of the outer forms.
- the interaction between the cores and the metal mold elements poses problems that go against the control of the dimensional positioning.
- the cores are generally made from a mixture of sand (usually silica) of well-defined particle size and organic chemical binders which ensure the cohesion and strength of the core.
- binders are conventionally cured according to two major families of coring processes, namely the so-called “cold box” technique (that is to say thanks to the intervention of a gaseous chemical catalyst) and the so-called “hot box” technique (that is to say, thanks to the supply of calories by the kernel box itself heated).
- the cores evolve in a similar way during the casting.
- the binders of the nuclei begin to decompose and emit gaseous residues.
- This process is further accelerated to the casting of liquid aluminum that enters the mold at temperatures generally between 600 and 750 ° C.
- the chamber profile is generally produced by a cooled metal mold element which locally accelerates the cooling of the aluminum during its solidification. in doing so, locally refine its microstructure and increase its properties (mechanical resistance, resistance to hot and cold fatigue, elongation at break, etc.)
- the smelter therefore wishes to space these cleanings as much as possible, but this is inconsistent with the elimination of scale buildup.
- the present invention aims to overcome these limitations of the state of the art.
- the present invention provides a method for positioning a core in a mold for producing a casting as defined in claim 10.
- FIG. 1 and 2 there is illustrated the conventional embodiment of a cylinder head CL by gravity casting in a mold essentially composed of a cooled metal sole S, Y ends and drawers T at the ends, these drawers closing the mold perpendicular to the yokes C.
- the inner shapes comprise cavities formed by the cores of Na inlet pipes, Nech exhaust pipes, Ne circulation, oil circulation and Nht roof (see in particular Figure 2), the latter core also realizing the weights that allow to feed the liquid metal part during solidification.
- the mold is fed with liquid metal from the bottom according to the usual technique of gravity casting for this type of part, by an attack system SA (FIG. 1).
- the cylinder head here is a four-cylinder, 16-valve, direct injection diesel engine cylinder head.
- the positioning accuracy of the intake pipes determined by the accuracy of the positioning of the corresponding cores, is essential for the control of engine performance.
- the mold-piece-casting appendages assembly is schematically represented as a whole in FIG.
- each pair of intake pipes is provided with metal end inserts I, as illustrated schematically in Figure 2 and in more detail on the enlarged views of Figures 3 and 4.
- Figure 4 illustrates in turn , by a section longitudinal, the fact that the insert I of Figure 3 in fact connects two intake pipes, and illustrates together with Figure 3 the guidance and supports made by this insert.
- insert I The main purpose of the presence of the insert I is to bring the metal mold member into contact with the core only, but with the core via this insert, secured to the core, and where appropriate by a or several other inserts, including another insert at the opposite end of the core. It should be noted in this regard that the number and arrangement of the inserts will depend essentially on the configuration of the core and the accuracy required for its positioning.
- each insert is able to define a precise positioning of the associated core cooperating with the metal mold member according to surfaces defining supports according to each of the axes x, y and z.
- the body 10 of the insert is received in a generally complementary cavity 20 formed in the sole S, and has on its underside a cavity 12 of generally parallelepipedal shape in which a generally complementary protuberance is embedded. 211 (the clearance - minimal - near) projecting from the bottom of the cavity 20. This ensures the positioning of the insert and therefore the core along the x and y axes.
- the insert has in the vicinity of its cavity 12 a bearing surface 123 adapted to come into contact with the bottom surface of the cavity 20 of the sole, so as to achieve the positioning of the insert and the core along the z axis.
- Figure 4 in particular illustrates other arrangements, namely 121, 122, 124 insert side and 212 sole side, which can also intervene for the proper positioning of the insert.
- the roof core here directly supports the z-axis on half of the intake pipes (see Figure 2), which guarantees the z-support of the inserts and thus the whole of the pipes cores Na inlet. It will be noted here that one could also, if necessary, provide inserts at the upper ends of the Na nuclei.
- Each insert I is made by casting under pressure.
- five inserts are placed in the kernel box before firing.
- the process of coring is here the so-called "cold box” process, and characterized in this case by a proportion of resin of 1% and by a silica sand particle size 55 AFS.
- the cylinder heads are here molded in gravity with a standard AS7U3G type alloy, of composition: Yes : 6.0-8.5 Fe: ⁇ 0.50 Cu: 2.8-3.8 Mg: 0.05-0.50 Zn: ⁇ 0.30 Mn: ⁇ 0.30 Ti: ⁇ 0.25 Other alone : 0.05% together : ⁇ 0,15% (values in% by weight)
- the casting temperature (measured in the holding oven) is 740 ° C.
- the sole S is cooled with water.
- the casting rate is 7 to 8 pieces / hour.
- the guidance by insert (s) realized according to the invention makes it possible to obtain on a casting of 30 consecutive yokes from a day.
- manufacturing a positioning of the ends of intake ducts (measured on parts after cooling, grit removal, elimination of the weights and metal feeding systems and inserts) characterized by a standard deviation less than or equal to 0.1 mm in the three directions of the space x, y and z.
- the rate of molding due to the regular maintenance of the mold during manufacture falls in the order of 5% to 10% compared to the example according to the invention.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
- Casting Devices For Molds (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Abstract
Description
La présente invention concerne d'une façon générale un système de positionnement de noyaux en moulage d'aluminium en moules métalliquesThe present invention relates generally to a system for positioning cores in aluminum casting in metal molds
Lors de la coulée avec noyaux de sable de pièces de fonderie notamment en alliage d'aluminium ou autre alliage léger, la précision de positionnement des noyaux en sable participe à la précision dimensionnelle des pièces moulées en moule métallique de façon déterminante, puisqu'elle affecte l'essentiel des formes intérieures de la pièce moulée et une partie des formes extérieures.During casting with sand cores of castings, in particular aluminum alloy or other light alloy, the positioning accuracy of the sand cores contributes to the dimensional accuracy of the molded metal moldings in a decisive way, since it affects most of the inner forms of the molded part and some of the outer forms.
Plus précisément et à titre d'exemple, dans le cas du moulage de culasses de moteurs thermiques pour véhicules automobiles, des fonctions moteur importantes sont directement liées au positionnement des noyaux : il en est ainsi des conduits ou pipes d'admission et d'échappement, totalement réalisés par noyautage, et dont la précision de positionnement a une influence directe sur les performances du moteur (puissance, consommation, émissions polluantes, etc.)More specifically, and by way of example, in the case of the molding of engine cylinder heads for motor vehicles, important engine functions are directly related to the positioning of the cores: this is the case for intake and exhaust pipes or pipes. , completely realized by coring, and whose positioning accuracy has a direct influence on engine performance (power, consumption, polluting emissions, etc.)
Or l'interaction entre les noyaux et les éléments de moule métalliques pose des problèmes qui vont à l'encontre de la maîtrise du positionnement dimensionnel. En effet les noyaux sont en général réalisés à partir d'un mélange de sable (le plus souvent la silice) de granulométrie bien définie et de liants chimiques organiques qui assurent la cohésion et la résistance du noyau.Now, the interaction between the cores and the metal mold elements poses problems that go against the control of the dimensional positioning. Indeed, the cores are generally made from a mixture of sand (usually silica) of well-defined particle size and organic chemical binders which ensure the cohesion and strength of the core.
Ces liants sont durcis conventionnellement selon deux grandes familles de procédés de noyautage, à savoir la technique dite de la « boite froide » (c'est-à-dire grâce à l'intervention d'un catalyseur chimique gazeux) et la technique dite de la « boite chaude » (c'est-à-dire grâce à l'apport de calories par la boite à noyaux elle-même portée en température). Mais que l'on retienne l'un ou l'autre de ces deux procédés de noyautage, les noyaux évoluent de façon similaire lors de la coulée. Ainsi, dès qu'ils sont placés dans le moule qui est lui-même à une certaine température, typiquement entre 80°C et 300°C pour les parties les plus froides et entre 400 et 500°C pour les parties les plus chaudes, les liants des noyaux commencent à se décomposer et à émettre des résidus gazeux.These binders are conventionally cured according to two major families of coring processes, namely the so-called "cold box" technique (that is to say thanks to the intervention of a gaseous chemical catalyst) and the so-called "hot box" technique (that is to say, thanks to the supply of calories by the kernel box itself heated). But whether one retains one or the other of these two methods of coring, the cores evolve in a similar way during the casting. Thus, as soon as they are placed in the mold which is itself at a certain temperature, typically between 80 ° C and 300 ° C for the coldest parts and between 400 and 500 ° C for the hottest parts, the binders of the nuclei begin to decompose and emit gaseous residues.
Ce processus est en outre accéléré à la coulée de l'aluminium liquide qui pénètre dans le moule à des températures généralement comprises entre 600 et 750°C.This process is further accelerated to the casting of liquid aluminum that enters the mold at temperatures generally between 600 and 750 ° C.
Ces résidus gazeux se condensent sur les parties métalliques du moule et créent localement des couches successives de calamine qui sont les résidus solides plus ou moins carbonisés de cette décomposition.These gaseous residues condense on the metal parts of the mold and locally create successive layers of calamine which are the more or less carbonized solid residues of this decomposition.
Ces résidus sont extrêmement durs et empêchent le bon positionnement des noyaux sur les parties métalliques.These residues are extremely hard and prevent the proper positioning of the cores on the metal parts.
Pour reprendre l'exemple des conduits d'admission ou d'échappement d'une culasse, le profil de chambre est réalisé en général par un élément de moule métallique refroidi qui permet d'accélérer localement le refroidissement de l'aluminium lors de sa solidification, et ce faisant d'affiner localement sa microstructure et d'accroître ses propriétés (résistance mécanique, tenue en fatigue à chaud et à froid, allongement à rupture, etc.)To take the example of the intake or exhaust ducts of a cylinder head, the chamber profile is generally produced by a cooled metal mold element which locally accelerates the cooling of the aluminum during its solidification. in doing so, locally refine its microstructure and increase its properties (mechanical resistance, resistance to hot and cold fatigue, elongation at break, etc.)
C'est sur cet élément métallique refroidi que viennent s'appuyer les noyaux destinés à former ces conduits. Ainsi l'accumulation de calamine à la surface de contact de l'élément de moule métallique décale les noyaux de conduits, et perturbe la précision de positionnement, avec les inconvénients précités.It is on this cooled metal element that the cores intended to form these ducts are supported. Thus the accumulation of calamine at the contact surface of the metal mold element shifts the conduit cores, and disturbs the positioning accuracy, with the aforementioned drawbacks.
Ce problème ne peut être réglé pratiquement en fabrication qu'en laissant un jeu substantiel aux guidages et appuis situés à la surface des éléments métalliques qui interagissent avec les surfaces en vis-à-vis sur le noyau, et en maintenant la propreté de ces surfaces par des interventions régulières de nettoyage en fabrication, par exemple par brossage.This problem can be resolved practically in manufacturing only by leaving a substantial clearance to the guides and supports located on the surface of the metal elements that interact with the surfaces facing the core, and by maintaining the cleanliness of these surfaces. by regular interventions of cleaning in manufacture, for example by brushing.
Ces dernières opérations perturbent la fabrication car elles rallongent les temps de cycle, détériorent le poteyage qui protège les éléments de moule vis-à-vis de l'aluminium liquide, et nécessitent de localement réparer ce poteyage en tant que de besoin.These latter operations disrupt manufacturing because they lengthen the cycle times, deteriorate the potting that protects the mold elements vis-à-vis the liquid aluminum, and require local repair this poteyage as needed.
Le' fondeur souhaite donc espacer ces nettoyages autant que possible, mais ceci est contradictoire avec l'élimination de l'accumulation de calamine.The smelter therefore wishes to space these cleanings as much as possible, but this is inconsistent with the elimination of scale buildup.
Ainsi la pratique effective, en production, est un compromis entre ces différentes contraintes, ce qui limite la précision dimensionnelle de positionnement des noyaux sur les éléments métalliques.Thus the actual practice, in production, is a compromise between these different constraints, which limits the dimensional accuracy of the positioning of the cores on the metal elements.
La présente invention vise à pallier ces limitations de l'état de la technique.The present invention aims to overcome these limitations of the state of the art.
Elle propose à cet effet, selon un premier aspect, un équipement de moulage de pièces de fonderie, en particulier de culasses de moteurs à combustion pour véhicules, tel que défini dans la revendication 1.For this purpose, it proposes, according to a first aspect, casting molding equipment, in particular of cylinder heads of combustion engines for vehicles, as defined in claim 1.
Certain aspects préférés, mais non limitatifs, de l'équipement de moulage selon l'invention sont définis dans les revendications dépendantes 2 à 9.Certain preferred, but not limiting, aspects of the molding equipment according to the invention are defined in the
Selon un deuxième aspect, la présente invention propose un procédé pour positionner un noyau dans un moule pour la réalisation d'une pièce de fonderie tel que défini dans la revendication 10.According to a second aspect, the present invention provides a method for positioning a core in a mold for producing a casting as defined in
Des aspects préférés, mais non limitatifs, du procédé selon l'invention sont définis dans les revendications 11 à 15.Preferred, but not limiting, aspects of the process according to the invention are defined in claims 11 to 15.
D'autres aspects, buts et avantages de la présente invention apparaîtront mieux à la lecture de la description détaillée suivante d'une forme de réalisation préférée de celle-ci, donnée à titre d'exemple non limitatif et faite en référence aux dessins annexés, sur lesquels :
- la figure 1 est une vue en section longitudinale d'un équipement de moulage d'une culasse,
- la figure 2 est une vue en section transversale, schématisée, du même équipement,
- la figure 3 est une vue en section transversale, à échelle agrandie, d'un détail de l'équipement selon l'invention, et
- la figure 4 est une vue en section longitudinale du détail de la figure 3.
- FIG. 1 is a view in longitudinal section of a molding equipment of a cylinder head,
- FIG. 2 is a schematic cross-sectional view of the same equipment,
- FIG. 3 is a cross-sectional view, on an enlarged scale, of a detail of the equipment according to the invention, and
- Figure 4 is a longitudinal sectional view of the detail of Figure 3.
En référence tout d'abord aux figures 1 et 2, on a illustré la réalisation classique d'une culasse CL par coulée en gravité dans un moule essentiellement composé d'une semelle métallique refroidie S, de chapes C et de tiroirs T en extrémités, ces tiroirs venant fermer le moule perpendiculairement aux chapes C.Referring firstly to Figures 1 and 2, there is illustrated the conventional embodiment of a cylinder head CL by gravity casting in a mold essentially composed of a cooled metal sole S, Y ends and drawers T at the ends, these drawers closing the mold perpendicular to the yokes C.
Les formes intérieures comprennent des cavités formées par les noyaux de pipes d'admission Na, de pipes d'échappement Nech, de circulation d'eau Ne, de circulation d'huile et de toit Nht (voir en particulier figure 2), ce dernier noyau réalisant également les masselottes qui permettent d'alimenter la pièce en métal liquide lors de la solidification. Le moule est alimenté en métal liquide par le bas selon la technique usuelle de la coulée en gravité pour ce type de pièce, par un système d'attaque SA (figure 1).The inner shapes comprise cavities formed by the cores of Na inlet pipes, Nech exhaust pipes, Ne circulation, oil circulation and Nht roof (see in particular Figure 2), the latter core also realizing the weights that allow to feed the liquid metal part during solidification. The mold is fed with liquid metal from the bottom according to the usual technique of gravity casting for this type of part, by an attack system SA (FIG. 1).
La culasse est ici une culasse de moteur à quatre cylindres, 16 soupapes, diesel à injection directe. Pour ce type de culasse, la précision du positionnement des pipes d'admission, déterminée par la précision du positionnement des noyaux correspondants, est essentielle pour la maîtrise des performances du moteur.The cylinder head here is a four-cylinder, 16-valve, direct injection diesel engine cylinder head. For this type of cylinder head, the positioning accuracy of the intake pipes, determined by the accuracy of the positioning of the corresponding cores, is essential for the control of engine performance.
L'ensemble moule-pièce-appendices de coulée est représenté schématiquement dans son ensemble sur la figure 1.The mold-piece-casting appendages assembly is schematically represented as a whole in FIG.
Selon l'invention chaque paire de pipes d'admission est munie d'inserts métalliques d'extrémités I, comme illustré schématiquement sur la figure 2 et plus en détail sur les vues agrandies des figures 3 et 4. La figure 4 illustre quant à elle, par une section longitudinale, le fait que l'insert I de la figure 3 relie en fait deux pipes d'admission, et illustre conjointement avec la figure 3 le guidage et les appuis réalisés par cet insert.According to the invention each pair of intake pipes is provided with metal end inserts I, as illustrated schematically in Figure 2 and in more detail on the enlarged views of Figures 3 and 4. Figure 4 illustrates in turn , by a section longitudinal, the fact that the insert I of Figure 3 in fact connects two intake pipes, and illustrates together with Figure 3 the guidance and supports made by this insert.
La présence de l'insert I a pour objet essentiel de mettre en contact l'élément métallique de moule non plus avec le noyau directement, mais avec le noyau par l'intermédiaire ce cet insert, solidarisé au noyau, et le cas échéant par un ou plusieurs autres inserts, notamment un autre insert à l'extrémité opposée du noyau. On notera à cet égard que le nombre et l'agencement des inserts dépendra pour l'essentiel de la configuration du noyau et de la précision requise pour son positionnement.The main purpose of the presence of the insert I is to bring the metal mold member into contact with the core only, but with the core via this insert, secured to the core, and where appropriate by a or several other inserts, including another insert at the opposite end of the core. It should be noted in this regard that the number and arrangement of the inserts will depend essentially on the configuration of the core and the accuracy required for its positioning.
Chaque insert I présente avantageusement les caractéristiques suivantes :
- il est solidarisé au(x) noyau(x) concerné(s) (ici deux noyaux Na1 et Na2 de pipes d'admission) en étant positionné dans la boite à noyau lors de la réalisation du ou des noyaux ;
- il présente un corps principal 10 à partir duquel font saillie, côté noyau, un ou plusieurs appendices de scellement, ici deux
111, 112 respectivement pour chacun des deux noyaux de pipes d'admission Na1 et Na2, ces appendices étant emprisonnés dans la masse de sable et de liants organiques au moment de la formation (tir) des noyaux, de telle sorte qu'après durcissement des liants, chaque noyau entoure ces appendices et qu'une liaison intime soit réalisée entre le noyau et l'insert ;appendices - le
corps 10 de l'insert intègre des formes aptes à réaliser son guidage et son positionnement, et donc celui du noyau, dans des formes généralement complémentaires prévues sur ou dans l'élément métallique de moule situé en vis-à-vis (ici la semelle S), comme on le verra en détail plus loin ; - l'insert est dessiné de telle sorte qu'il assure la surface de contact entre le noyau dont il est solidaire et l'élément métallique de moule en vis-à-vis de telle sorte que la calamine due à la dégradation à chaud du noyau ne perturbe pas le positionnement du noyau muni de son ou de ses inserts sur l'élément métallique ;
- la forme de l'insert I est choisie pour qu'il puisse être facilement réalisé, par exemple par un procédé de moulage métallique, notamment d'aluminium sous pression, en choisissant un matériau compatible avec l'alliage de la pièce à mouler, et qui en particulier ne pose pas de problème de compatibilité à la refusion ;
- en outre, quel que soit le procédé de réalisation choisi pour le ou les inserts, il est préférable de définir toutes les formes et surfaces de guidage et d'appui sur un même élément de l'outillage (typiquement un même élément de moule) de réalisation des inserts. Ceci permet d'éviter des décalages mutuels indésirables dans ces formes et surfaces, ce qui pourrait être le cas notamment si certaines d'entre elles étaient obtenues par des tiroirs dont le positionnement lors du moulage n'est pas toujours garanti avec une bonne précision.
- it is secured to the (x) nucleus (s) concerned (here two Na1 and Na2 nuclei intake pipes) being positioned in the core box during the realization of the nucleus (s);
- it has a
main body 10 from which protrude, on the core side, one or more sealing appendages, here two 111, 112 respectively for each of the two pipes Na1 and Na2 intake pipes, these appendages being imprisoned in the mass sand and organic binders at the time of formation (firing) of the cores, such that after curing the binders, each core surrounds these appendages and an intimate connection is made between the core and the insert;appendices - the
body 10 of the insert incorporates shapes able to carry out its guidance and its positioning, and therefore that of the core, in generally complementary shapes provided on or in the metal mold element located vis-à-vis (here the sole S), as will be seen in detail below; - the insert is designed so that it ensures the contact surface between the core which it is integral with and the metal mold element vis-à-vis so that the scale due to the hot degradation of the core does not disturb the positioning of the core provided with its or its inserts on the metal element;
- the shape of the insert I is chosen so that it can easily be produced, for example by a metal molding process, in particular pressurized aluminum, by choosing a material compatible with the alloy of the part to be molded, and which in particular does not pose a problem of compatibility with remelting;
- in addition, whatever the method of realization chosen for the insert or inserts, it is preferable to define all the shapes and surfaces of guide and support on the same element of the tooling (typically the same mold element) of realization of the inserts. This avoids undesirable mutual offsets in these shapes and surfaces, which could be the case especially if some of them were obtained by drawers whose positioning during molding is not always guaranteed with good accuracy.
On va maintenant décrire en détail, à titre d'exemple, des guidages et appuis possibles pour des inserts dans les trois directions de l'espace telles qu'indiquées sur la figure 4, x désignant la direction longitudinale de la culasse, y sa direction transversale et z la verticale.We will now describe in detail, by way of example, possible guides and supports for inserts in the three directions of space as indicated in FIG. 4, where x denotes the longitudinal direction of the yoke, and its direction. transverse and z the vertical.
Dans une forme de réalisation de base, chaque insert est apte à définir un positionnement précis du noyau associé en coopérant avec l'élément métallique de moule selon des surfaces définissant des appuis selon chacun des axes x, y et z.In a basic embodiment, each insert is able to define a precise positioning of the associated core cooperating with the metal mold member according to surfaces defining supports according to each of the axes x, y and z.
Ainsi, dans le présent exemple, le corps 10 de l'insert est reçu dans une cavité généralement complémentaire 20 formée dans la semelle S, et présente sur sa face inférieure une cavité 12 de forme générale parallélépipédique dans laquelle s'encastre une protubérance généralement complémentaire 211 (aux jeux - minimes - près) en saillie à partir du fond de la cavité 20. Ceci assure le positionnement de l'insert et donc du noyau selon les axes x et y. En outre, l'insert possède au voisinage de sa cavité 12 une surface d'appui 123 apte à venir au contact de la surface de fond de la cavité 20 de la semelle, de façon à réaliser le positionnement de l'insert et du noyau selon l'axe z.Thus, in the present example, the
La figure 4 en particulier illustre d'autres aménagements, à savoir 121, 122, 124 côté insert et 212 côté semelle, qui peuvent également intervenir pour le bon positionnement de l'insert.Figure 4 in particular illustrates other arrangements, namely 121, 122, 124 insert side and 212 sole side, which can also intervene for the proper positioning of the insert.
On observe par ailleurs que, pour faciliter l'engagement du corps 10 de l'insert I dans sa cavité 20, on prévoit avantageusement au niveau des faces latérales d'insert et de la cavité un angle de dépouille relativement important.It is furthermore observed that, in order to facilitate the engagement of the
Avantageusement, ce sont ces mêmes aménagements de l'insert (ici la cavité 12 et la surface 123) que l'on utilise pour positionner l'insert dans la boite à noyaux au moment du tir du noyau. De ce fait on optimise la précision dimensionnelle obtenue quant au positionnement du noyau dans le moule en ne se référant qu'à un seul jeu de surfaces de positionnement.Advantageously, it is these same arrangements of the insert (here the
Dans certains cas, et notamment dans l'exemple d'une culasse à plusieurs cylindres, il n'est pas nécessaire de guider les noyaux d'admission dans chaque chambre selon les trois axes, car ces noyaux sont par ailleurs solidarisés entre eux par une partie de noyau commune Npa, comme illustré sur la figure 1.In some cases, and particularly in the example of a multi-cylinder cylinder head, it is not necessary to guide the intake cores in each chamber along the three axes, because these cores are otherwise secured to each other by a common core part Npa, as illustrated in FIG.
Dans ce type de configuration, et dans l'exemple particulier d'un moteur à cinq cylindres, on peut prévoir que les inserts, ordonnés de 1 à 5 (un par cylindre), puissent coopérer avec des cavités formées dans la semelle S selon les guidages et les appuis suivants :
- insert 1 :
- selon y et z
- insert 2 :
- selon z
- insert 3 :
- selon x, y et z
- insert 4 :
- selon z
- insert 5 :
- selon y et z
- insert 1:
- according to y and z
- insert 2:
- according to z
- insert 3:
- according to x, y and z
- insert 4:
- according to z
- insert 5:
- according to y and z
Par ailleurs, Le noyau de toit appuie ici directement selon l'axe z sur la moitié des pipes d'admissions (voir figure 2), ce qui garantit l'appui en z des inserts et ce faisant de l'ensemble des noyaux de pipes d'admission Na. On notera ici que l'on pourrait également, si nécessaire, prévoir des inserts aux extrémités supérieures des noyaux Na.Furthermore, the roof core here directly supports the z-axis on half of the intake pipes (see Figure 2), which guarantees the z-support of the inserts and thus the whole of the pipes cores Na inlet. It will be noted here that one could also, if necessary, provide inserts at the upper ends of the Na nuclei.
Chaque insert I est réalisé par fonderie sous pression. Pour la réalisation de chaque ensemble de noyaux Na de pipes d'admission, cinq inserts sont placés dans la boite à noyaux avant le tir. Le procédé de noyautage est ici le procédé dit de « boite froide », et
caractérisé en l'espèce par une proportion de résine de 1% et par un sable siliceux de granulométrie 55 AFS.Each insert I is made by casting under pressure. For the realization of each set of Na pipes of intake pipes, five inserts are placed in the kernel box before firing. The process of coring is here the so-called "cold box" process, and
characterized in this case by a proportion of resin of 1% and by a silica sand particle size 55 AFS.
Les culasses sont ici moulées en gravité avec un alliage standard de type AS7U3G, de composition :
La température de coulée (mesurée dans le four de maintien) est de 740°C. La semelle S est refroidie à l'eau. La cadence de coulée est de 7 à 8 pièces/heure.The casting temperature (measured in the holding oven) is 740 ° C. The sole S is cooled with water. The casting rate is 7 to 8 pieces / hour.
Par rapport aux départs d'usinage, situés au niveau de la semelle, de la culasse brute de moulage, le guidage par insert(s) réalisé selon l'invention permet d'obtenir sur une coulée de 30 culasses consécutives issues d'une journée de fabrication un positionnement des extrémités de conduits d'admission (mesuré sur pièces après refroidissement, dessablage, élimination des systèmes de masselottage et d'alimentation en métal et des inserts) caractérisé par un écart type inférieur ou égal à 0,1 mm dans les trois directions de l'espace x, y et z.Compared to the machining starts, located at the level of the sole, of the raw cylinder head, the guidance by insert (s) realized according to the invention makes it possible to obtain on a casting of 30 consecutive yokes from a day. manufacturing a positioning of the ends of intake ducts (measured on parts after cooling, grit removal, elimination of the weights and metal feeding systems and inserts) characterized by a standard deviation less than or equal to 0.1 mm in the three directions of the space x, y and z.
Par ailleurs on observe visuellement que les formes de guidage de l'insert restent très propres, et notamment exemptes de calamine, ce qui assure la reproductibilité du guidage dans le temps.Furthermore, it is observed visually that the guiding forms of the insert remain very clean, and in particular calamine free, which ensures the reproducibility of the guidance over time.
La même culasse montée selon les mêmes principes et avec le même alliage, mais avec un guidage direct des noyaux de pipes d'admission dans la semelle métallique, permet d'obtenir des précisions en positionnement en x, y et z qui sont au mieux comprises entre 0,20 et 0,25 mm. La cadence de moulage en raison de l'entretien régulier du moule en cours de fabrication chute de l'ordre de 5% à 10% par rapport à l'exemple selon l'invention.The same cylinder head mounted according to the same principles and with the same alloy, but with a direct guide of the intake pipe cores in the metal base, makes it possible to obtain precise positioning in x, y and z which are at best understood. between 0.20 and 0.25 mm. The rate of molding due to the regular maintenance of the mold during manufacture falls in the order of 5% to 10% compared to the example according to the invention.
Bien entendu, la présente invention ne se limite nullement à la forme de réalisation décrite en particulier ci-dessus, mais l'homme du métier saura y apporter de nombreuses variantes et modifications.Of course, the present invention is not limited to the embodiment described in particular above, but the skilled person will be able to make many variations and modifications.
Claims (15)
- Equipment for molding castings, in particular cylinder heads for vehicle engines, in a mold (S, T, C) having at least one sand core (Na1, Na2), in which the positioning of the or each core is obtained by the core co-operating with an element (S) of the mold, in particular a metal mold element, the equipment being characterized in that at least one core possesses a metal insert (I) secured to the core while making said core and via which said core is suitable for co-operating with the mold element in question.
- Molding equipment according to claim 1, characterized in that the or each insert (I) possesses one or more sealing appendices (111, 112) suitable for being held captive in the mass of the core(s) (Na1, Na2) during preparation thereof.
- Equipment according to claim 1 or claim 2, characterized in that at least two cores (Na1, Na2) possess a common insert (I) provided with a corresponding number of respective sealing appendices (111, 112).
- Equipment according to claim 3 or claim 4, characterized in that the co-operation between the or each insert (I) and the associated mold element (S) is shape co-operation defining a support in at least one out of three dimensions.
- Equipment according to claim 4, characterized in that the shape co-operation between the or each insert (I) and the associated mold element (S) defines support in two out of three dimensions.
- Equipment according to claim 4, characterized in that the shape co-operation between the or each insert (I) and the associated mold element (S) defines support in all three dimensions.
- Equipment according to claim 4, characterized in that the shape co-operation between the or each insert (I) and the associated mold element (S) defines wedging in at least one direction (x, y) extending transversely to a main support direction (z) for the insert.
- Equipment according to any one of claims 1 to 7, characterized in that it includes a set of cores made as a single piece and having a plurality of inserts (I) secured thereto suitable for co-operating with a common mold element (S), and in that the various inserts (I) provide support and/or wedging in different ones of three dimensions.
- Equipment according to any one of claims 1 to 8, characterized in that the cores (Na1, Na2) are admission pipe cores for a cylinder head (CL) of an engine having a plurality of cylinders.
- A method of positioning a core (Na1, Na2) in a mold for making a casting (CL) having at least one cavity defined by the positioning of a core, such as an aluminum alloy cylinder head for an engine, the method being characterized in that it comprises the following steps:· making a metal insert (I) having at least one support surface (12, 123) suitable for co-operating with a mold element (S), and at least one element (111, 112) for anchoring to the core;· making the core in a core box in which the insert (I) has previously been placed in a predetermined position so that an end region of the core becomes anchored to said insert via the anchoring element(s) thereof; and· placing the core with its insert in the mold in a position that is predetermined by co-operation between the support surface(s) of the insert and said mold element.
- A method according to claim 10, characterized in that the predetermined position of the insert in the core box is determined by co-operation between the support surface(s) (12, 123) of said insert and a support portion (211, 20) of the core box.
- A method according to claim 10 or claim 11, characterized in that the step of making the core comprises making at least two cores (Na1, Na2) which are anchored to a common insert (I).
- A method according to any one of claims 10 to 12, characterized in that the insert (I) is made by molding metal under pressure.
- A method according to any one of claims 10 to 13, characterized in that the core (Na1, Na2) is an admission pipe core.
- A method according to any one of claims 10 to 14, characterized in that the core is made by the cold box method.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0009602 | 2000-07-21 | ||
FR0009602A FR2812572B1 (en) | 2000-07-21 | 2000-07-21 | MOLDING EQUIPMENT FOR FOUNDRY PARTS WITH PERFECTED MEANS OF POSITIONING SAND CORES, AND ASSOCIATED POSITIONING PROCESS |
PCT/FR2001/002352 WO2002007914A1 (en) | 2000-07-21 | 2001-07-19 | Equipment for moulding foundry parts with improved means for positioning sand cores, and related positioning method |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1301298A1 EP1301298A1 (en) | 2003-04-16 |
EP1301298B1 true EP1301298B1 (en) | 2006-08-16 |
Family
ID=8852789
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP01956609A Expired - Lifetime EP1301298B1 (en) | 2000-07-21 | 2001-07-19 | Equipment for moulding foundry parts with improved means for positioning sand cores, and related positioning method |
Country Status (8)
Country | Link |
---|---|
US (1) | US6942007B2 (en) |
EP (1) | EP1301298B1 (en) |
AT (1) | ATE336313T1 (en) |
DE (1) | DE60122340T2 (en) |
FR (1) | FR2812572B1 (en) |
HU (1) | HU226303B1 (en) |
MX (1) | MXPA03000559A (en) |
WO (1) | WO2002007914A1 (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7143807B2 (en) * | 2004-06-04 | 2006-12-05 | General Motors Corporation | Mold design for improved bore liner dimensional accuracy |
FR2872722B1 (en) * | 2004-07-07 | 2006-10-13 | Renault Sas | DEVICE FOR MOLDING A METAL PIECE |
US7150309B2 (en) * | 2004-09-09 | 2006-12-19 | General Motors Corporation | Cylinder bore liners for cast engine cylinder blocks |
AT500943B1 (en) * | 2004-10-21 | 2007-04-15 | Austria Alu Guss Ges M B H | GIESS TOOL FOR THE PRODUCTION OF WORKPIECES MADE OF LIGHT METAL ALLOYS AND METHODS OF USING THEM |
US8434546B1 (en) | 2010-03-30 | 2013-05-07 | Honda Motor Co., Ltd. | Casting mold core retention device and method |
US20110315336A1 (en) * | 2010-06-25 | 2011-12-29 | United Technologies Corporation | Contoured Metallic Casting Core |
GB2492101B (en) * | 2011-06-21 | 2014-12-10 | Jaguar Land Rover Ltd | Apparatus and method for embedding an element |
KR101326884B1 (en) * | 2011-11-16 | 2013-11-11 | 현대자동차주식회사 | Multi-layer type cylinder head and manufacturing method therefor |
CN107321918A (en) * | 2017-08-10 | 2017-11-07 | 吴昌友 | Radiator casting sand type with positioning core print and preparation method thereof |
CN111054893A (en) * | 2019-12-30 | 2020-04-24 | 山东常林铸业有限公司 | Core assembly structure and process for end cover casting |
CN112676538B (en) * | 2020-11-17 | 2022-10-11 | 中国航发西安动力控制科技有限公司 | Process method for laminating core assembly |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH640440A5 (en) * | 1979-06-29 | 1984-01-13 | Fischer Ag Georg | Method for the production of a metal casting with at least one hole and a die for its production |
US4858670A (en) * | 1987-12-24 | 1989-08-22 | Ford Motor Company | Method of making and apparatus for monoblock engine construction |
US4981168A (en) * | 1989-07-11 | 1991-01-01 | Farley, Inc. | Mandrel holds expendable core in casting die |
US5219408A (en) * | 1992-03-02 | 1993-06-15 | Sun Donald J C | One-body precision cast metal wood |
US5392841A (en) * | 1994-06-10 | 1995-02-28 | General Motors Corporation | Mounting expendable core in die cast die |
US5704412A (en) * | 1996-02-05 | 1998-01-06 | Ford Global Technologies, Inc. | Self-aligning sand mold insert assembly |
CA2187574C (en) * | 1996-10-10 | 2000-07-18 | Constantin Eliat | Movable insert for die-casting mold with retractable core |
ITTO20010135A1 (en) * | 2001-02-15 | 2002-08-16 | Teksid Spa | MOLD STRUCTURE FOR THE PRODUCTION OF METALLIC CASTINGS OF LIGHT ALLOY AND THE CASTING PROCEDURE THAT USES IT. |
-
2000
- 2000-07-21 FR FR0009602A patent/FR2812572B1/en not_active Expired - Fee Related
-
2001
- 2001-07-19 AT AT01956609T patent/ATE336313T1/en active
- 2001-07-19 DE DE60122340T patent/DE60122340T2/en not_active Expired - Lifetime
- 2001-07-19 US US10/333,479 patent/US6942007B2/en not_active Expired - Lifetime
- 2001-07-19 HU HU0302946A patent/HU226303B1/en not_active IP Right Cessation
- 2001-07-19 EP EP01956609A patent/EP1301298B1/en not_active Expired - Lifetime
- 2001-07-19 WO PCT/FR2001/002352 patent/WO2002007914A1/en active IP Right Grant
- 2001-07-19 MX MXPA03000559A patent/MXPA03000559A/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
DE60122340D1 (en) | 2006-09-28 |
WO2002007914A1 (en) | 2002-01-31 |
MXPA03000559A (en) | 2004-12-13 |
HUP0302946A2 (en) | 2003-12-29 |
FR2812572A1 (en) | 2002-02-08 |
EP1301298A1 (en) | 2003-04-16 |
ATE336313T1 (en) | 2006-09-15 |
US20040099398A1 (en) | 2004-05-27 |
DE60122340T2 (en) | 2007-09-13 |
HU226303B1 (en) | 2008-08-28 |
FR2812572B1 (en) | 2003-03-07 |
US6942007B2 (en) | 2005-09-13 |
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