EP1595620A1 - Broken mould moulding method - Google Patents
Broken mould moulding method Download PDFInfo
- Publication number
- EP1595620A1 EP1595620A1 EP05103958A EP05103958A EP1595620A1 EP 1595620 A1 EP1595620 A1 EP 1595620A1 EP 05103958 A EP05103958 A EP 05103958A EP 05103958 A EP05103958 A EP 05103958A EP 1595620 A1 EP1595620 A1 EP 1595620A1
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- EP
- European Patent Office
- Prior art keywords
- mullite
- layers
- layer
- solidification
- particles
- 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.)
- Granted
Links
- 238000000034 method Methods 0.000 title claims description 33
- 238000000465 moulding Methods 0.000 title description 2
- KZHJGOXRZJKJNY-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical compound O=[Si]=O.O=[Si]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O.O=[Al]O[Al]=O KZHJGOXRZJKJNY-UHFFFAOYSA-N 0.000 claims abstract description 32
- 229910052863 mullite Inorganic materials 0.000 claims abstract description 32
- 239000002245 particle Substances 0.000 claims abstract description 24
- 239000011230 binding agent Substances 0.000 claims abstract description 22
- 239000000203 mixture Substances 0.000 claims abstract description 22
- 239000000919 ceramic Substances 0.000 claims abstract description 16
- 238000001035 drying Methods 0.000 claims abstract description 14
- 239000004576 sand Substances 0.000 claims abstract description 14
- 229910052845 zircon Inorganic materials 0.000 claims abstract description 12
- GFQYVLUOOAAOGM-UHFFFAOYSA-N zirconium(iv) silicate Chemical compound [Zr+4].[O-][Si]([O-])([O-])[O-] GFQYVLUOOAAOGM-UHFFFAOYSA-N 0.000 claims abstract description 11
- 238000007598 dipping method Methods 0.000 claims abstract description 10
- 229910052500 inorganic mineral Inorganic materials 0.000 claims abstract description 4
- 239000011707 mineral Substances 0.000 claims abstract description 4
- 238000007711 solidification Methods 0.000 claims description 31
- 230000008023 solidification Effects 0.000 claims description 31
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical group O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 26
- 238000004519 manufacturing process Methods 0.000 claims description 19
- 235000013312 flour Nutrition 0.000 claims description 18
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 16
- 239000002671 adjuvant Substances 0.000 claims description 14
- 238000005266 casting Methods 0.000 claims description 14
- 235000013339 cereals Nutrition 0.000 claims description 12
- 239000008119 colloidal silica Substances 0.000 claims description 10
- 230000002787 reinforcement Effects 0.000 claims description 10
- 239000002184 metal Substances 0.000 claims description 7
- 229910052751 metal Inorganic materials 0.000 claims description 7
- 230000015572 biosynthetic process Effects 0.000 claims description 6
- 238000000151 deposition Methods 0.000 claims description 6
- 238000010411 cooking Methods 0.000 claims description 5
- 230000003014 reinforcing effect Effects 0.000 claims description 5
- 230000008021 deposition Effects 0.000 claims description 4
- 238000010410 dusting Methods 0.000 claims description 4
- 238000002791 soaking Methods 0.000 claims description 4
- 238000010438 heat treatment Methods 0.000 claims description 3
- 238000009826 distribution Methods 0.000 claims description 2
- 238000009434 installation Methods 0.000 claims description 2
- 239000006259 organic additive Substances 0.000 claims 1
- 239000000463 material Substances 0.000 abstract description 6
- 239000011248 coating agent Substances 0.000 abstract 2
- 238000000576 coating method Methods 0.000 abstract 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 abstract 1
- 229910052782 aluminium Inorganic materials 0.000 abstract 1
- 239000004411 aluminium Substances 0.000 abstract 1
- 229910052710 silicon Inorganic materials 0.000 abstract 1
- 239000010703 silicon Substances 0.000 abstract 1
- 239000010410 layer Substances 0.000 description 51
- 239000003795 chemical substances by application Substances 0.000 description 8
- HIGRAKVNKLCVCA-UHFFFAOYSA-N alumine Chemical compound C1=CC=[Al]C=C1 HIGRAKVNKLCVCA-UHFFFAOYSA-N 0.000 description 4
- 230000035945 sensitivity Effects 0.000 description 4
- 230000035939 shock Effects 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 238000009736 wetting Methods 0.000 description 4
- 241001508691 Martes zibellina Species 0.000 description 3
- 229910045601 alloy Inorganic materials 0.000 description 3
- 239000000956 alloy Substances 0.000 description 3
- 238000000518 rheometry Methods 0.000 description 3
- QGZKDVFQNNGYKY-UHFFFAOYSA-O Ammonium Chemical compound [NH4+] QGZKDVFQNNGYKY-UHFFFAOYSA-O 0.000 description 2
- 244000007835 Cyamopsis tetragonoloba Species 0.000 description 2
- 239000002270 dispersing agent Substances 0.000 description 2
- 230000007613 environmental effect Effects 0.000 description 2
- 229920000058 polyacrylate Polymers 0.000 description 2
- 239000000377 silicon dioxide Substances 0.000 description 2
- 239000000080 wetting agent Substances 0.000 description 2
- 101100536354 Drosophila melanogaster tant gene Proteins 0.000 description 1
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 1
- VGGSQFUCUMXWEO-UHFFFAOYSA-N Ethene Chemical compound C=C VGGSQFUCUMXWEO-UHFFFAOYSA-N 0.000 description 1
- IAYPIBMASNFSPL-UHFFFAOYSA-N Ethylene oxide Chemical compound C1CO1 IAYPIBMASNFSPL-UHFFFAOYSA-N 0.000 description 1
- BPQQTUXANYXVAA-UHFFFAOYSA-N Orthosilicate Chemical compound [O-][Si]([O-])([O-])[O-] BPQQTUXANYXVAA-UHFFFAOYSA-N 0.000 description 1
- BOTDANWDWHJENH-UHFFFAOYSA-N Tetraethyl orthosilicate Chemical compound CCO[Si](OCC)(OCC)OCC BOTDANWDWHJENH-UHFFFAOYSA-N 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 125000003158 alcohol group Chemical group 0.000 description 1
- 150000001298 alcohols Chemical class 0.000 description 1
- 150000004645 aluminates Chemical class 0.000 description 1
- 150000001413 amino acids Chemical class 0.000 description 1
- 229910010293 ceramic material Inorganic materials 0.000 description 1
- 238000004138 cluster model Methods 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 239000000084 colloidal system Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- CRHLEZORXKQUEI-UHFFFAOYSA-N dialuminum;cobalt(2+);oxygen(2-) Chemical compound [O-2].[O-2].[O-2].[O-2].[O-2].[Al+3].[Al+3].[Co+2].[Co+2] CRHLEZORXKQUEI-UHFFFAOYSA-N 0.000 description 1
- 238000010981 drying operation Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 125000001495 ethyl group Chemical group [H]C([H])([H])C([H])([H])* 0.000 description 1
- 150000002191 fatty alcohols Chemical class 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000001033 granulometry Methods 0.000 description 1
- 238000007654 immersion Methods 0.000 description 1
- 239000011229 interlayer Substances 0.000 description 1
- 239000004014 plasticizer Substances 0.000 description 1
- 229920001281 polyalkylene Polymers 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 229910000601 superalloy Inorganic materials 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
- 229920001285 xanthan gum Polymers 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/02—Sand moulds or like moulds for shaped castings
- B22C9/04—Use of lost patterns
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22C—FOUNDRY MOULDING
- B22C9/00—Moulds or cores; Moulding processes
- B22C9/12—Treating moulds or cores, e.g. drying, hardening
Definitions
- the present invention relates to the manufacture of parts such as blading complex geometries according to the technique known as lost wax foundry.
- a model wax or other equivalent material easily removable by the following. If necessary we group together several models into one cluster. We made around this model a ceramic mold by soaking in a first slip to form a first layer of material in contact with its area. Sand the surface of this layer to reinforce and facilitate the hanging of the next layer, and we dry the whole: what constitutes respectively the stuccage and drying operations. We then repeat the soaking operation in slip of possible compositions different, operation always associated with the successive operations of stuccage and drying. Thus, a ceramic shell consisting of a plurality of layers.
- the slips are composed of particles of ceramic materials, flour, such as alumina, mullite, zircon or the like, with a mineral colloidal binder and adjuvants, if any, depending on the rheology desired.
- These adjuvants make it possible to control and stabilize characteristics of the different types of layers, while avoiding the effects of different physicochemical characteristics of raw materials constituting the slips. It can be a wetting agent, a plasticizer or a texturizer based, for the latter, the desired thickness for the deposit.
- the carapace mold is then dewaxed, which is an operation by which eliminates the material constituting the original model. After elimination of the model, we obtain a ceramic mold whose cavity reproduces all the details of the model. The mold then undergoes heat treatment at high temperature or "cooking", which gives it the mechanical properties required.
- the carapace mold is thus ready for the manufacture of the metal part by casting.
- the step The next step is to sink a molten metal into the mold cavity and then to the solidify.
- solidification techniques In the field of lost-wax foundry, there is currently a distinction several solidification techniques, therefore several casting techniques, according to the nature of the alloy and the expected properties of the part resulting from the casting. It may be directed solidification with columnar structure (DS), directed solidification with monocrystalline structure (SX) or solidification equiaxe (EX) respectively.
- DS columnar structure
- SX directed solidification with monocrystalline structure
- EX solidification equiaxe
- the shell is broken by a shaking operation, and we complete the manufacture of the metal part.
- shells can be made at through several processes. Each carapace must have properties specific to ensure the desired type of solidification. For example, for equiaxed solidification, several different processes can be one using a silicate binder of ethyl, another using a silica binder colloid. For directed solidification, shells can be made from different fillers, based on silico-aluminous, silica-zircon or silica.
- the invention achieves these objectives with the following method.
- the method is characterized by the fact that ceramic particles of the slips comprise a refractory oxide or a a mixture of refractory oxides without zircon, none of the layers comprising zircon.
- the slip for the formation of the reinforcement layers is much more fluid than the second slip.
- the binder for different slips is a solution colloidal mineral such as colloidal silica.
- the stucco grains for the layers of contact, intermediate and reinforcement are made from mullite grains and no zircon.
- the stuccage operations are carried out with stucco grains covering a size range between 80 and 1000 microns.
- stucco is preferably applied by dusting to the first layers, and is preferably applied by fluidized bed, for layers from the fourth.
- Stucco is applied automatically, so that the movements of the robot can make a carapace mold having a porosity after baking, between 20 and 35%. More shell is porous, the more it reduces its sensitivity to thermal shocks such as those products during different types of pouring.
- the baking cycle of the mold comprises a heating up to a temperature between 1000 and 1150 ° C, preferably between 1030 ° C and 1070 ° C.
- the first slip can be formed from mullite flours and of alumina without zircon, with or without germinating.
- the contact is composed mainly of mullite flour in quantity between 40 and 80% by weight, possibly of alumina flour, a binder based on colloidal silica, and organic adjuvants.
- the contact layer is composed of a mixture of alumina flours and mullite in quantities between 40 and 80% by weight and between 2 and 30% by weight, remainder comprising a binder based on colloidal silica, a germinant, and organic adjuvants.
- the second and third slip are common to any solidification process, and comprise a mixture of alumina and mullite flours in an amount of between 45 and 95% by weight, and mullite grains in an amount of between 0 and 25% by weight.
- the mold structure thus defined finds, indifferently, a use for the manufacture of a part with solidification of directed type with a columnar structure, the contact layer being formed mainly from a mullite flour, for the manufacture of a monocrystalline structured type solidification-type part, the contact layer being formed predominantly from a mullite flour or else for producing a piece with equiaxed type solidification, the contact layer being formed from a mixture of alumina flour and mullite.
- the invention also relates to a method for manufacturing parts by casting molten metal that, irrespective of the type of solidification, directed to columnar structure, directed at monocrystalline or equiaxed structure, molds with a common shell skeleton: intermediate layer and common reinforcement layer.
- the invention also relates to an installation for the production of parts by casting a molten metal in a shell mold comprising a station of manufacture of molds and casting stations for different solidifications, said stations being fed with molds having reinforcement layers identical.
- the method of manufacturing shell molds for use common to all types of parts includes a first step of manufacturing the model in wax or other equivalent material known in the field.
- wax or other equivalent material known in the field.
- the models are shaped to the dimensions of the final pieces, alloys.
- the carapace manufacturing steps are preferably carried out by a robot whose movements are common to all types of parts, programmed to have an optimal action on the quality of the deposits made, and to free oneself the geometric aspect of the various blades.
- slips are prepared in which they are quenched successively the models or the cluster to make a deposit of matter ceramic.
- layer # 1 contact, once the model removed from the first slip after an immersion phase, the covered model undergoes a dewatering phase then topping. Then, sprinkles of stucco are applied to do not disturb the thin layer of contact.
- mullite whose granulometry in this first layer is fine. It is between 80 and 250 microns. The surface condition of the pieces in final depends in part.
- the No. 1 layer is dried.
- the dipping is then carried out in a second slip to form a layer N ° 2, called intermediate.
- the composition is the same regardless of the solidification mode adopted.
- a stucco is deposited by dusting and dried.
- mullite whose particle size is average. It can be between 120 and 1000 microns.
- the state of porosity final shells depend in part on it.
- the model is then quenched in a third slip to form the layer No. 3 which is the first so-called reinforcement layer.
- the same stucco is then applied to layer 2 by dusting, and dried.
- the soaking operations are repeated in the third slip, stuccage and drying to form the layers of "reinforcement".
- the stuccage is carried out by fluidized bed.
- a glazing operation is performed which does not include a stuccage operation.
- the carapace in final can consist of 5 to 12 layers.
- Soak programs are optimized for each type of layer, in order to to overcome the geometrical aspect of the different types of pieces, and are therefore common to all references.
- the interlayer drying range is optimized for each type of layer, to overcome the geometric aspect of the different types of parts.
- the range is therefore common.
- the range allows indeed for each type of layer, a drying of molds with geometries as different as vanes movers, distributors, or structural parts.
- the baking cycle of molds is the same for all types of solidification, and thus free from the type of room. It includes a rising phase in temperature, a plateau at the cooking temperature and a phase of cooling.
- the cooking cycle is chosen to optimize the properties mechanical shells so as to allow cold handling without risk of breakage, and in order to minimize sensitivity to thermal shock that can be generated during the different stages of casting.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
- Mold Materials And Core Materials (AREA)
Abstract
Description
La présente invention porte sur la fabrication de pièces telles que des aubages métalliques à géométries complexes selon la technique connue sous le nom de fonderie à cire perdue.The present invention relates to the manufacture of parts such as blading complex geometries according to the technique known as lost wax foundry.
Pour la fabrication des aubages de turboréacteurs, tels que les pièces de rotors ou de stators, ou bien des pièces de structure selon cette technique, on en réalise d'abord un modèle en cire ou autre matériau équivalent facilement éliminable par la suite. Le cas échéant on regroupe plusieurs modèles en une grappe. On confectionne autour de ce modèle un moule céramique par trempage dans une première barbotine pour former une première couche de matière au contact de sa surface. On sable la surface de cette couche afin de la renforcer et de faciliter l'accrochage de la couche suivante, et on sèche l'ensemble : ce qui constitue respectivement les opérations de stuccage et de séchage. On répète ensuite l'opération de trempage dans des barbotines de compositions éventuellement différentes, opération toujours associée aux opérations successives de stuccage et de séchage. On réalise ainsi une carapace céramique constituée d'une pluralité de couches. Les barbotines sont composées de particules de matériaux céramiques, notamment une farine, tel que l'alumine, la mullite, le zircon ou autre, avec un liant colloïdal minéral et des adjuvants le cas échéant en fonction de la rhéologie souhaitée. Ces adjuvants permettent de maítriser et de stabiliser les caractéristiques des différents types de couches, tout en s'affranchissant des effets des différentes caractéristiques physico-chimiques des matières premières constituant les barbotines. Il peut s'agir d'un agent mouillant, d'un fluidifiant ou d'un texturant en fonction, pour ce dernier, de l'épaisseur désirée pour le dépôt.For the manufacture of turbojet blades, such as rotor parts or stators, or structural parts according to this technique, it is realized first a model wax or other equivalent material easily removable by the following. If necessary we group together several models into one cluster. We made around this model a ceramic mold by soaking in a first slip to form a first layer of material in contact with its area. Sand the surface of this layer to reinforce and facilitate the hanging of the next layer, and we dry the whole: what constitutes respectively the stuccage and drying operations. We then repeat the soaking operation in slip of possible compositions different, operation always associated with the successive operations of stuccage and drying. Thus, a ceramic shell consisting of a plurality of layers. The slips are composed of particles of ceramic materials, flour, such as alumina, mullite, zircon or the like, with a mineral colloidal binder and adjuvants, if any, depending on the rheology desired. These adjuvants make it possible to control and stabilize characteristics of the different types of layers, while avoiding the effects of different physicochemical characteristics of raw materials constituting the slips. It can be a wetting agent, a plasticizer or a texturizer based, for the latter, the desired thickness for the deposit.
On procède ensuite au décirage du moule carapace, qui est une opération par laquelle on élimine le matériau constituant le modèle d'origine. Après élimination du modèle, on obtient un moule céramique dont la cavité reproduit tous les détails du modèle. Le moule subit ensuite un traitement thermique à haute température ou « cuisson », qui lui confère les propriétés mécaniques nécessaires.The carapace mold is then dewaxed, which is an operation by which eliminates the material constituting the original model. After elimination of the model, we obtain a ceramic mold whose cavity reproduces all the details of the model. The mold then undergoes heat treatment at high temperature or "cooking", which gives it the mechanical properties required.
Le moule carapace est ainsi prêt pour la fabrication de la pièce métallique par coulée. Après contrôle de l'intégrité interne et externe du moule carapace, l'étape suivante consiste à couler un métal en fusion dans la cavité du moule puis à le solidifier. Dans le domaine de la fonderie à cire perdue on distingue actuellement plusieurs techniques de solidification, donc plusieurs techniques de coulée, selon la nature de l'alliage et les propriétés attendues de la pièce résultant de la coulée. Il peut s'agir de solidification dirigée à structure colonnaire (DS), de solidification dirigée à structure monocristalline (SX) ou de solidification équiaxe (EX) respectivement. Les deux premières familles de pièces concernent des superalliages pour pièces soumises à de fortes contraintes tant thermiques que mécaniques dans le turboréacteur, comme les aubes de turbines HP.The carapace mold is thus ready for the manufacture of the metal part by casting. After checking the internal and external integrity of the carapace mold, the step The next step is to sink a molten metal into the mold cavity and then to the solidify. In the field of lost-wax foundry, there is currently a distinction several solidification techniques, therefore several casting techniques, according to the nature of the alloy and the expected properties of the part resulting from the casting. It may be directed solidification with columnar structure (DS), directed solidification with monocrystalline structure (SX) or solidification equiaxe (EX) respectively. The first two families of pieces concern superalloys for parts subject to high thermal stress that mechanical in the turbojet engine, such as HP turbine blades.
Après coulée de l'alliage, on casse la carapace par une opération de décochage, et on parachève la fabrication de la pièce métallique.After casting of the alloy, the shell is broken by a shaking operation, and we complete the manufacture of the metal part.
Lors de l'étape de moulage, plusieurs types de carapaces peuvent être réalisés au travers de plusieurs procédés. Chaque carapace doit posséder des propriétés spécifiques qui permettent d'assurer le type de solidification désiré. Par exemple, pour la solidification équiaxe, plusieurs procédés différents peuvent être mis en oeuvre, l'un utilisant un liant silicate d'éthyle, un autre utilisant un liant silice colloïdale. Pour la solidification dirigée, les carapaces peuvent être réalisées à partir de charges différentes, à base silico-alumineuse, silice-zircon ou silice.During the molding step, several types of shells can be made at through several processes. Each carapace must have properties specific to ensure the desired type of solidification. For example, for equiaxed solidification, several different processes can be one using a silicate binder of ethyl, another using a silica binder colloid. For directed solidification, shells can be made from different fillers, based on silico-aluminous, silica-zircon or silica.
Dans un but de simplification et d'uniformisation des procédés mis en oeuvre, il existe un besoin pour une carapace à structure dite « unique » dont les propriétés lui permettraient d'être utilisée dans les différents cas de solidification.In order to simplify and standardize the processes used, it is There is a need for a shell with a "unique" structure whose properties would allow it to be used in different cases of solidification.
D'autre part, pour des raisons de respect des normes environnementales et de coûts, il existe aussi un besoin d'éviter l'emploi de liants à base alcool tel que le silicate d'éthyle.On the other hand, for reasons of respect for environmental standards and costs, there is also a need to avoid the use of alcohol-based binders such as ethyl silicate.
Pour des raisons de coûts de rejet, il est aussi souhaitable de mettre au point une structure de carapace ne comprenant pas de zircon. Ce matériau, même faiblement radio-actif, nécessite en effet l'établissement de procédures de traitement des déchets très contraignantes industriellement et financièrement.For reasons of rejection costs, it is also desirable to develop a shell structure not including zircon. This material, even low level of radioactivity, requires the establishment of treatment of highly binding waste industrially and financially.
L'invention parvient à ces objectifs avec le procédé suivant.The invention achieves these objectives with the following method.
Le procédé de fabrication de moule carapace céramique à plusieurs couches, dont
au moins une couche de contact, une couche intermédiaire et plusieurs couches
de renfort à partir d'un modèle en cire ou autre matériau semblable, consiste à
réaliser les opérations suivantes :
Conformément à l'invention le procédé est caractérisé par le fait que les particules céramiques des barbotines comprennent un oxyde réfractaire ou un mélange d'oxydes réfractaires sans zircon, aucune des couches ne comportant de zircon.According to the invention, the method is characterized by the fact that ceramic particles of the slips comprise a refractory oxide or a a mixture of refractory oxides without zircon, none of the layers comprising zircon.
De préférence la barbotine pour la formation des couches de renfort est beaucoup plus fluide que la deuxième barbotine.Preferably the slip for the formation of the reinforcement layers is much more fluid than the second slip.
On a constaté qu'un moule carapace présentant cette composition et cette structure, à la couche de contact près, pouvait être conçu pour être commun à tous les types de pièces coulées selon les techniques rapportées plus haut. On peut ainsi avantageusement ajuster les propriétés mécaniques du moule, en particulier, sa sensibilité aux chocs thermiques, pour satisfaire aux conditions de coulée répondant aux contraintes des différents procédés de solidification (EX, DS ou SX).It has been found that a shell mold having this composition and this structure, at the near contact layer, could be designed to be common to all types of castings according to the techniques reported above. We can thus advantageously adjust the mechanical properties of the mold, particular, its sensitivity to thermal shocks, to satisfy the conditions of casting corresponding to the constraints of the various solidification processes (EX, DS or SX).
De préférence et pour satisfaire aux contraintes économiques et environnementales, le liant pour les différentes barbotines est une solution colloïdale minérale telle que la silice colloïdale. De même pour satisfaire aux contraintes économiques liées aux rejets, les grains de stucco pour les couches de contact, intermédiaire et de renfort sont constitués à partir de grains de mullite et non de zircon.Preferably and to satisfy the economic and environmental, the binder for different slips is a solution colloidal mineral such as colloidal silica. Similarly to satisfy economic constraints related to the rejects, the stucco grains for the layers of contact, intermediate and reinforcement are made from mullite grains and no zircon.
Afin de maítriser la porosité du moule, et de ce fait maítriser la sensibilité de la carapace aux chocs thermiques, les opérations de stuccage sont réalisées avec des grains de stucco couvrant une gamme granulométrique comprise entre 80 et 1000 microns. Par ailleurs, le stucco est appliqué de préférence par saupoudrage pour les premières couches, et est appliqué de préférence par lit fluidisé, pour les couches à partir de la quatrième. On applique le stucco automatiquement, de sorte que les mouvements du robot permettent de réaliser un moule carapace présentant une porosité après cuisson, comprise entre 20 et 35%. Plus la carapace est poreuse, plus on diminue sa sensibilité aux chocs thermiques tels que ceux produits lors des différents types de coulées.In order to control the porosity of the mold, and thereby control the sensitivity of the thermal shocks, the stuccage operations are carried out with stucco grains covering a size range between 80 and 1000 microns. In addition, stucco is preferably applied by dusting to the first layers, and is preferably applied by fluidized bed, for layers from the fourth. Stucco is applied automatically, so that the movements of the robot can make a carapace mold having a porosity after baking, between 20 and 35%. More shell is porous, the more it reduces its sensitivity to thermal shocks such as those products during different types of pouring.
En particulier, pour pouvoir être appliqué à deux modes distincts de solidification, le cycle de cuisson du moule comprend un chauffage jusqu'à une température comprise entre 1000 et 1150°C, de préférence entre 1030°C et 1070°C.In particular, in order to be applied to two distinct modes of solidification, the baking cycle of the mold comprises a heating up to a temperature between 1000 and 1150 ° C, preferably between 1030 ° C and 1070 ° C.
Il suffit d'adapter seulement la couche de contact au mode de solidification. Ainsi la première barbotine peut être formée à partir de farines de mullite et d'alumine sans zircon, avec ou sans germinant.It suffices to adapt only the contact layer to the solidification mode. Thus the first slip can be formed from mullite flours and of alumina without zircon, with or without germinating.
Dans un cas particulier, pour des solidifications de types DS ou SX, la couche de contact est composée majoritairement de farine de mullite en quantité comprise entre 40 et 80% en poids, éventuellement de farine d'alumine, un liant à base de silice colloïdale, et des adjuvants organiques.In a particular case, for DS or SX type solidifications, the contact is composed mainly of mullite flour in quantity between 40 and 80% by weight, possibly of alumina flour, a binder based on colloidal silica, and organic adjuvants.
Dans le cas particulier de la solidification équiaxe, la couche de contact est composée d'un mélange de farines d'alumine et de mullite en quantités respectivement comprises entre 40 et 80% en poids et entre 2 et 30% en poids, le reste comprenant un liant à base de silice colloïdale, un germinant, et des adjuvants organiques.In the particular case of equiaxed solidification, the contact layer is composed of a mixture of alumina flours and mullite in quantities between 40 and 80% by weight and between 2 and 30% by weight, remainder comprising a binder based on colloidal silica, a germinant, and organic adjuvants.
Conformément à une autre caractéristiques, les deuxième et troisième barbotines
sont communes à tout procédé de solidification, et comprennent un mélange de
farines d'alumine et de mullite en quantité comprise entre 45 et 95% en poids, et
des grains de mullite en quantité comprise entre 0 et 25% en poids.
La structure de moule ainsi définie trouve, indifféremment, une utilisation
pour la fabrication d'une pièce avec solidification de type dirigé à
structure colonnaire, la couche de contact étant formée majoritairement à partir
d'une farine de mullite,
pour la fabrication d'une pièce avec solidification de type dirigé à
structure monocristalline, la couche de contact étant formée majoritairement à
partir d'une farine de mullite ou bien
pour la fabrication d'une pièce avec solidification de type équiaxe, la
couche de contact étant formée à partir d'un mélange de farine d'alumine et de
mullite.According to another characteristic, the second and third slip are common to any solidification process, and comprise a mixture of alumina and mullite flours in an amount of between 45 and 95% by weight, and mullite grains in an amount of between 0 and 25% by weight.
The mold structure thus defined finds, indifferently, a use
for the manufacture of a part with solidification of directed type with a columnar structure, the contact layer being formed mainly from a mullite flour,
for the manufacture of a monocrystalline structured type solidification-type part, the contact layer being formed predominantly from a mullite flour or else
for producing a piece with equiaxed type solidification, the contact layer being formed from a mixture of alumina flour and mullite.
L'invention porte aussi sur un procédé de fabrication de pièces par coulée de métal en fusion selon lequel, quel que soit le type de solidification, dirigée à structure colonnaire, dirigée à structure monocristalline ou équiaxe, on utilise des moules présentant un squelette de carapaces commun : couche intermédiaire et couche de renfort communes.The invention also relates to a method for manufacturing parts by casting molten metal that, irrespective of the type of solidification, directed to columnar structure, directed at monocrystalline or equiaxed structure, molds with a common shell skeleton: intermediate layer and common reinforcement layer.
L'invention porte aussi sur une installation pour la fabrication de pièces par coulée d'un métal en fusion dans un moule carapace comprenant un poste de fabrication de moules et des postes de coulée pour des solidifications différentes, lesdits postes étant alimentés avec des moules présentant des couches de renfort identiques.The invention also relates to an installation for the production of parts by casting a molten metal in a shell mold comprising a station of manufacture of molds and casting stations for different solidifications, said stations being fed with molds having reinforcement layers identical.
On décrit ci-après le procédé plus en détail.The process is described in more detail below.
Le procédé de fabrication des moules carapaces permettant une utilisation commune à tous types de pièces comprend une première étape de fabrication du modèle en cire ou en un autre matériau équivalent connu dans le domaine. Le plus généralement connu est la cire. Selon le type de pièce, on peut regrouper les modèles en grappe de manière à pouvoir en fabriquer plusieurs simultanément. Les modèles sont façonnés aux dimensions des pièces définitives, au retrait près des alliages.The method of manufacturing shell molds for use common to all types of parts includes a first step of manufacturing the model in wax or other equivalent material known in the field. The more generally known is wax. Depending on the type of part, you can group the cluster models so that several can be made simultaneously. The models are shaped to the dimensions of the final pieces, alloys.
Les étapes de fabrication de la carapace sont de préférence menées par un robot dont les mouvements sont communs à tous types de pièces, programmés pour avoir une action optimale sur la qualité des dépôts réalisés, et pour s'affranchir de l'aspect géométrique des différents aubages.The carapace manufacturing steps are preferably carried out by a robot whose movements are common to all types of parts, programmed to have an optimal action on the quality of the deposits made, and to free oneself the geometric aspect of the various blades.
On prépare parallèlement des barbotines dans lesquelles on trempe successivement les modèles ou la grappe pour effectuer un dépôt de matière céramique.In parallel, slips are prepared in which they are quenched successively the models or the cluster to make a deposit of matter ceramic.
On distingue une première barbotine pour la solidification EQX. We distinguish a first slip for solidification EQX.
Elle comprend en pourcentage pondéral :
- un mélange de farines d'alumine (40 - 80%) et de mullite (2 - 30%) ;
- un germinant, aluminate de cobalt (0 - 10%) ;
- un liant silice colloïdale (18 - 30%) ;
- de l'eau (0 - 5%) ;
- trois adjuvants : agents mouillant, fluidifiant et texturant ;
- a mixture of flours of alumina (40-80%) and mullite (2 - 30%);
- a germinant, cobalt aluminate (0-10%);
- a colloidal silica binder (18 - 30%);
- water (0 - 5%);
- three adjuvants: wetting, thinning and texturing agents;
Pour la solidification dirigée à structure colonnaire ou monocristalline, la composition de la première barbotine en pourcentage pondéral est la suivante :
- un mélange de farines d'alumine (2 - 30%) et de mullite (40 - 80%) ;
- un liant silice colloïdale (18 - 30%) ;
- de l'eau (0-5%) ;
- trois adjuvants : agents mouillant, fluidifiant et texturant ;
- a mixture of flours of alumina (2 - 30%) and mullite (40 - 80%);
- a colloidal silica binder (18 - 30%);
- water (0-5%);
- three adjuvants: wetting, thinning and texturing agents;
La deuxième barbotine intermédiaire, commune à tous types de solidification, comprend en pourcentage pondéral les composants suivants :
- un mélange de farines d'alumine (50 - 75%) et de mullite (5 - 20%) ;
- un liant silice colloïdale (20 - 30%) ;
- de l'eau (0 - 5%) ;
- trois adjuvants : agents mouillant, fluidifiant et texturant ;
- a mixture of flours of alumina (50-75%) and mullite (5-20%);
- a colloidal silica binder (20 - 30%);
- water (0 - 5%);
- three adjuvants: wetting, thinning and texturing agents;
La troisième barbotine de renfort, commune à tous types de solidification, comprend les composants suivants en pourcentage pondéral :
- un mélange de farines d'alumine (30 - 45%) et de mullite (15 - 30%) ;
- des grains de Mullite (14 - 24%) ;
- un liant silice colloïdale (10 - 20%) ;
- de l'eau (5 - 15%) ;
- quatre adjuvants : agents mouillant, fluidifiant, texturant et de frittage ;
- a mixture of flours of alumina (30 - 45%) and mullite (15 - 30%);
- Mullite grains (14 - 24%);
- a colloidal silica binder (10-20%);
- water (5 - 15%);
- four adjuvants: wetting, thinning, texturizing and sintering agents;
Les 3 premiers adjuvants ont respectivement les fonctions suivantes :
- Le fluidifiant permet d'obtenir plus rapidement la rhéologie désirée lors de la fabrication de la couche. Il agit en tant que dispersant. Il peut appartenir à la famille des acides aminés, à la gamme des polyacrylates d'ammonium, ou à la famille des tri - acides carboxyliques à groupements alcools ;
- Le mouillant permet de faciliter le nappage de la couche lors du trempé. Il peut appartenir à la famille des alcools gras poly - alkylènes, ou alcools alkoxylates ;
- Le texturant permet d'optimiser la rhéologie de la couche afin d'obtenir des dépôts adaptés. Il peut appartenir à la famille des polymères de l'oxyde d'éthylène, des gommes de xanthane, ou des gommes de guar ;
- The fluidizer makes it possible to obtain the desired rheology more quickly during the manufacture of the layer. It acts as a dispersant. It may belong to the family of amino acids, to the range of ammonium polyacrylates, or to the family of carboxylic tri-acids with alcohol groups;
- The wetting agent makes it easier to coat the layer during dipping. It may belong to the family of polyalkylene fatty alcohols, or alkoxylated alcohols;
- The texturizer makes it possible to optimize the rheology of the layer in order to obtain suitable deposits. It may belong to the family of polymers of ethylene oxide, xanthan gums, or guar gums;
Pour la couche N°1, de contact, une fois le modèle retiré de la première barbotine après une phase d'immersion, le modèle recouvert subit une phase d'égouttage puis de nappage. Puis, on applique des grains de stucco par saupoudrage afin de ne pas perturber la fine couche de contact. Pour l'opération de stuccage, on utilise de la mullite dont la granulométrie dans cette première couche est fine. Elle est comprise entre 80 et 250 microns. L'état de surface des pièces en final en dépend en partie.For layer # 1, contact, once the model removed from the first slip after an immersion phase, the covered model undergoes a dewatering phase then topping. Then, sprinkles of stucco are applied to do not disturb the thin layer of contact. For the stuccage operation, one uses mullite whose granulometry in this first layer is fine. It is between 80 and 250 microns. The surface condition of the pieces in final depends in part.
On sèche la couche N°1.The No. 1 layer is dried.
On procède ensuite au trempé dans une seconde barbotine pour former une couche N°2, dite intermédiaire. La composition est la même quel que soit le mode de solidification adopté.The dipping is then carried out in a second slip to form a layer N ° 2, called intermediate. The composition is the same regardless of the solidification mode adopted.
Comme précédemment, on dépose un stucco par saupoudrage, et on sèche. Pour l'opération de stuccage, on utilise de la mullite dont la granulométrie est moyenne. Elle peut être comprise entre 120 et 1000 microns. L'état de porosité des carapaces en final en dépend en partie.As before, a stucco is deposited by dusting and dried. For the stuccowork operation, we use mullite whose particle size is average. It can be between 120 and 1000 microns. The state of porosity final shells depend in part on it.
On trempe ensuite le modèle dans une troisième barbotine pour former la couche N°3 qui est la première couche dite de renfort.The model is then quenched in a third slip to form the layer No. 3 which is the first so-called reinforcement layer.
On applique ensuite le stucco identique à la couche N°2 par saupoudrage, et on sèche. On répète les opérations de trempage dans la troisième barbotine, de stuccage et de séchage pour former les couches « de renfort ». Pour ces couches de renfort, le stuccage s'effectue par lit fluidisé.The same stucco is then applied to layer 2 by dusting, and dried. The soaking operations are repeated in the third slip, stuccage and drying to form the layers of "reinforcement". For these layers reinforcement, the stuccage is carried out by fluidized bed.
Pour la dernière couche, on procède à une opération de glaçage qui ne comprend
pas d'opération de stuccage.
La carapace en final peut être constituée de 5 à 12 couches.For the last layer, a glazing operation is performed which does not include a stuccage operation.
The carapace in final can consist of 5 to 12 layers.
Les trempés pour les différentes couches sont effectués de manières différentes et sont adaptés afin d'obtenir une répartition homogène des épaisseurs et d'éviter la formation de bulles, notamment dans les zones d'enfermées.Soaked for different layers are made in different ways and are adapted to obtain a homogeneous distribution of the thicknesses and to avoid the bubble formation, especially in enclosed areas.
Les programmes de trempés sont optimisés pour chaque type de couche, afin de s'affranchir de l'aspect géométrique des différents types de pièces, et sont donc communs à toutes références.Soak programs are optimized for each type of layer, in order to to overcome the geometrical aspect of the different types of pieces, and are therefore common to all references.
La gamme de séchage intercouche est optimisée pour chaque type de couche, afin de s'affranchir de l'aspect géométrique des différents types de pièces. La gamme est donc commune. La gamme permet en effet pour chaque type de couche, un séchage de moules à géométries aussi différentes que des aubes mobiles, des distributeurs, ou bien des pièces de structure.The interlayer drying range is optimized for each type of layer, to overcome the geometric aspect of the different types of parts. The range is therefore common. The range allows indeed for each type of layer, a drying of molds with geometries as different as vanes movers, distributors, or structural parts.
On procède à un séchage final après la formation de la dernière couche, commun à tous types de pièces.Final drying is carried out after the formation of the last, common layer to all types of rooms.
Le cycle de cuisson des moules est le même pour tous les types de solidification, et s'affranchit donc aussi du type de pièce. Il comprend une phase de montée en température, un palier à la température de cuisson et une phase de refroidissement. Le cycle de cuisson est choisi pour optimiser les propriétés mécaniques des carapaces de manière à permettre les manipulations à froid sans risques de casses, et de manière à minimiser la sensibilité aux chocs thermiques pouvant être générés lors des différentes étapes de coulées.The baking cycle of molds is the same for all types of solidification, and thus free from the type of room. It includes a rising phase in temperature, a plateau at the cooking temperature and a phase of cooling. The cooking cycle is chosen to optimize the properties mechanical shells so as to allow cold handling without risk of breakage, and in order to minimize sensitivity to thermal shock that can be generated during the different stages of casting.
On constate, que l'on peut réaliser une cuisson unique au lieu des deux types de cuisson qui étaient réalisées auparavant pour préparer les carapaces EQX, DS et SX aux différents modes de coulée.It can be seen that a single cooking can be done instead of both types of previously made to prepare the EQX, DS and SX to different casting modes.
Claims (19)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0405143A FR2870147B1 (en) | 2004-05-12 | 2004-05-12 | LOST WAX FOUNDRY PROCESS |
FR0405143 | 2004-05-12 |
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EP1595620A1 true EP1595620A1 (en) | 2005-11-16 |
EP1595620B1 EP1595620B1 (en) | 2011-07-20 |
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EP05103958A Active EP1595620B1 (en) | 2004-05-12 | 2005-05-11 | Broken mould moulding method |
Country Status (5)
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US (1) | US7318466B2 (en) |
EP (1) | EP1595620B1 (en) |
JP (1) | JP4937528B2 (en) |
CA (1) | CA2507170C (en) |
FR (1) | FR2870147B1 (en) |
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EP2208556A1 (en) * | 2009-01-06 | 2010-07-21 | General Electric Company | Casting molds for use in directional solidification processes and methods of making |
FR3071423A1 (en) * | 2017-09-22 | 2019-03-29 | Safran | FOUNDRY BARBOTINE |
RU2774243C2 (en) * | 2017-09-22 | 2022-06-16 | Сафран | Casting mixture |
WO2024149952A1 (en) * | 2023-01-12 | 2024-07-18 | Safran | Method for manufacturing a mould comprising cracking particles |
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EP1935530A1 (en) * | 2006-12-21 | 2008-06-25 | Siemens Aktiengesellschaft | Method for manufacturing a ceramic casting die and utilisation of the same |
JP5178366B2 (en) * | 2008-07-14 | 2013-04-10 | 伊藤忠セラテック株式会社 | Stucco material for mold manufacturing for precision casting and mold for precision casting using the same |
CN104646633B (en) * | 2013-11-20 | 2017-06-30 | 沈阳工业大学 | The single crystal blade of local retractable labyrinth ceramic core preparation technology |
JP6317995B2 (en) * | 2014-05-08 | 2018-04-25 | 伊藤忠セラテック株式会社 | Slurry filler material for manufacturing precision casting mold, slurry obtained by using the filler, and precision casting mold |
JP2016002572A (en) * | 2014-06-18 | 2016-01-12 | 伊藤忠セラテック株式会社 | Slurry composition for manufacturing precision casting mold and manufacturing method of the same |
JP6368596B2 (en) * | 2014-09-11 | 2018-08-01 | 伊藤忠セラテック株式会社 | Slurry composition for producing precision casting mold and method for producing the same |
FR3068271B1 (en) | 2017-06-29 | 2021-12-10 | Safran Aircraft Engines | FOUNDRY PROCESS WITH HOT MOLD CASTING |
CN108115088B (en) * | 2017-12-23 | 2020-01-21 | 青田保俐铸造有限公司 | Investment shell casting process of gypsum composite polymer viscous mortar |
FR3085286B1 (en) | 2018-08-28 | 2021-08-06 | Safran Aircraft Engines | METHOD OF MANUFACTURING A MULTI-LAYER CERAMIC LAYER TEST, TEST OBTAINED BY THE IMPLEMENTATION OF SUCH MANUFACTURING PROCESS AND USE OF SUCH A TEST FOR A UNIAXIAL HOT COMPRESSION TEST |
FR3103400B1 (en) | 2019-11-21 | 2022-08-19 | Safran Aircraft Engines | FOUNDRY MOLD, METHOD FOR MAKING THE MOLD AND FOUNDRY METHOD |
FR3145299A1 (en) | 2023-01-27 | 2024-08-02 | Safran Aircraft Engines | Foundry mold |
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WO2024149952A1 (en) * | 2023-01-12 | 2024-07-18 | Safran | Method for manufacturing a mould comprising cracking particles |
FR3144930A1 (en) * | 2023-01-12 | 2024-07-19 | Safran | Process for manufacturing a mold comprising cracking particles |
Also Published As
Publication number | Publication date |
---|---|
FR2870147B1 (en) | 2007-09-14 |
FR2870147A1 (en) | 2005-11-18 |
CA2507170C (en) | 2012-12-11 |
CA2507170A1 (en) | 2005-11-12 |
US7318466B2 (en) | 2008-01-15 |
US20050252634A1 (en) | 2005-11-17 |
JP4937528B2 (en) | 2012-05-23 |
JP2005324253A (en) | 2005-11-24 |
EP1595620B1 (en) | 2011-07-20 |
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