![]() PROCESS FOR MANUFACTURING A COMPOSITE MATERIAL PART BY INJECTING A BARBOTIN CHARGED IN A POROUS MOLD
专利摘要:
A method of manufacturing a composite material part comprises the following steps: - injection under pressure of a slip (150) containing a powder of refractory ceramic particles (1500) in a fibrous texture, - drainage of the liquid (1501) of the slip (150) having passed through the fibrous texture (10) and retention of the powder of refractory ceramic particles within said texture so as to obtain a fibrous preform (15) loaded with refractory ceramic particles (1500). The injection tool comprises a mold of porous material (110) having an inner housing (113) in which the fibrous texture is placed, the slip (150) being injected into the fibrous texture (10) by at least one port of injection (134) present on the injection tool and opening into the inner housing (113) of the mold of porous material (110). The tooling further comprises an enclosure of rigid material (130) in which the porous material mold (110) is maintained during the pressure injection of the slip (150) and the drainage of the liquid (1501) of said slip, the liquid (1501) of the slip being evacuated by at least one vent (135) present on the enclosure of rigid material. 公开号:FR3041890A1 申请号:FR1559430 申请日:2015-10-05 公开日:2017-04-07 发明作者:Nicolas Droz;Ludovic Philippe Liais;Adrien Paixao;Michael Podgorski;Sofia Haifi 申请人:Safran SA;SNECMA SAS; IPC主号:
专利说明:
Background of the invention The present invention relates to a method for manufacturing a composite material part, in particular of the oxide / oxide or ceramic matrix (CMC) type, that is to say having a fiber reinforcement formed from densified refractory ceramic fibers. by a matrix also made of refractory ceramic material. The oxide / oxide composite material parts are generally produced by draping in a mold of a plurality of fibrous layers made from refractory oxide fibers, the layers being each impregnated beforehand with a slip loaded with refractory oxide particles. All of the layers thus disposed is then compacted using a counter-mold or a vacuum cover and an autoclave. The filled preform thus obtained is then subjected to sintering in order to form a refractory oxide matrix in the preform and obtain a piece of oxide / oxide composite material. This technique can also be used to produce ceramic matrix composite (CMC) parts. In this case, the fibrous layers are made from silicon carbide (SiC) or carbon fibers and are impregnated with a slurry loaded with carbide particles (eg SiC), boride (eg ΤΊΒ2) or nitride particles. (eg Si3N4). However, this type of production method makes it possible to produce only oxide / oxide or CMC composite material having a small thickness and two-dimensional (2D) fibrous reinforcement. The mechanical characteristics of these types of composite material remain limited in certain directions. In particular, these materials have a low resistance to delamination and do not withstand shear forces well. The production of fibrous textures obtained by three-dimensional weaving between continuous warp and weft yarns makes it possible to increase the mechanical strength of the material and in particular its resistance to delamination. In this case and also for thick 2D fibrous textures, only processes using a pressure gradient, such as infusion-type processes, such as "RTM" injection molding or submicron powder suction called "APS", make it possible to penetrate a slurry loaded into the fibrous texture whose thickness can reach several tens of millimeters depending on the intended applications. However, the pressure gradient between the part of the fibrous texture through which the loaded slip is injected and the other part of the fibrous texture by which the liquid phase of the slip is to be removed is difficult to control over the entire fibrous texture. If the pressure is not balanced over the entire surface of the fibrous texture facing the bottom of the mold having one or more evacuation vents through which or the liquid phase of the slurry must be evacuated, it is created a pressure difference between the areas near the vents and the more distant areas. In this case, the evacuation of the liquid phase is difficult because it must be removed from the texture without disturbing the distribution of solid particles (refractory oxide, carbide, boride, nitride, etc.) deposited via the slip. Indeed, during its evacuation, the liquid phase can take with it particles and / or modify the distribution of the latter in the fibrous texture and lead to the appearance of large porosities in the final material due to lack of matrix in certain places. Object and summary of the invention The object of the present invention is to overcome the aforementioned drawbacks and to propose a solution that makes it possible to produce composite material parts, particularly of the oxide / oxide or CMC type, from a thick fibrous texture and / or complex geometry, and this in a fast and reliable manner while allowing a good control of the deposition and the distribution of the solid particles in the fibrous texture in order to obtain a material with a very low macroporosity rate. For this purpose, the invention provides a method of manufacturing a composite material part comprising the following steps: - formation of a fibrous texture from refractory ceramic fibers, - placement of the fibrous texture in an injection tooling - Pressurized injection of a slip containing a powder of refractory ceramic particles in the fibrous texture, - drainage of the liquid of the slip passed through the fibrous texture and retention of the powder of refractory ceramic particles within said texture. in order to obtain a fibrous preform loaded with refractory particles, - drying of the fibrous preform, - demolding of the fibrous preform, and - sintering of the refractory ceramic particles present in the fibrous preform in order to form a refractory matrix in said preform, characterized in that that the injection tool comprises a mold made of porous material comprising a lo internal composition in which the fibrous texture is placed, the slip being injected into the fibrous texture by at least one injection port present on the injection tool and opening into the inner housing of the porous material mold, the tooling comprising in addition, an enclosure of rigid material in which the mold of porous material is maintained during the pressure injection of the slip and the drainage of the liquid from said slip, the liquid of the slurry being discharged through at least one vent present on the enclosure made of rigid material. By using a mold made of porous material, the method of the invention makes it possible to eliminate the liquid phase of the slip introduced into the fibrous texture without removing the refractory solid particles also present in the texture. In addition, the mold of porous material surrounding the entire fibrous texture, the liquid of the slip can be drained out of said texture in all directions, that is to say at any point of the interface between the texture and the mold. This makes it possible to promote a deposit by homogeneous and dense sedimentation of the refractory ceramic particles in the fibrous texture and to obtain, consequently, a high matrix volume ratio in the final piece made of composite material and to significantly increase the residence time. drainage. The composite material part has, therefore, improved mechanical properties. In addition, the mold of porous material being held in a rigid material enclosure, it can withstand the injection pressures of the slip loaded in the texture as well as those exerted by pumping for the evacuation of the liquid medium of the slip. According to a particular characteristic of the method of the invention, the mold made of porous material has a size smaller than the internal volume of the enclosure made of rigid material, the volume present between the mold made of porous material and the enclosure made of rigid material being filled by a porous compact medium. The use of a porous medium facilitates in particular the integration of the porous material mold in the injection tooling by matching any type of mold shape even complex while ensuring a good transfer of forces between the mold and the enclosure injection equipment. This transfer makes it possible to ensure the increase in pressure without deformation of the porous mold. The sealing problems are thus considerably reduced. Moreover, the presence of a porous medium around the mold makes it possible to better evacuate the liquid from the slip from the mold of porous material, thus facilitating its cleaning after each injection and, consequently, its reuse. The void volume present in the porous medium is preferably greater than the volume of the liquid phase of the slip injected into the fiber texture. The porous medium may consist in particular of sand of a foam, or any granular material having a stacking rate to provide a housing or passage to the filtrate. According to a particular aspect of the process of the invention, the mold may be made of a material chosen from at least one of the following materials: porous resin and plaster. During the fiber-forming step, the yarns can be woven in three-dimensional or multi-layer weave. The fibrous texture can also be produced by stacking woven layers in a two-dimensional weave, the texture having a thickness of at least 0.5 mm and preferably at least 1 mm. The yarns of the preform may be fiber yarns made of one or more of the following materials: alumina, mullite, silica, aluminosilicate, borosilicate, silicon carbide, and carbon. The refractory ceramic particles may be of a material chosen from: alumina, mullite, silica, an aluminosilicate, an aluminophosphate, zirconia, a carbide, a boride and a nitride. In an exemplary embodiment, the piece of composite material obtained may constitute a turbomachine blade. BRIEF DESCRIPTION OF THE DRAWINGS Other characteristics and advantages of the invention will emerge from the following description of particular embodiments of the invention, given by way of non-limiting examples, with reference to the appended drawings, in which: FIG. 1 is a schematic perspective exploded view of an injection tool according to an embodiment of the invention, - Figure 2 is a schematic sectional view showing the tool of Figure 1 closed with a fiber texture positioned 3 is a diagrammatic sectional view showing the steps of impregnating a fibrous texture with a slip loaded in the tool of FIG. 2. Detailed description of embodiments The method of manufacturing a composite material part, especially of the oxide / oxide or CMC type according to the present invention, starts with the production of a fibrous texture intended to form the reinforcement of the part. The fibrous structure is made in a known manner by weaving by means of a jacquard loom on which a bundle of warp yarns or strands has been arranged in a plurality of layers, the warp yarns being bound by yarns of yarn. frame or vice versa. The fibrous texture can be made by stacking strata or plies obtained by two-dimensional weaving (2D). The fibrous texture can also be made directly in one piece by three-dimensional weaving (3D). By "two-dimensional weaving" is meant here a conventional weaving mode whereby each weft yarn passes from one side to another son of a single chain layer or vice versa. The method of the invention is particularly adapted to allow the introduction of a loaded slip in 2D fiber textures, namely textures obtained by stacking 2D layers or plies, of significant thickness, that is to say 2D fibrous structures having a thickness of at least 0.5 mm, preferably at least 1 mm. By "three-dimensional weaving" or "3D weaving" or "multilayer weaving" is meant here a weaving mode whereby at least some of the weft yarns bind warp yarns on several layers of warp yarns or conversely following a weave corresponding to a weave weave which can be chosen in particular from one of the following armor: interlock, multi-fabric, multi-satin and multi-twill. By "weave or interlock fabric" is meant here a 3D weave armor, each layer of warp threads binding several layers of weft threads with all the threads of the same warp column having the same movement in the plane of the weave. armor. By "armor or multi-fabric fabric" is meant here a 3D weave with several layers of weft threads whose basic armor of each layer is equivalent to a conventional canvas type armor but with some points of the armor that bind the layers of weft threads together. By "multi-satin weave or fabric" is meant here a 3D weave with several layers of weft yarns whose basic weave of each layer is equivalent to a classic satin-like weave but with certain points of the weave which bind the layers of weft threads together. By "weave or multi-twill fabric" is meant here a 3D weave with several layers of weft threads whose basic armor of each layer is equivalent to a classic twill type armor but with some points of the armor that bind the layers of weft threads together. 3D textures have a complex geometry in which it is difficult to introduce and evenly distribute solid particles in suspension. The process of the invention is also very well suited for introducing a filled slip into 3D woven fiber textures. The yarns used to weave the fibrous texture intended to form the fibrous reinforcement of the piece of composite material may in particular be formed of fibers consisting of one of the following materials: alumina, mullite, silica, an aluminosilicate, a borosilicate, silicon carbide, carbon or a mixture of several of these materials. Once the fibrous texture is produced, it is placed in an injection tool according to the invention which makes it possible, as explained hereinafter, to deposit refractory particles within the fibrous texture. For this purpose and as illustrated in FIGS. 1 and 2, a fibrous texture 10 is placed in an injection tool 100. In the example described here, the fibrous texture 10 is produced according to one of the techniques defined above (stacking). 2D layers or 3D weave) with Nextel 610 ™ alumina wires. The fibrous texture 10 is here intended to form the fibrous reinforcement of a blade of oxide / oxide composite material. The tooling 100 comprises a mold made of porous material 110 formed in two parts 111 and 112 each respectively comprising a cavity 1110 and a cavity 1120. The cavities 1110 and 1120 delimit a molding cavity 113 (FIG. 2) when the two parts 111 and 112 are assembled against each other, cavity in which the fibrous texture is intended to be placed. The impressions 1110 and 1120 have a shape corresponding to the shape of the workpiece to be made from the fibrous texture. The two parts 111 and 112 serve to size the preform and thus the part to be obtained and to adjust the fiber content in the part to be obtained. In the example described here, the portion 111 of the porous material mold 110 comprises a channel 1111 for injecting a slurry loaded into the fibrous texture as explained hereinafter in detail. Injection tooling 100 also comprises an enclosure made of rigid material 130 in which the mold of porous material 110 is maintained. The enclosure 130 comprises a bottom 131, a side wall 132 integral with the bottom 131 and a cover 133. The enclosure 130 may be made of any type of material having sufficient rigidity to withstand the injection pressures of the slip and the pumping (vacuum draw) for the evacuation of the liquid phase thereof. The enclosure may in particular be made of metal or plastic material. The lid 133 comprises an injection port 134 through which the slip is intended to be injected in order to penetrate the porosity of the fibrous texture 10. In the example illustrated in FIGS. 1 and 2, the slip is intended to be injected through an injection port 134 opening into the molding cavity 113. However, it is not beyond the scope of the invention when the slip is injected through a plurality of injection ports opening into the cavity molding. The enclosure 130 comprises a single vent 135 of the liquid medium of the slip, present here on the side wall 132 in the vicinity of the bottom 131. Of course, it is not beyond the scope of the invention when a plurality of Exit vents are implemented at different locations in the enclosure. In the embodiment described here, the porous material mold 110 has a size smaller than the internal volume of the metallic material enclosure 130. In this case, the volume present between the porous material mold and the metal material enclosure is filled by a porous medium 120 to allow the circulation and evacuation of the liquid phase of the slip. The porous medium 120 may consist in particular of sand, foam or granular material. Regarding the foam, any type of foam, rigid or flexible, which has a porosity network for the passage of the liquid medium of the slip can be used as a porous medium. Similarly, any type of granular material having a stacking rate compatible with the passage of the liquid phase of the slip can be used as a porous medium. The porous medium 120 comprises a conduit 121 in communication with both the injection port 134 of the enclosure 130 and the channel 1111 of the porous material mold 110 in order to allow the injection of the slip into the fibrous texture 10. The void volume present in the porous medium is preferably greater than the amount or volume of the liquid phase of the slip that is to be injected into the fiber texture. This makes it possible to evacuate the entire liquid phase from the walls of the porous mold when a vacuum draw is made at the evacuation port or vents and / or during the application of the pressure in the injection port. . According to an alternative embodiment, the mold of porous material has external dimensions equivalent to the internal volume of the enclosure. In this case, the mold of porous material is directly in contact with the internal walls of the enclosure. In this case, the porous material mold is preferably dimensioned so that it has a void volume greater than the quantity or volume of the liquid phase of the slip which must be injected into the fibrous texture. This optimizes the filling of the fibrous texture when a vacuum draw is made at the evacuation vent or vents. The mold of porous material 110 may for example be made from a porous resin. In this case, the portions 111 and 112 of the mold 110 are themselves molded by injecting and polymerizing a resin between a mold and a counter-mold, the mold having a shape corresponding to the impressions 1110 and 1120 of the parts 111 and 112 if said fingerprints are identical. In the opposite case, a different mold is used for each part 111 and 112 so as to form in each of them a different imprint. The characteristics of the porous network within the mold, particularly in terms of pore size and porosity level, can be controlled by adjusting the polymerization cycle (s) depending on the nature of the resin used. As a result, there are as many choices of porosity networks as there are porous resins available. By way of non-limiting examples, the following porous resins may be used for producing the porous material mold: - Gil-Resin® T with pores having a size of between 8 and 13 μm, - Gil-Resin® F + with pores having a size of between 4 and 7 μm; - SamaPore with pores having a size of between 3 and 10 μm; - Microplast Fine with pores having an average size of 7 μm. The mold 110, or more precisely the parts 111 and 112 constituting the mold 110, can be made from a rigid porous material such as microporous polytetrafluoroethylene (PTFE) such as "microporous PTFE" products sold by the company Porex® . For example, the PM 0130 material sold by the company Porex® having a pore size of between 1 μm and 2 μm can be used to produce the mold 110. The cavities 1110 and 1120 are each respectively produced by thermoforming or machining the porous material. By way of non-limiting example, the mold 110 can also be made with plaster. The mold made of porous material 110 allows the liquid medium of the slip to be drained outside the fibrous texture 10 and evacuated through the vent 135 due to the application of a pressure gradient between the vent 135 and injection port 134. By way of example, the average pore size (D50) of the mold of porous material may for example be between 1 μm and 10 μm. Figure 3 illustrates the configuration obtained during the injection of a slurry 150 and the drainage of the medium or liquid phase thereof. Before injection of the slip into the tooling, a vacuum was produced in the mold of porous material to then fill the fibrous texture with the slip to the maximum. The vacuum draw can be carried out by pumping at the exhaust vent 135. In FIG. 3, the slurry 150 has been injected under pressure through the injection port 121 and transported to the fibrous texture 10 via the conduit 121 and the channel 1111 so as to penetrate into the fibrous texture 10. The refractory particles 1500 in the slurry 150 are intended to allow the formation of a refractory ceramic matrix in the porosity of the fibrous texture 10. This refractory ceramic matrix may, in an exemplary embodiment, be a refractory oxide matrix. The slip may for example be a suspension of an alumina powder in water. The alumina powder used may be an alpha alumina powder marketed by Baikowski under the name SM8. More generally, the slip may be a suspension comprising refractory ceramic particles having a mean particle size of between 0.1 μm and 10 μm. The volume content of refractory ceramic particles in the slip may, before injection, be between 15% and 40%. The refractory ceramic particles may comprise a material chosen from: alumina, mullite, silica, aluminosilicates, aluminophosphates, carbides, borides, nitrides and mixtures of such materials. Depending on their basic composition, the refractory ceramic particles may, in addition, be mixed with particles of alumina, zirconia, aluminosilicate, a rare earth oxide, rare earth silicate (which may example be used in environmental or thermal barriers) or any other load to functionalize the piece of composite material to obtain as carbon black, graphite or silicon carbide. The medium or liquid phase of the slip may, for example, comprise an aqueous phase having an acidic pH (i.e. a pH below 7) and / or an alcoholic phase comprising for example ethanol. The slip may comprise an acidifier such as nitric acid and the pH of the liquid medium may for example be between 1.5 and 4. The slip may, in addition, comprise an organic binder such as polyvinyl alcohol (PVA which is especially soluble in water. As illustrated in FIG. 3, the refractory ceramic particles 1500 are present after injection of the slip 150 into the porosity of the fibrous texture 10. The arrows 1501 represent the movement of the medium or liquid phase 1501 of the slip drained by the mold made of material porous 110. A pumping P may, in addition, be performed at the outlet vent 135 during drainage, for example by means of a primary vacuum pump. The realization of such pumping improves the drainage and dry more quickly the fibrous texture. In this configuration, the porous material mold 110 makes it possible to retain in the fibrous texture 10 the refractory ceramic particles 1500 initially present in the slip and that all or some of these particles are deposited by filtration in the fibrous texture 10. By using the porous material mold 110, the medium or liquid phase 1501 of the slip can be drained out of the fibrous texture 10 in all directions, with the liquid medium or phase 1501 then flowing in the porous medium 120 until at the vent 135 through which it is discharged from the injection tool 100. This drainage of the liquid medium in all directions makes it possible to promote a deposit by homogeneous and dense sedimentation of the refractory ceramic particles 1500 in the fibrous texture 10 and to obtain, therefore, a high matrix volume ratio in the final piece. In addition, the mold of porous material 110 being held in a rigid material enclosure 130, it can withstand the injection pressures of the slip loaded in the texture and those exerted by the pumping for the evacuation of the liquid medium of the slip. Once the injection and drainage steps have been performed, a fibrous preform 15 is obtained which is filled with refractory ceramic particles, for example particles of refractory ceramic oxide or alumina. The preform obtained is then dried and demolded, the preform can retain after demolding the shape adopted in the mold cavity. The preform is then subjected to a sintering heat treatment, for example in air at a temperature of between 1000 ° C. and 1200 ° C. in order to sinter the refractory ceramic particles and thus form a refractory ceramic matrix in the porosity of the fibrous preform. A piece of composite material is thus obtained, for example a part made of composite Oxide / Oxide material, provided with a fibrous reinforcement formed by the fibrous preform and having a high matrix volume ratio with a homogeneous distribution of the refractory ceramic matrix in all the fibrous reinforcement. A piece of CMC composite material other than Oxide / Oxide can be obtained in the same way by producing the fiber texture with silicon carbide and / or carbon fibers and by using a slurry loaded with carbide particles (for example SiC ), boride (for example TiB2) or nitride (for example Si3N4).
权利要求:
Claims (9) [1" id="c-fr-0001] 1. A method of manufacturing a composite material part comprising the following steps: - formation of a fibrous texture (10) from refractory ceramic fibers, - placement of the fibrous texture (10) in an injection tool ( 110), - pressurized injection of a slurry (150) containing a powder of refractory ceramic particles (1500) in the fibrous texture (10), - drainage of the liquid (1501) of the slurry (150) having passed through the fibrous texture (10) and retention of the powder of refractory ceramic particles within said texture so as to obtain a fiber preform (15) loaded with refractory ceramic particles (1500), - drying of the fiber preform (15), - demolding the fibrous preform (15), and - sintering the refractory ceramic particles present in the fiber preform to form a refractory matrix in said preform, characterized in that the injection tooling comprises a porous material mold (110) having an inner housing (113) in which the fibrous texture (10) is placed, the slip (150) being injected into the fibrous texture (10) by at least one injection port ( 134) present on the injection tooling and opening into the inner housing (113) of the mold of porous material (110), the tooling further comprising a rigid material enclosure (130) in which the mold of porous material ( 110) is maintained during the pressure injection of the slip (150) and the drainage of the liquid (1501) from said slip, the liquid (1501) of the slurry being discharged through at least one vent (135) present on the enclosure made of rigid material. [2" id="c-fr-0002] 2, The method of claim 1, characterized in that the mold of porous material (110) has a size smaller than the internal volume of the rigid material enclosure (130) and in that the volume between the mold of porous material and the enclosure of metallic material is filled by a porous medium (120). [3" id="c-fr-0003] 3. Method according to claim 2, characterized in that the porous medium (120) consists at least of sand or foam. [4" id="c-fr-0004] 4. Method according to any one of claims 1 to 3, characterized in that the void volume present in the porous medium (120) is greater than the volume of the liquid phase (1501) of the slip (150) injected into the fibrous texture (10). [5" id="c-fr-0005] 5. Method according to any one of claims 1 to 4, characterized in that the mold (110) is of a material selected from one of the following materials: porous resin and plaster. [6" id="c-fr-0006] 6. Method according to any one of claims 1 to 5, characterized in that, during the step of forming the fibrous texture (10), the son are woven in a three-dimensional weave or multilayer. [7" id="c-fr-0007] 7. Method according to any one of claims 1 to 6, characterized in that the son of the fibrous texture (10) are formed of fibers consisting of one or more of the following materials: alumina, mullite, silica , an aluminosilicate, a borosilicate, silicon carbide and carbon. [8" id="c-fr-0008] 8. Process according to any one of claims 1 to 7, characterized in that the refractory ceramic particles (1500) are made of a material chosen from: alumina, mullite, silica, an aluminosilicate, an aluminophosphate, zirconia carbide, boride and nitride. [9" id="c-fr-0009] 9. Method according to any one of claims 1 to 8, characterized in that the piece of composite material obtained is a turbomachine blade.
类似技术:
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同族专利:
公开号 | 公开日 BR112018006792A2|2018-10-16| EP3359506B1|2022-02-09| US10954169B2|2021-03-23| CN108779033B|2021-08-24| JP2018537378A|2018-12-20| WO2017060601A8|2017-12-21| EP3359506A1|2018-08-15| RU2018116397A|2019-11-08| US20180297901A1|2018-10-18| RU2018116397A3|2020-03-23| FR3041890B1|2017-11-24| WO2017060601A1|2017-04-13| RU2721674C2|2020-05-21| CN108779033A|2018-11-09| JP6878420B2|2021-05-26| CA3000963A1|2017-04-13|
引用文献:
公开号 | 申请日 | 公开日 | 申请人 | 专利标题 FR2359803A1|1976-07-28|1978-02-24|Porcelaine Cie Nle|Porcelain or ceramic mouldings prodn. - by pressure injection of aq. barbotine into porous plaster moulds through which the water flows| FR2702475A1|1993-03-08|1994-09-16|Agency Ind Science Techn|Process for the manufacture of ceramics reinforced with fibres arranged in three dimensions, and apparatus for implementing this process| US5436042A|1994-03-11|1995-07-25|The Carborundum Company|Ceramic fiber-reinforced composite articles and their production| WO2010049961A1|2008-10-31|2010-05-06|Universita' Del Salento|Method for the production of components made of ceramic-matrix composite material| EP2357070A1|2010-02-12|2011-08-17|Fraunhofer-Gesellschaft zur Förderung der Angewandten Forschung e.V.|Injection moulding method for condensation resins and device for the method|FR3071257A1|2017-09-19|2019-03-22|Safran Ceramics|METHOD FOR INJECTING A SUSPENSION LOADED IN A FIBROUS TEXTURE AND METHOD FOR MANUFACTURING A PIECE OF COMPOSITE MATERIAL| WO2020234550A1|2019-05-23|2020-11-26|Safran|Method for producing a part from composite material by injecting a loaded slip into a fibrous texture|CA2268019C|1997-08-11|2007-03-13|Volvo Aero Corporation|A method for manufacturing a ceramic composite material| GB9827889D0|1998-12-18|2000-03-29|Rolls Royce Plc|A method of manufacturing a ceramic matrix composite| JP4850352B2|2001-06-06|2012-01-11|イビデン株式会社|Large graphite material and manufacturing method thereof| CA2434447A1|2003-06-27|2004-12-27|Eduardo Ruiz|Manufacture of composites through a flexible injection process using a double-cavity or multi-cavity mold| WO2010057502A2|2008-11-24|2010-05-27|Vestas Wind Systems A/S|Wind turbine blade comprising particle-reinforced bonding material| CN101880172B|2010-06-13|2013-01-16|东华大学|Preparation method for three-dimensional woven fiber reinforced ceramic matrix composite| RU2516628C1|2012-12-28|2014-05-20|Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Московский государственный технический университет имени Н.Э. Баумана" |Method for manufacturing parts from composite materials| FR3014008B1|2013-12-04|2016-10-28|Snecma|METHOD FOR IMPREGNATING A FIBROUS PREFORM AND DEVICE FOR IMPLEMENTING SAID METHOD| FR3030505B1|2014-12-23|2019-07-12|Safran|PROCESS FOR PRODUCING A FIBROUS PREFORM CHARGED WITH REFRACTORY CERAMIC PARTICLES|FR3051187B1|2016-05-11|2018-06-01|Safran Ceramics|PIECE OF COMPOSITE MATERIAL| FR3071245B1|2017-09-21|2019-09-20|Safran Ceramics|METHOD FOR INJECTING A BARBOTIN CHARGED WITH FIBROUS TEXTURE| FR3071765B1|2017-10-03|2020-11-20|Safran Ceram|COMPOSITE MATERIAL REALIZATION OF A FLOW MIXER LOBE STRUCTURE| US11122935B2|2018-05-29|2021-09-21|Chun-Shyong LEE|Ceramic deep-frying device capable of withstanding high temperatures and releasing far-infrared energy and method for making the same| US10780498B2|2018-08-22|2020-09-22|General Electric Company|Porous tools and methods of making the same| FR3087194B1|2018-10-12|2021-02-26|Safran Aircraft Engines|PROCESS FOR MANUFACTURING A PART IN COMPOSITE MATERIAL WITH CHECK OF CONFORMITY| FR3098434A1|2019-07-11|2021-01-15|Safran Aircraft Engines|Tooling for the injection of a loaded slip| WO2021005282A2|2019-07-11|2021-01-14|Safran Aircraft Engines|Method for producing a part from composite material by injecting a filled slip into a fibrous texture| FR3098433A1|2019-07-11|2021-01-15|Safran Aircraft Engines|Manufacturing process of a composite material part by injection of a slip loaded in a fibrous texture| CN111039687A|2019-12-13|2020-04-21|中国航空制造技术研究院|Damage-free hole making method for continuous fiber reinforced ceramic matrix composite| CN112140282B|2020-09-28|2022-02-15|中航装甲科技有限公司|Method for improving fluidity of silicon-based ceramic core slurry|
法律状态:
2016-10-05| PLFP| Fee payment|Year of fee payment: 2 | 2017-04-07| PLSC| Publication of the preliminary search report|Effective date: 20170407 | 2017-09-21| PLFP| Fee payment|Year of fee payment: 3 | 2018-08-17| CD| Change of name or company name|Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20180717 Owner name: SAFRAN, FR Effective date: 20180717 | 2018-09-19| PLFP| Fee payment|Year of fee payment: 4 | 2019-09-19| PLFP| Fee payment|Year of fee payment: 5 | 2020-09-17| PLFP| Fee payment|Year of fee payment: 6 | 2021-09-22| PLFP| Fee payment|Year of fee payment: 7 |
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申请号 | 申请日 | 专利标题 FR1559430A|FR3041890B1|2015-10-05|2015-10-05|PROCESS FOR MANUFACTURING A COMPOSITE MATERIAL PART BY INJECTING A BARBOTIN CHARGED IN A POROUS MOLD|FR1559430A| FR3041890B1|2015-10-05|2015-10-05|PROCESS FOR MANUFACTURING A COMPOSITE MATERIAL PART BY INJECTING A BARBOTIN CHARGED IN A POROUS MOLD| RU2018116397A| RU2721674C2|2015-10-05|2016-10-04|Method of producing part from composite ceramic material by pressure injection of a filled suspension into a porous mold| JP2018517597A| JP6878420B2|2015-10-05|2016-10-04|A method for producing ceramic composite parts by pressure injection of charged slurry into a porous mold.| PCT/FR2016/052535| WO2017060601A1|2015-10-05|2016-10-04|Process for manufacturing a ceramic composite material part by pressurized injection of a loaded slurry into a porous mould| US15/766,206| US10954169B2|2015-10-05|2016-10-04|Process for manufacturing a ceramic composite material part by pressurized injection of a loaded slurry into a porous mould| EP16790654.4A| EP3359506B1|2015-10-05|2016-10-04|Process for the manufacturing of a ceramic composite part by injection of a loaded slurry in a porous mould| BR112018006792-0A| BR112018006792A2|2015-10-05|2016-10-04|method for manufacturing a piece of composite material.| CA3000963A| CA3000963A1|2015-10-05|2016-10-04|Process for manufacturing a composite material part by injection of a loaded slurry into a porous mould| CN201680070989.0A| CN108779033B|2015-10-05|2016-10-04|Method for producing a ceramic composite component by pressure injection of a loading slurry into a porous mould| 相关专利
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