FR3052164A1 - MANUFACTURING A CMC PIECE WITH RETOUCHING INDICATIONS - Google Patents
MANUFACTURING A CMC PIECE WITH RETOUCHING INDICATIONS Download PDFInfo
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- FR3052164A1 FR3052164A1 FR1655079A FR1655079A FR3052164A1 FR 3052164 A1 FR3052164 A1 FR 3052164A1 FR 1655079 A FR1655079 A FR 1655079A FR 1655079 A FR1655079 A FR 1655079A FR 3052164 A1 FR3052164 A1 FR 3052164A1
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- intermediate piece
- slip
- ceramic
- retouching
- manufacturing
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- 238000004519 manufacturing process Methods 0.000 title claims abstract description 23
- 239000000919 ceramic Substances 0.000 claims abstract description 45
- 239000011159 matrix material Substances 0.000 claims abstract description 19
- 238000010438 heat treatment Methods 0.000 claims abstract description 16
- 239000002131 composite material Substances 0.000 claims abstract description 10
- 239000000945 filler Substances 0.000 claims abstract description 7
- 238000011049 filling Methods 0.000 claims abstract description 6
- 239000000835 fiber Substances 0.000 claims description 6
- 238000007598 dipping method Methods 0.000 claims description 4
- 238000001035 drying Methods 0.000 claims description 4
- 238000000227 grinding Methods 0.000 claims description 2
- 239000000463 material Substances 0.000 description 14
- 238000000034 method Methods 0.000 description 14
- 239000000843 powder Substances 0.000 description 6
- 239000012528 membrane Substances 0.000 description 5
- 229920001343 polytetrafluoroethylene Polymers 0.000 description 3
- 239000004810 polytetrafluoroethylene Substances 0.000 description 3
- 230000002787 reinforcement Effects 0.000 description 3
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 2
- 239000004744 fabric Substances 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 239000007769 metal material Substances 0.000 description 2
- 229940104181 polyflex Drugs 0.000 description 2
- -1 polytetrafluoroethylene Polymers 0.000 description 2
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 2
- 229910010271 silicon carbide Inorganic materials 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 239000002904 solvent Substances 0.000 description 2
- 239000000725 suspension Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- QYEXBYZXHDUPRC-UHFFFAOYSA-N B#[Ti]#B Chemical compound B#[Ti]#B QYEXBYZXHDUPRC-UHFFFAOYSA-N 0.000 description 1
- 229910052581 Si3N4 Inorganic materials 0.000 description 1
- 229920006362 Teflon® Polymers 0.000 description 1
- 229910033181 TiB2 Inorganic materials 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 239000012736 aqueous medium Substances 0.000 description 1
- 239000007864 aqueous solution Substances 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 230000008595 infiltration Effects 0.000 description 1
- 238000001764 infiltration Methods 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 238000009745 resin transfer moulding Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 239000002002 slurry Substances 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
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- C04B35/71—Ceramic products containing macroscopic reinforcing agents
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- C04B35/626—Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B
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Abstract
L'invention concerne un procédé de fabrication (S) d'une pièce en matériau composite à matrice céramique ou au moins partiellement en céramique comprenant les étapes suivantes : - prévoir une préforme fibreuse (S1), - remplir (S2) la préforme fibreuse avec une matrice céramique ou au moins partiellement en céramique de manière à obtenir une pièce intermédiaire en matériau composite, - démouler (S3) la pièce intermédiaire, - retoucher la pièce intermédiaire en appliquant une barbotine comprenant au moins une charge céramique sur tout ou partie de la surface de la pièce intermédiaire, et - appliquer un traitement thermique (S5) à la pièce intermédiaire afin d'obtenir une pièce finale.The invention relates to a manufacturing method (S) of a piece of ceramic matrix or at least partially ceramic composite material comprising the steps of: - providing a fibrous preform (S1), - filling (S2) the fibrous preform with a ceramic matrix or at least partially ceramic so as to obtain an intermediate piece of composite material, - demolding (S3) the intermediate piece, - retouching the intermediate piece by applying a slip comprising at least one ceramic filler on all or part of the surface of the intermediate piece, and - apply a heat treatment (S5) to the intermediate piece to obtain a final piece.
Description
DOMAINE DE L’INVENTION L'invention concerne la réalisation de pièces en matériau composite à matrice céramique ou au moins partiellement en céramique, désigné ci-après par matériau CMC.FIELD OF THE INVENTION The invention relates to the production of ceramic matrix or at least partly ceramic composite material parts, hereinafter referred to as CMC material.
Un domaine d'application de l'invention est la réalisation de pièces destinées à être exposées en service à des températures élevées en atmosphère oxydante, notamment dans des domaines aéronautique et spatial, en particulier des pièces de parties chaudes de turbomachines aéronautiques, étant noté que l'invention peut être appliquée dans d'autres domaines, par exemple le domaine des turbines à gaz industrielles.A field of application of the invention is the production of parts intended to be exposed in service at high temperatures in an oxidizing atmosphere, particularly in the aeronautical and space fields, in particular parts of hot parts of aeronautical turbomachines, being noted that the invention can be applied in other fields, for example the field of industrial gas turbines.
ARRIERE-PLAN TECHNOLOGIQUEBACKGROUND
Les matériaux composites à matrice céramique ou au moins partiellement en céramique possèdent des bonnes propriétés thermostructurales, c'est-à-dire des propriétés mécaniques élevées qui les rendent aptes à constituer des pièces structurales, et la capacité de conserver ces propriétés à hautes températures. L'utilisation de ces matériaux à la place de matériaux métalliques pour des pièces exposées en service à des températures élevées a donc été préconisée, d'autant que les matériaux CMC présentent une masse volumique sensiblement plus faible que les matériaux métalliques auxquels ils se substituent.Ceramic matrix or at least partially ceramic composite materials have good thermostructural properties, i.e., high mechanical properties that make them suitable for forming structural parts, and the ability to maintain these properties at high temperatures. The use of these materials instead of metal materials for parts exposed in service at high temperatures has been recommended, especially since CMC materials have a density significantly lower than the metal materials to which they substitute.
Un premier procédé bien connu pour la fabrication de pièces en matériau CMC comprend la réalisation d'une préforme fibreuse à partir d'une texture fibreuse tissée, la préforme étant consolidée par injection d’une matrice céramique dans une cavité formée de deux demi-coquilles.A first well-known method for manufacturing parts made of CMC material comprises the production of a fibrous preform from a woven fibrous texture, the preform being consolidated by injection of a ceramic matrix into a cavity formed of two half-shells .
Un deuxième procédé bien connu sous le nom de procédé poly-flex consiste à mettre en forme une préforme fibreuse sur un outillage comportant une surface ayant le profil désiré du produit final. La préforme est ensuite couverte par une membrane imperméable déformable et de la barbotine est injectée entre la membrane et la préforme. De l'autre côté de la membrane, une pression isostatique est exercée sur la membrane par un fluide lequel engendre une déformation de la face de la membrane située en regard de la préforme. Ce fluide force la matrice entre les fibres. Un tel procédé est par exemple décrit dans le document US 7,866,969.A second method, well known as the poly-flex process, consists in shaping a fiber preform on a tool having a surface having the desired profile of the final product. The preform is then covered by a deformable impermeable membrane and the slip is injected between the membrane and the preform. On the other side of the membrane, isostatic pressure is exerted on the membrane by a fluid which causes a deformation of the face of the membrane located opposite the preform. This fluid forces the matrix between the fibers. Such a method is for example described in US Pat. No. 7,866,969.
Selon un troisième procédé connu, le matériau CMC peut être obtenu par infiltration sous vide-pression (ou aspiration de poudre submicronique, APS). Dans ce procédé, un renfort fibreux est placé sur un filtre, une suspension céramique en milieux aqueux est versée sur la surface supérieure du renfort, une pression est appliquée sur la surface libre de la suspension pour la faire pénétrer dans le renfort et un vide est fait sous la face inférieure du filtre pour éliminer l'eau sous forme liquide.According to a third known method, the CMC material can be obtained by infiltration under vacuum (or aspiration of submicron powder, APS). In this method, a fibrous reinforcement is placed on a filter, a ceramic suspension in aqueous media is poured on the upper surface of the reinforcement, a pressure is applied on the free surface of the suspension to make it penetrate the reinforcement and a vacuum is made under the underside of the filter to remove water in liquid form.
Toutefois, quel que soit son procédé de fabrication, l’étape de démoulage de la pièce en matériau CMC s’avère être une opération critique. En effet, la pièce n’est pas à son stade final au moment du démoulage, un traitement thermique à haute température devant encore être appliqué par la suite pour conférer au matériau CMC ses caractéristiques finales. De ce fait, des agglomérats constitués de plusieurs grains (qui ne seront consolidés que lors du futur traitement thermique) peuvent se détacher de la surface de la pièce en CMC et former des indications.However, whatever its manufacturing process, the demolding step of the piece of CMC material turns out to be a critical operation. Indeed, the part is not in its final stage at the time of demolding, a high temperature heat treatment still to be applied thereafter to give the CMC material its final characteristics. As a result, agglomerates consisting of several grains (which will be consolidated only during the future heat treatment) can be detached from the surface of the CMC part and form indications.
Il a donc été proposé d’appliquer un agent démoulant et/ou un tissu comprenant du polytétrafluoroéthylène (PTFE - commercialisé sous la marque Teflon® notamment) afin de réduire le risque d’apparition d’indications. Toutefois, des indications peuvent encore apparaître ponctuellement, notamment dans les zones de la pièce en matériau CMC subissant de fortes contraintes au démoulage.It has therefore been proposed to apply a release agent and / or a fabric comprising polytetrafluoroethylene (PTFE - marketed under the trademark Teflon® in particular) in order to reduce the risk of indications appearing. However, indications may still appear punctually, especially in the parts of the CMC material part undergoing strong stresses to demoulding.
RESUME DE L’INVENTIONSUMMARY OF THE INVENTION
Un objectif de l’invention est donc de proposer un procédé de fabrication d’une pièce en matériau composite à matrice céramique ou au moins partiellement en céramique qui supprime les indications susceptibles d’apparaître à la surface de la pièce finie et permette ainsi de réduire le risque de mise en rebut de la pièce.An object of the invention is therefore to provide a method of manufacturing a piece of ceramic matrix or at least partially ceramic composite material which eliminates the indications that may appear on the surface of the finished part and thus reduces the risk of scrapping the part.
Pour cela, l’invention propose un procédé de fabrication d’une pièce en matériau composite à matrice céramique ou au moins partiellement en céramique comprenant les étapes suivantes : - prévoir une préforme fibreuse, - remplir la préforme fibreuse avec une matrice céramique ou au moins partiellement en céramique de manière à obtenir une pièce intermédiaire en matériau composite, - démouler la pièce intermédiaire, et - appliquer un traitement thermique à la pièce intermédiaire afin d’obtenir une pièce finale.For this, the invention proposes a method of manufacturing a piece of ceramic matrix or at least partially ceramic composite material comprising the following steps: - providing a fiber preform, - filling the fiber preform with a ceramic matrix or at least partially ceramic so as to obtain an intermediate piece of composite material, - unmolding the intermediate piece, and - apply heat treatment to the intermediate piece to obtain a final piece.
Le procédé de fabrication comprend en outre une étape de retouche de tout ou partie d’une surface de la pièce intermédiaire, ladite étape de retouche comprenant une application d’une barbotine comprenant au moins une charge céramique sur tout ou partie de la surface de la pièce intermédiaire.The manufacturing method further comprises a step of retouching all or part of a surface of the intermediate part, said retouching step comprising an application of a slip comprising at least one ceramic filler on all or part of the surface of the intermediate piece.
Certaines caractéristiques préférées mais non limitatives du procédé de fabrication sont les suivantes, prises individuellement ou en combinaison : - l’étape de traitement thermique de la pièce intermédiaire est réalisée après l’étape de retouche, - la barbotine est appliquée par trempage de tout ou partie de la surface de la pièce intermédiaire dans un bain de barbotine, - le procédé comprend en outre une étape d’homogénéisation de la barbotine déposée sur la surface de la pièce intermédiaire qui a été trempée par vibrations, - une viscosité du bain de barbotine lors de l’étape de retouche est comprise entre 100 mPa.s et 500 mPa.s, - la barbotine est appliquée à l’aide d’un pistolet et/ou d’un pinceau, - une viscosité de la barbotine lors de l’étape de retouche est inférieure ou égale à 100 mPa.s, - le procédé comprend en outre une étape de séchage en étuve de la pièce intermédiaire préalablement à l’étape de traitement thermique, - le procédé comprend en outre une étape de rectification de tout ou partie de la pièce intermédiaire avant l’étape de traitement thermique, et/ou - un taux volumique de la charge céramique de la barbotine est compris entre 5% et 50%.Some preferred but non-limiting characteristics of the manufacturing process are as follows, taken individually or in combination: the step of heat treatment of the intermediate part is carried out after the retouching step, the slip is applied by dipping all or part of the surface of the intermediate piece in a slip bath, - the method further comprises a step of homogenizing the slip deposited on the surface of the intermediate part which has been quenched by vibrations, - a viscosity of the slip bath during the retouching step is between 100 mPa.s and 500 mPa.s, - the slip is applied using a gun and / or a brush, - a viscosity of the slip at the same time. retouching step is less than or equal to 100 mPa.s, - the method further comprises a step of drying in an oven of the intermediate part prior to the treatment step thermal, - the method further comprises a step of rectification of all or part of the intermediate piece before the heat treatment step, and / or - a volume ratio of the ceramic charge of the slip is between 5% and 50% .
BREVE DESCRIPTION DES DESSINS D’autres caractéristiques, buts et avantages de la présente invention apparaîtront mieux à la lecture de la description détaillée qui va suivre, et au regard de la figure unique annexée donnée à titre d’exemples non limitatifs et sur laquelle a été représenté un organigramme d’un procédé de fabrication d’une pièce conforme à un mode de réalisation de l’invention.BRIEF DESCRIPTION OF THE DRAWINGS Other features, objects and advantages of the present invention will appear better on reading the detailed description which follows, and with reference to the single appended figure given by way of non-limiting examples and on which has been shown a flowchart of a method of manufacturing a part according to an embodiment of the invention.
DESCRIPTION DETAILLEE D’UN MODE DE REALISATIONDETAILED DESCRIPTION OF AN EMBODIMENT
Afin de réaliser une pièce en matériau composite à matrice céramique ou au moins partiellement en céramique (matrice CMC), le procédé S comprend une première étape au cours de laquelle la matrice CMC est déposée par voie liquide selon un procédé S conventionnel, tel que le procédé RTM, le procédé poly-flex, le procédé APS ou tout autre équivalent.In order to produce a piece of ceramic matrix or at least partially ceramic (CMC matrix) composite material, the method S comprises a first step in which the CMC matrix is deposited by a liquid process according to a conventional method S, such as the RTM process, poly-flex process, APS process or any other equivalent.
Pour cela, de manière conventionnelle, une préforme fibreuse est placée S1 dans un moule ou sur un outillage puis remplie S2 avec la matrice céramique ou au moins partiellement céramique de manière à obtenir une pièce intermédiaire. Le cas échéant, un agent démoulant est enduit sur les parois du moule ou de l’outillage et/ou un tissu comprenant du polytétrafluoroéthylène est placé sur la préforme afin de réduire les risques de formation d’indications sur la pièce intermédiaire.For this, conventionally, a fibrous preform is placed S1 in a mold or on a tool then filled S2 with the ceramic matrix or at least partially ceramic so as to obtain an intermediate piece. If appropriate, a release agent is coated on the walls of the mold or tool and / or a fabric comprising polytetrafluoroethylene is placed on the preform to reduce the risk of forming indications on the intermediate part.
Cette pièce intermédiaire est ensuite démoulée S3 puis subit un traitement thermique S5 (du type frittage) à une température supérieure ou égale à 800°C afin de conférer à la pièce ses caractéristiques finales.This intermediate part is then demolded S3 and then undergoes a heat treatment S5 (sintering type) at a temperature greater than or equal to 800 ° C to give the piece its final characteristics.
Les étapes de remplissage, de démoulage et de traitement thermique étant conventionnelles, elles ne seront pas davantage détaillées ici.The filling, demolding and heat treatment steps being conventional, they will not be further detailed here.
Dans ce qui suit, on désignera par « pièce intermédiaire » la pièce en matériau CMC après l’étape S2 de remplissage de la préforme fibreuse (et évacuation du solvant) avec la matrice céramique ou au moins partiellement céramique mais avant application du traitement thermique S5, par opposition à la « pièce finale » qui correspond à la pièce CMC après traitement thermique S5.In what follows, will be designated by "intermediate piece" CMC material part after step S2 filling the fiber preform (and solvent evacuation) with the ceramic matrix or at least partially ceramic but before application of heat treatment S5 , as opposed to the "final part" which corresponds to the CMC part after S5 heat treatment.
Lorsque la pièce intermédiaire présente des indications, c’est-à-dire qu’un ou plusieurs agglomérats de matrice céramique ou partiellement céramique se détachent de la surface de la pièce intermédiaire, le procédé S comprend en outre une étape S4 de retouche de la pièce intermédiaire au cours de laquelle une barbotine comprenant une charge céramique est appliquée sur tout ou partie de la surface de la pièce intermédiaire. En d’autres termes, soit la barbotine est appliquée sur toute la surface de la pièce intermédiaire, soit la barbotine n’est appliquée que dans les zones de la pièce intermédiaire dans laquelle se sont formées les indications et qui doivent donc être retouchées.When the intermediate piece has indications, that is to say that one or more agglomerates of ceramic or partial ceramic matrix are detached from the surface of the intermediate piece, the method S further comprises a step S4 retouching the intermediate piece during which a slurry comprising a ceramic filler is applied on all or part of the surface of the intermediate piece. In other words, either the slip is applied over the entire surface of the intermediate piece, or the slip is applied only in the areas of the intermediate part in which the indications are formed and which must be retouched.
Une barbotine comprenant une charge céramique est une poudre céramique présente dans une solution, typiquement une solution aqueuse ou organique. Dans ce qui suit, l’invention sera décrite dans le cas d’une solution aqueuse. Ceci n’est cependant pas limitatif. La poudre peut notamment comprendre l’un ou plusieurs des matériaux suivants : - du carbure, par exemple du carbure de silicium SiC, et/ou - du borure, par exemple du diborure de titane TiB2, et/ou - du nitrure, par exemple du nitrure de silicium SÎ3Ni4, et/ou - un oxyde d’alumine ou de zircone.A slip comprising a ceramic filler is a ceramic powder present in a solution, typically an aqueous or organic solution. In what follows, the invention will be described in the case of an aqueous solution. This is not, however, limiting. The powder may in particular comprise one or more of the following materials: carbide, for example silicon carbide SiC, and / or boride, for example titanium diboride TiB 2, and / or nitride, for example S3Ni4 silicon nitride, and / or an oxide of alumina or zirconia.
Le taux volumique de la poudre céramique (ou charge) dans la barbotine dépend de la poudre céramique utilisée dans ladite barbotine et peut être compris entre 5% et 50%.The volume ratio of the ceramic powder (or filler) in the slip depends on the ceramic powder used in said slip and may be between 5% and 50%.
La charge céramique de la barbotine peut comprendre un même matériau que la matrice céramique de la pièce intermédiaire, ou en variante comprendre un matériau différent.The ceramic charge of the slip may comprise the same material as the ceramic matrix of the intermediate piece, or alternatively comprise a different material.
Dans un mode de réalisation, la poudre peut présenter une granulométrie inférieure au micron afin de faciliter l’étape S2 de remplissage.In one embodiment, the powder may have a sub-micron particle size to facilitate step S2 of filling.
Cette étape S4 de retouche est réalisée avant l’étape S5 de traitement thermique. L’application S4 de la barbotine peut être réalisée par trempage de tout ou partie de la surface de la pièce intermédiaire dans un bain de barbotine comprenant des charges céramiques. Pour cela, soit une zone à retoucher, soit la pièce intermédiaire complète est trempée dans le bain de barbotine.This step S4 retouching is carried out before step S5 heat treatment. The S4 application of the slip may be carried out by dipping all or part of the surface of the intermediate piece in a slip bath comprising ceramic fillers. For this purpose, either an area to be retouched or the complete intermediate part is soaked in the slip bath.
Afin d’assurer un bon recouvrement de la zone à retoucher ou de la pièce intermédiaire par trempage, la viscosité du bain de barbotine est comprise entre 100 mPa.s et 500 mPa.s. La mesure de la viscosité est réalisée ici avec un viscosimètre Brookfield à température ambiante (entre 20°C et 23°C) dans le solvant de la barbotine, à une vitesse de rotation de 100 rpm dans une cuve présentant un volume de cuve de 150 mL. L’épaisseur du dépôt de charge céramique appliqué sur la surface immergée de la pièce intermédiaire peut, de manière optionnelle, être ensuite homogénéisée. Pour cela, la pièce intermédiaire peut par exemple être vibrée, typiquement à l’aide d’un panier ou table vibrant(e).In order to ensure a good recovery of the area to be retouched or the intermediate part by dipping, the viscosity of the slip bath is between 100 mPa.s and 500 mPa.s. The measurement of the viscosity is carried out here with a Brookfield viscometer at room temperature (between 20 ° C. and 23 ° C.) in the solvent of the slip, at a rotation speed of 100 rpm in a tank having a tank volume of 150. mL. The thickness of the ceramic charge deposit applied to the immersed surface of the intermediate piece may, optionally, then be homogenized. For this, the intermediate piece may for example be vibrated, typically using a basket or vibrating table (e).
En variante, l’application S4 de la barbotine peut être réalisée à l’aide d’un pistolet ou d’un pinceau sur tout ou partie de la pièce intermédiaire.Alternatively, the application S4 of the slip can be performed using a gun or a brush on all or part of the intermediate piece.
Pour cela, la viscosité de la barbotine est de préférence inférieure ou égale à 100 mPa.s.For this, the viscosity of the slip is preferably less than or equal to 100 mPa.s.
Dans une variante de réalisation, la pièce intermédiaire peut être égouttée afin d’éviter un surplus local de matière dans des zones de la pièce intermédiaire ne nécessitant pas de retouche. Cette étape d’égouttage peut notamment être privilégiée lorsque la barbotine est appliquée sur toute la surface de la pièce intermédiaire.In an alternative embodiment, the intermediate piece can be drained in order to avoid a local surplus of material in areas of the intermediate piece that does not require retouching. This dewatering step can in particular be preferred when the slip is applied over the entire surface of the intermediate piece.
Après application de la barbotine, la pièce intermédiaire peut être séchée. Par exemple, l’étape de séchage peut être réalisée dans une étuve, par exemple à une température comprise entre 40°C et 90°C afin d’éviter l’évaporation trop rapide de l’eau (création de bulles) pendant une durée comprise entre 1h et 10h, selon la taille de la pièce et la température. Pour déterminer si la pièce est bien sèche, un suivi de masse peut être réalisé jusqu’à stabilisation de la masse.After application of the slip, the intermediate part can be dried. For example, the drying step may be carried out in an oven, for example at a temperature of between 40 ° C. and 90 ° C. in order to prevent the water from being evaporated too rapidly (creation of bubbles) for a period of time. between 1h and 10h, depending on the size of the room and the temperature. To determine if the part is dry, a mass tracking can be carried out until mass stabilization.
Le cas échéant, lorsque l’épaisseur du dépôt de charge céramique obtenu par application de la barbotine est trop importante par rapport aux dimensions requises pour la pièce, la pièce intermédiaire peut être rectifiée préalablement à l’étape de traitement thermique, par exemple par ponçage afin de retirer le surplus de matière. L’étape de rectification peut notamment être réalisée après séchage de la pièce intermédiaire.If necessary, when the thickness of the ceramic charge deposit obtained by application of the slip is too great in relation to the dimensions required for the part, the intermediate part may be ground prior to the heat treatment step, for example by sanding to remove excess material. The grinding step may in particular be carried out after drying of the intermediate piece.
Claims (10)
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EP2181974A1 (en) * | 2008-10-31 | 2010-05-05 | AVIO S.p.A. | Method for the production of components made of ceramic-matrix composite material |
FR3001409A1 (en) * | 2013-01-29 | 2014-08-01 | Herakles | METHOD FOR MANUFACTURING ALVEOLAR STRUCTURE OF CURVED SHAPE IN COMPOSITE MATERIAL |
WO2016102842A1 (en) * | 2014-12-23 | 2016-06-30 | Snecma | Method for manufacturing part made of composite material |
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US4936939A (en) * | 1989-05-05 | 1990-06-26 | Ceracom Technologies, Inc. | Fabric-reinforced ceramic matrix composite material |
EP0495700A1 (en) * | 1991-01-18 | 1992-07-22 | Societe Europeenne De Propulsion | Method of densification of a porous substrate by a matrix containing carbon |
US6497776B1 (en) * | 1998-12-18 | 2002-12-24 | Rolls-Royce Plc | Method of manufacturing a ceramic matrix composite |
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