• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    A method of manufacturing a composite material part comprises placing a fibrous texture (10) in a mold (110) having in its lower part a piece of porous material (130) on which a first face (10b) rests of the texture (10), the injection under pressure of a liquid (150) containing a powder of refractory ceramic particles in the fibrous texture (10), and the drainage by the porous material part (120) of the liquid having passed through the fibrous texture (10) and retention of the refractory ceramic particle powder within said texture by said porous material piece (130). A perforated rigid element (140) is interposed between the bottom (111) of the mold (110) and the piece of porous material (130).
    公开号:FR3050454A1
    申请号:FR1653635
    申请日:2016-04-25
    公开日:2017-10-27
    发明作者:Michael Podgorski；Bruno Jacques Gerard Dambrine；Edu Ruiz
    申请人:Safran SA；
    IPC主号:
    专利说明:

    Background of the invention
    The present invention relates to a method for manufacturing a part made of thermostructural composite material, in particular of the oxide / oxide or ceramic matrix (CMC) type, that is to say having a fibrous reinforcement formed from fibers made of refractory ceramic material. densified by a matrix also made of refractory ceramic material.
    Parts made of composite Oxide / Oxide material 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 a sintering or a ceramic heat treatment in order to form a refractory oxide matrix in the preform and obtain a piece of composite material Oxide / Oxide. 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 TiB2) or nitride particles. (eg S13N4).
    However, this type of production method makes it possible to produce only composite parts Oxide / Oxide or CMC having limited mechanical characteristics 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, especially of the Oxide / Oxide or CMC type, from a thick fibrous texture and / or complex geometry, and this in a fast and reliable way 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 without macroporosity. 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 a mold comprising in its lower part a piece of porous material on which a first face of said texture rests, - closure of the mold with a counter-mold or a cover placed opposite a second face of the fibrous texture, - injection under pressure of a liquid containing a powder of refractory ceramic particles or particles of a refractory ceramic precursor in the fibrous texture, - drainage through the porous material part of the liquid having passed through the fibrous texture and retention of the powder of refractory ceramic particles or particles of a refractory ceramic precursor within said texture by said piece of porous mani material to obtain a fiber preform loaded with refractory ceramic particles or particles of a refractory ceramic precursor, the liquid being discharged through at least one vent present on the bottom of the mold, a perforated rigid element being interposed between the bottom of the mold and the piece of porous material, - drying of the fibrous preform, - demolding of the fibrous preform, and - heat treatment of the refractory ceramic particles or particles of a refractory ceramic precursor present in the fibrous preform to form a refractory ceramic matrix in said preform.
    By using a piece of porous material for draining the liquid from the slip, the method of the invention makes it possible to eliminate the liquid introduced into the fibrous texture without removing the refractory ceramic solid particles or the particles of a precursor of refractory ceramic. also present in the texture. Furthermore, by interposing a rigid perforated element between the bottom of the mold and the piece of porous material, it is possible to have a balanced pressure on the underside of the porous material part, the face through which the liquid is discharged. Thanks to the presence of a rigid perforated element between the bottom of the mold and the piece of porous material, the liquid can circulate between the piece of porous material and the bottom of the mold and easily reach the exhaust or evacuation vents regardless its point of exit at the porous material part.
    With the method of the invention, the elimination of the liquid by drainage does not disturb the distribution of the particles within the fibrous texture and therefore makes it possible to obtain a piece of composite material with a homogeneous distribution of the matrix in all the fibrous reinforcement. The piece of thermostructural composite material has, therefore, improved mechanical properties.
    According to a first particular aspect of the method of the invention, the perforated rigid element comprises a plurality of openings, each aperture having a parallelepipedal shape whose sides extend over a distance of less than or equal to 5 mm or a circular shape having a diameter less than or equal to 5 mm.
    According to a second particular aspect of the method of the invention, the perforated rigid element has a thickness of about 1 mm.
    According to a third particular aspect of the method of the invention, the perforated rigid element comprises notches or cuts on its lower face in contact with the inner surface of the bottom of the mold.
    According to a fourth particular aspect of the process of the invention, the perforated rigid element is made of a material chosen from one of the following materials: polytetrafluoroethylene (PTFE), metallic material, polymer, etc.
    According to one embodiment of the method of the invention, the mold in which the fiber texture is placed comprises an impregnation chamber comprising in its lower part the piece of porous material on which a first face of the texture rests, the impregnation chamber being closed in its upper part by a deformable impermeable membrane placed opposite a second face of the fibrous texture, said membrane separating the impregnation chamber from a compaction chamber, the liquid containing the refractory ceramic particles or the particles of a refractory ceramic precursor being injected into the impregnation chamber between the second face of the fibrous texture and the membrane, a compaction fluid being injected into the compaction chamber, the fluid exerting a pressure on the membrane to force the loaded liquid through the fibrous texture. 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 be a turbine engine blade or a rear body part, a combustion chamber, a flap, a post-combustion arm, etc.
    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 diagrammatic exploded perspective view of a tool according to an embodiment of the invention; FIG. 2 is a diagrammatic sectional view showing the tool of FIG. 1 closed with a fibrous texture positioned in this tool; FIG. 3 is a diagrammatic sectional view showing the steps of impregnating a fibrous texture with a slip loaded in the tool of FIG. 2; FIG. 4 is a diagrammatic sectional view of an tooling according to another embodiment of the invention, - Figure 5 is a schematic sectional view showing the tool of Figure 4 closed with a fibrous texture positioned in cel Figures 6 and 7 are diagrammatic sectional views showing the steps of impregnating a fibrous texture with a slip loaded in the tool of Figure 5.
    Detailed description of embodiments
    The method of manufacturing a piece of composite material, in particular 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 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 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 a tool according to the invention which makes it possible, as explained hereinafter, to deposit refractory ceramic particles or particles of a refractory ceramic precursor within the texture. fibrous. For this purpose and as illustrated in FIGS. 1 and 2, a fibrous texture 10 is placed in a tool 100. In the example described here, the fibrous texture 10 is produced according to one of the techniques defined above (stacking 2D or 3D weave) with Nextel 610 ™ alumina threads. The fibrous texture 10 is here intended to form the fibrous reinforcement of a blade made of composite material Oxide / Oxide. The tooling 100 comprises a mold 110 and a counter mold 120. The mold 110 comprises a bottom 111 provided with a vent 112. The mold 110 also comprises a side wall 113 which forms with the bottom 111 a molding cavity 114. In the example illustrated, the tool 100 in which the fibrous texture 10 is present is closed in its lower part by the mold 110 and is closed in its upper part by the counter-mold 120 forming a cover closing the tool 100. The mold 110 and the counter-mold 120 serve to size the preform and thus the part to be obtained and to adjust the fiber content in the part to be obtained.
    The counter-mold 120 has a plurality of injection ports 121 through which a liquid charged with refractory ceramic particles or particles of a refractory ceramic precursor is intended to be injected to penetrate the porosity of the fibrous texture. through the first face 10a of the fibrous texture 1. In the example illustrated in FIGS. 1 and 2, the charged liquid is intended to be injected through a plurality of injection ports 121 opening into different zones of the molding cavity. However, it is not beyond the scope of the invention when the liquid is injected through a single injection pore.
    The mold 110 comprises, meanwhile, a single vent 112 of the liquid. Of course, it is not beyond the scope of the invention when a plurality of output vents is implemented.
    A piece of porous material 130 is present in the molding cavity 114 between the mold 110 and the fibrous texture 10. The piece of porous material 130 has an upper face 130a in contact with the second face 10b of the fibrous texture 10 through which drainage of the liquid is intended to be realized. The second face 10b of the fibrous texture 10 is, in the example illustrated in FIGS. 1 and 2, located on the opposite side to the first face 10a through which the slip is intended to penetrate the texture 1. The liquid loaded with Refractory ceramic particles can also be injected on the sides of the preform.
    The piece of porous material 130 may for example be made of 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 for producing the piece of porous material 130.
    The porous material part 130 allows the drainage of the liquid outside the fibrous texture 10 and its evacuation through the outlet vent 112 due to the application of a pressure gradient between the outlet vent 112 and injection ports 121. By way of example, the piece of porous material 130 may have a thickness greater than or equal to 1 mm, or even several millimeters. The average porosity rate of the porous material part 130 can be about 30%. The average pore size (D50) of the porous material part may for example be between 1 μm and 2 μm.
    In an exemplary embodiment, the piece of porous material 130 may be rigid and have a shape corresponding to the shape of the preform and the piece of composite material to obtain. In this case, the piece of porous material may for example be made by thermoforming. Alternatively, the piece of porous material may be deformable and may take the form of the mold which corresponds to the shape of the preform and the composite material part to obtain.
    According to the invention, a perforated rigid element 140 is interposed between the bottom 111 of the mold 110 and the piece of porous material 130. More specifically, the perforated rigid element 140 has an upper face 140a in contact with the lower face 130b of the piece of porous material 130 and a lower face 140b in contact with the inner surface 111a of the bottom 111 of the mold 110.
    In the example described here, the perforated rigid element 140 has a grid shape formed by the perpendicular crossing between walls 142 with walls 143, the walls 142 and 143 delimiting between them openings 141 of parallelepiped shape. The openings 141 preferably have a side length less than or equal to 5 mm in order to avoid local deformation of the piece of porous material 130. The perforated rigid element 140 may have, for example, an Emo thickness less than or equal to 1 mm. . The perforated rigid element is made of a material that is chemically and / or mechanically compatible with both the liquid injected into the fibrous texture and the piece of porous material. In the example described here, the perforated rigid element 140 is made of polytetrafluoroethylene (PTFE) as the piece of porous material 130.
    According to a feature of the present invention, the lower face 140b of the rigid element 140 in contact with the inner surface 111a of the bottom 111 of the mold 110 has at the walls 142 and 143 notches or cutouts 1420 and 1430 to facilitate the flow of liquid to the outlet vent 112.
    Before the injection of a slip into the fibrous texture 10, a compaction pressure for compacting the fibrous texture between the mold 110 and the counter mold 120 can be applied by clamping the mold or by means of a press, this compaction pressure can be maintained during the injection.
    Alternatively, the compaction pressure can be applied after the start of the injection of the charged liquid and can then be maintained. The application of a compaction pressure may allow the texture to be compacted to assist in the drainage of the liquid and to achieve a target thickness for the fibrous preform without damaging it.
    In the example described here, the charged liquid corresponds to a slip containing refractory ceramic particles. FIG. 3 illustrates the configuration obtained during the injection of a slurry 150 and the drainage of the liquid medium therefrom. The slurry 150 was injected under pressure through the injection ports 121 so as to penetrate the fibrous texture 10 through its first face 10a. The refractory ceramic particles 1500 present 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 one exemplary embodiment, be a refractory oxide matrix. .
    The slip may for example be a suspension of an alumina powder in water. The average particle size (D50) of the alumina powder may be from 0.1 μm to 0.3 μm. 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 20% and 40%. The refractory ceramic particles may comprise a material chosen from: alumina, mullite, silica, an aluminosilicate, an aluminophosphate, zirconia, a carbide, a boride and a nitride. 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 liquid medium 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 151 represent the movement of the slip 150 injected into the fibrous texture 10. The arrows 152 represent as for them the movement of the medium or liquid phase of the slip sucked by the piece of porous material 130.
    Counter mold 120 exerts pressure on the fibrous texture during and after the injection step.
    Pumping P can also be performed at the outlet vent 112 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.
    Alternatively or in combination, it is possible during the drainage to heat the liquid medium still present in the porosity of the fibrous texture in order to evaporate the latter through the second face of the fibrous texture and the piece of porous material. For example, the temperature of the liquid medium can be raised to a temperature between 80 ° C and 105 ° C.
    In this configuration, the piece of porous material 130 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.
    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, for example alumina.
    The preform obtained is then dried and demolded, the preform can retain after demolding the shape adopted in the molding cavity, for example its shape adopted after compaction between the mold and against the mold through the presence of a binder in the slip such as PVA.
    The preform is then subjected to a heat treatment, here sintering, for example in air at a temperature between 1000 ° C and 1200 ° C to sinter the refractory ceramic particles and thus form a refractory ceramic matrix in the porosity of the preform fibrous. 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).
    The filled liquid injected into the preform may, in a variant, comprise particles of a refractory ceramic precursor, for example of the sol-gel or polymeric type. In this case, the heat treatment comprises at least one step of converting the refractory ceramic precursor into a ceramic material (so-called ceramization step) optionally followed by an additional sintering step in order to further densify the composite material part.
    Figures 4 to 7 illustrate a method of manufacturing a composite material part according to another embodiment of the invention. As illustrated in FIGS. 4 and 5, a fibrous texture 20 is placed in a tool 200. In the example described here, the fibrous texture 20 is produced according to one of the techniques defined above (stacking 2D strata or 3D weaving) with Nextel 610 ™ alumina wires. The fibrous texture 20 is here intended to form the fibrous reinforcement of a blade made of composite material Oxide / Oxide. The tool 200 comprises a mold 210 whose bottom 211 is provided with a vent 212. The mold 210 also comprises a side wall 213 having an injection port 215 equipped with a valve 2150. A piece of porous material 230 is placed below the fibrous texture 20, the piece of porous material 120 having an upper face 230a for receiving the fibrous texture 20. In the example described here, the part 230 is made of a deformable material so as to conform to a shape or a profile corresponding to the shape of the final piece to be manufactured defined by the mold 210, here an aeronautical engine blade. By conforming, the piece 230 has on its upper face 230a a shape similar to that of the part to be manufactured. The piece 120 may for example be made of microporous polytetrafluoroethylene (PTFE) such as "microporous PTFE" products sold by the company Porex®. According to an alternative embodiment, the piece of porous material is rigid and has on its upper surface a geometry corresponding to the shape of the final piece to be manufactured. In this case, the part may in particular be made by thermoforming. For example, the piece of porous material may have a thickness of several millimeters and an average porosity of about 30%. The average pore size (D50) of the porous material part may for example be between 1 μm and 2 μm.
    According to the invention, a perforated rigid element 240 is interposed between the bottom 211 of the mold 210 and the piece of porous material 230. More specifically, the perforated rigid element 240 has an upper face 240a in contact with the lower face 230b of the piece of porous material 230 and a lower face 240b in contact with the inner surface 211a of the bottom 211 of the mold 210.
    In the example described here, the perforated rigid element 240 has, like the perforated rigid element 140 shown in FIG. 1, a grid shape formed by the perpendicular crossing between walls 242 with walls 243, walls 242 and 243 delimiting between them openings of parallelepiped shape. The openings preferably have a side length less than or equal to 5 mm to prevent local deformation of the porous material part 230. The perforated rigid element 240 may have for example a thickness E240 less than or equal to 1 mm. The perforated rigid element 240 is further shaped according to a curvature corresponding to that presented by the surface 211a of the 211 of the mold 210. The perforated rigid element is made of a material that is chemically and / or mechanically compatible with both the loaded liquid. injected into the fibrous texture and the piece of porous material. In the example described here, the perforated rigid element 240 is made of polytetrafluoroethylene (PTFE) as the piece of porous material 230.
    According to a feature of the present invention, the lower face 240b of the rigid element 240 in contact with the inner surface 211a of the bottom 211 of the mold 210 has at its walls 243 notches or cutouts 2430 to facilitate the circulation of the liquid phase to the outlet vent 212. The walls 242 also have notches or cuts (not shown in Figures 4 to 7). The tool 200 further comprises a cover 220 comprising an injection port 221 equipped with a valve 2210 and a deformable membrane 280 which, once the tool has been closed (FIG. 5), separates an impregnation chamber 201 in which The fibrous texture 20 of a compaction chamber 202 above the membrane 280 is present. The membrane 280 can be made for example of silicone.
    After placing the texture 20 on the upper face 230a of the piece of porous material 230, the mold 210 is closed with the lid 230 (Figure 5). A charged liquid, here a slurry 250, is then injected into the impregnation chamber 201 via the injection port 215 whose valve 2150 is open (FIG. 6). The slurry 250 is, in this example, intended to allow the formation of a refractory oxide matrix in the texture. Slurry 250 corresponds to a suspension containing a powder of refractory oxide particles, the particles having an average particle size of between 0.1 μm and 10 μm. The liquid phase of the slurry may in particular consist of water (acidic pH), ethanol or any other liquid in which it is possible to suspend the desired powder. An organic binder can also be added (PVA for example, soluble in water). This binder ensures the holding of the raw material after drying and before sintering.
    The slurry 250 may for example correspond to an aqueous suspension consisting of alumina powder whose mean particle size (D50) is between 0.1 μm and 0.3 μm and whose volume fraction is between 20% and 40%. the suspension being acidified with nitric acid (pH between 1.5 and 4). In addition to alumina, the refractory oxide particles may also be made of a material chosen from alumina, mullite, silica, an aluminosilicate, an aluminophosphate, zirconia, a carbide, a boride and a nitride. Depending on their base composition, the refractory oxide particles may be further mixed with particles of alumina, zirconia, aluminosilicate, rare earth oxides, rare earth dissilicates (used for example in environmental or thermal barriers) or any other load that makes it possible to add specific functions to the final material (carbon black, graphite, silicon carbide, etc.).
    The amount of slurry 250 injected into the impregnation chamber 201 is determined as a function of the volume of the fibrous texture to be impregnated. It is the quantity of powder initially introduced which will control the thickness of setting and thus the volume ratio of fibers (Tvf) and matrix (Tvm).
    Once the slip has been injected into the impregnation chamber 201, the compaction operation is carried out by injecting a compaction fluid 260, for example oil, into the compaction chamber 202 through the injection port 221 of which the valve 2210 is open, the valve 2150 of the injection port 215 having been previously closed (Figure 7). The compression fluid 260 applies a pressure on the slip 250 through the membrane 280 which forces the slip 250 to penetrate into the fibrous texture 20. The fluid 260 imposes a pressure on the entire membrane 280 and, therefore, on the entirety of the slip present above the texture 20. The pressure applied by the membrane 280 on the slip and on the fibrous texture is preferably less than 15 bar, for example 7 bar, so as to penetrate the slip in the texture and sufficiently compact the texture to allow the liquid phase of the slip to be drained by the piece of porous material without degrading the resulting preform.
    The piece of porous material 230 which is located on the side of the face 20b of the fibrous texture opposite the face 20a from which the slip penetrates into the texture performs several functions. In fact, the part 230 allows the liquid of the slip to be drained outside the fibrous texture, the liquid thus drained being evacuated here by the vent 212. The drainage is carried out both during and after the compaction. When there is no more liquid flowing through the vent 212, drainage is complete. In combination with the application of pressure on the slip by the compression fluid, a pumping P, for example by means of a primary vacuum pump (not shown in Figures 4 to 7), can be achieved at of the vent 212. This pumping is optional. Heating can suffice. Conversely, pumping without heating may suffice. However, the combination of both speeds up drying.
    In addition, the tool may be provided with heating means, such as resistive elements integrated into the walls of the tool, in order to increase the temperature in the compaction chamber and facilitate evacuation of the liquid from the slip by evaporation. The temperature in the compaction chamber can be raised to a temperature between 80 ° C and 105 ° C.
    The piece of porous material 220 retains the solid particles of refractory oxide present in the slip, the refractory oxide particles thus gradually deposited in the fibrous texture. This makes it possible to obtain later (i.e. after sintering) the matrix.
    The part 220 also makes it possible to maintain the fibrous texture in shape during the compaction operation because it resumes on its upper face 220a the shape of the bottom 211 of the mold 210 corresponding to the shape of the final piece to be manufactured.
    A fibrous preform 30 filled with refractory oxide particles is then obtained, here particles of alumina of the type described above. The preform is then demolded by emptying the compression fluid of the compaction chamber 202, the preform retaining after demolding its compaction geometry through the presence of a binder in the slip such as PVA.
    The preform is then extracted from the tooling and subjected to an air sinter heat treatment at a temperature of between 1000 ° C. and 1200 ° C. in order to sinter the refractory oxide particles together and thus form a refractory oxide matrix in the preform. This gives a piece of composite material Oxide / Oxide provided with a fiber reinforcement obtained by 3D weaving with a homogeneous distribution of the matrix throughout the fibrous reinforcement.
    A piece of CMC composite material can be obtained in the same way by producing the fibrous texture with silicon carbide or carbon fibers and using a slurry loaded with carbide carbide particles (eg SiC), boride (ex. TiB2) or nitride (eg SI3N4).
    The filled liquid injected into the preform may, in a variant, comprise particles of a refractory ceramic precursor, for example of the sol-gel or polymeric type. In this case, the heat treatment comprises at least one step of converting the refractory ceramic precursor into a ceramic material (so-called ceramization step) optionally followed by an additional sintering step in order to further densify the composite material part. The rigid perforated element according to the invention can have various shapes. It may in particular have a grid shape with parallelepiped openings as described above, a plate shape comprising a plurality of circular perforations forming the openings, or a form of alveolar Nida® type whose cells constitute the openings.
    As indicated above, the perforated rigid element is preferably made of a material which is chemically and / or mechanically compatible with both the slip injected into the fibrous texture and the piece of porous material. The perforated rigid element may in particular be made with one of the following materials: polytetrafluoroethylene (PTFE), metal material, polymer.
    权利要求:
    Claims (10)
    [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 a mold (110) comprising in its lower part a piece of porous material (130) on which rests a first face (10b) of said texture (10), - closure of the mold with a counter-mold or a cover (120) placed next to a second face (10a) of the fibrous texture (10), - injection under pressure of a liquid (150) containing a powder of refractory ceramic particles or particles of a refractory ceramic precursor in the fibrous texture (10), - drainage by the porous material part (120) of the liquid having passed through the fibrous texture (10) and retention of the powder of refractory ceramic particles or particles of a refractory ceramic precursor inside said texture by the piece of porous material (130) so as to obtain a fibrous preform (15) loaded with refractory ceramic particles or particles of a refractory ceramic precursor, the liquid being discharged through at least one vent present on the bottom of the mold, drying the fiber preform (15), demolding the fiber preform (15), and heat-treating the refractory ceramic particles or particles of a refractory ceramic precursor present in the fiber preform to form a refractory ceramic matrix. in said preform, characterized in that a perforated rigid element (140) is interposed between the bottom (111) of the mold (110) and the piece of porous material (130).
    [2" id="c-fr-0002]
    2. Method according to claim 1, characterized in that the perforated rigid element (140) comprises a plurality of openings (141), each aperture having a parallelepiped shape whose sides extend over a distance less than or equal to 5 mm or a circular shape having a diameter less than or equal to 5 mm.
    [3" id="c-fr-0003]
    3. Method according to claim 2, characterized in that the perforated rigid element (140) has a thickness (Ewo) of about 1 mm.
    [4" id="c-fr-0004]
    4. Method according to any one of claims 1 to 3, characterized in that the perforated rigid element (140) has notches or cuts (1420, 1430) on its lower face (140b) in contact with the inner surface ( 111a) of the bottom (111) of the mold (110).
    [5" id="c-fr-0005]
    5. Method according to any one of claims 1 to 4, characterized in that the perforated rigid element (140) is a material selected from one of the following materials: polytetrafluoroethylene (PTFE), metal material, polymer.
    [6" id="c-fr-0006]
    6. Method according to any one of claims 1 to 5, characterized in that the mold (210) in which is placed the fibrous texture comprises an impregnation chamber (201) having in its lower part the piece of porous material ( 230) on which a first face (20b) of said texture (20) rests, the impregnation chamber (201) being closed in its upper part by a deformable impermeable membrane (280) placed opposite a second face (20a). ) of the fibrous texture (20), said membrane (280) separating the impregnation chamber (201) from a compaction chamber (202), the liquid (250) containing the powder of refractory ceramic particles or particles of a refractory ceramic precursor being injected into the impregnation chamber between the second face (20a) of the fibrous texture (20) and the membrane (280), a compaction fluid (260) being injected into the compaction chamber (202) ), the fluid exerting a pressing the membrane (280) to force the liquid (250) containing the refractory ceramic particle powder or particles of a refractory ceramic precursor (250) to pass through the fibrous texture (20).
    [7" id="c-fr-0007]
    7. Method according to any one of claims 1 to 6, characterized in that, during the step of forming the fibrous texture, the son are woven in a three-dimensional weave or multilayer.
    [8" id="c-fr-0008]
    8. Method according to any one of claims 1 to 7, characterized in that the son of the preform are formed of fibers consisting of one or more of the following materials: alumina, mullite, silica, an aluminosilicate, borosilicate, silicon carbide and carbon.
    [9" id="c-fr-0009]
    9. Process according to any one of claims 1 to 8, characterized in that the refractory ceramic particles are of a material chosen from: alumina, mullite, silica, an aluminosilicate, an aluminophosphate, zirconia, a carbide , a boride and a nitride.
    [10" id="c-fr-0010]
    10. Method according to any one of claims 1 to 9, characterized in that the composite material part obtained is a turbomachine blade, a rear body part, a combustion chamber, a shutter or a post-combustion arm.
    类似技术:
    公开号 | 公开日 | 专利标题
    EP3237660B1|2018-12-05|Process for the manufacturing of a fibrous preform loaded with ceramic refractory particles
    FR3050454B1|2019-07-12|PROCESS FOR MANUFACTURING A COMPOSITE MATERIAL PART BY INJECTING A BARBOTIN CHARGED WITH FIBROUS TEXTURE
    EP3359506B1|2022-02-09|Process for the manufacturing of a ceramic composite part by injection of a loaded slurry in a porous mould
    EP3237358B1|2018-09-19|Process for manufacturing a refractory composite body
    EP3237359B1|2019-05-22|Method for manufacturing a part made of a composite material
    EP3684575B1|2021-08-18|Process for injecting a loaded slurry into a fibrous texture
    EP3768405A1|2021-01-27|Method for the production of a part made from a composite material, by means of the injection of powder into a fibrous reinforcement with drainage through a composite filtration layer
    EP3774690A1|2021-02-17|Method for producing a part made from a composite material by means of the injection of a laden ceramic slurry into a fibrous structure
    WO2018234669A1|2018-12-27|Process for manufacturing a composite material part having one or more local thickness variations
    WO2021005282A2|2021-01-14|Method for producing a part from composite material by injecting a filled slip into a fibrous texture
    EP3863992A1|2021-08-18|Method for manufacturing a part made of composite material with compliance control
    WO2020234550A1|2020-11-26|Method for producing a part from composite material by injecting a loaded slip into a fibrous texture
    FR3098433A1|2021-01-15|Manufacturing process of a composite material part by injection of a slip loaded in a fibrous texture
    FR3098434A1|2021-01-15|Tooling for the injection of a loaded slip
    CA2971332A1|2018-12-19|Fabrication process for a composite material part by injection and polymerization of a resin in a fibrous texture
    同族专利:
    公开号 | 公开日
    EP3448829B1|2020-08-19|
    CA3022103A1|2017-11-02|
    RU2018141255A|2020-05-26|
    US20190134848A1|2019-05-09|
    RU2728306C2|2020-07-29|
    CN109195930A|2019-01-11|
    BR112018071896A2|2019-02-05|
    RU2018141255A3|2020-06-03|
    EP3448829A1|2019-03-06|
    FR3050454B1|2019-07-12|
    WO2017187050A1|2017-11-02|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US4814127A|1986-03-31|1989-03-21|Aisin Seiki Kabushiki Kaisha|Method of producing a reinforced ceramic|
    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|
    US20120217670A1|2003-06-27|2012-08-30|Polyvalor, Limited Partnership|Manufacture of Composites by a Flexible Injection Process Using a Double or Multiple Cavity Mold|
    FR2958933A1|2010-04-20|2011-10-21|Onera |PROCESS FOR PRODUCING A CERAMIC MATRIX COMPOSITE PIECE|
    EP2481558A1|2011-01-31|2012-08-01|Eurocopter Deutschland GmbH|Device and method for manufacturing of preimpregnated preform and multi-layer preimpregnated preform resulting from said method|WO2020128364A1|2018-12-21|2020-06-25|Safran Ceramics|Tool and method for manufacturing a composite-material part by means of a liquid process|US5143604A|1990-05-22|1992-09-01|Filtercorp, Inc.|One-way guided filter pad assembly|
    US20050230863A1|2003-11-12|2005-10-20|Mike Scott|Vacuum molding of fibrous structures|
    SE529164C2|2004-11-26|2007-05-22|Pakit Int Trading Co Inc|Pulp form and use of pulp form|
    DE102006058198C5|2006-12-07|2018-01-18|Fibretemp Gmbh & Co. Kg|Electrically heated mold in plastic construction|
    IT1394969B1|2009-07-30|2012-08-07|Sacmi|METHOD FOR THE REALIZATION OF A MANUFACTURED MATERIAL IN CERAMIC MATERIAL AND IMPLANTATION OF THIS METHOD.|
    FR2961740B1|2010-06-25|2014-03-07|Snecma|METHOD FOR MANUFACTURING AN ARTICLE IN COMPOSITE MATERIAL|
    US8387504B2|2011-01-06|2013-03-05|General Electric Company|Fiber-reinforced Al-Li compressor airfoil and method of fabricating|
    CN103469121B|2013-08-27|2015-10-28|西北工业大学|The apparatus and method of preparation aluminium oxide short staple preform|FR3076242B1|2017-12-28|2020-01-10|Safran Ceramics|METHOD FOR MANUFACTURING A PART OF COMPOSITE MATERIAL BY INJECTING POWDER IN A FIBROUS REINFORCEMENT WITH DRAINAGE BY COMPOSITE FILTRATION STRATE|
    FR3080113B1|2018-04-13|2020-05-01|Safran Ceramics|PROCESS FOR THE MANUFACTURE OF A PART OF COMPOSITE MATERIAL BY INJECTION OF A BARBOTINE LOADED IN A FIBROUS TEXTURE|
    FR3087194B1|2018-10-12|2021-02-26|Safran Aircraft Engines|PROCESS FOR MANUFACTURING A PART IN COMPOSITE MATERIAL WITH CHECK OF CONFORMITY|
    CN109808201B|2019-01-22|2020-08-18|西安交通大学|Preparation and forming method of nano gradient fiber reinforced wear-resistant composite material|
    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|
    DE102019126607A1|2019-10-02|2021-04-08|Technische Universität Dresden|Device and method for connecting textile-reinforced structural modules, device and method for producing textile reinforcement or a textile-reinforced structural module, concrete component and printer description file|
    法律状态:
    2017-04-13| PLFP| Fee payment|Year of fee payment: 2 |
    2017-10-27| PLSC| Publication of the preliminary search report|Effective date: 20171027 |
    2018-03-22| PLFP| Fee payment|Year of fee payment: 3 |
    2020-03-19| PLFP| Fee payment|Year of fee payment: 5 |
    2021-03-23| PLFP| Fee payment|Year of fee payment: 6 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1653635|2016-04-25|
    FR1653635A|FR3050454B1|2016-04-25|2016-04-25|PROCESS FOR MANUFACTURING A COMPOSITE MATERIAL PART BY INJECTING A BARBOTIN CHARGED WITH FIBROUS TEXTURE|FR1653635A| FR3050454B1|2016-04-25|2016-04-25|PROCESS FOR MANUFACTURING A COMPOSITE MATERIAL PART BY INJECTING A BARBOTIN CHARGED WITH FIBROUS TEXTURE|
    CA3022103A| CA3022103A1|2016-04-25|2017-04-19|Method for producing a part from composite material by injecting a loaded slip into a fibrous texture|
    PCT/FR2017/050931| WO2017187050A1|2016-04-25|2017-04-19|Method for producing a part from composite material by injecting a loaded slip into a fibrous texture|
    EP17722117.3A| EP3448829B1|2016-04-25|2017-04-19|Method for producing a part from composite material by injecting a loaded slip into a fibrous texture|
    BR112018071896A| BR112018071896A2|2016-04-25|2017-04-19|process for manufacturing a piece of composite material.|
    US16/096,034| US20190134848A1|2016-04-25|2017-04-19|A method of fabricating a composite material part by injecting a filled slurry into a fiber texture|
    CN201780028223.0A| CN109195930A|2016-04-25|2017-04-19|The method that fibrous texture manufactures composite material parts is injected by the way that slurry will be loaded|
    RU2018141255A| RU2728306C2|2016-04-25|2017-04-19|Method of making part from composite material by injecting slurry with filler into fibrous structure|
    [返回顶部]