专利摘要:
The invention relates to a method of manufacturing a fibrous preform charged with refractory ceramic particles (20) comprising the following steps: a) placing a fibrous texture (1) comprising refractory ceramic fibers in a molding cavity (2) defined by a mold (3) and a counter-mold (4; 4 '), b) injection of a slip, comprising a powder of refractory ceramic particles (20) present in a liquid medium, in the porosity of the fibrous texture (1) present in the molding cavity (2), the injection being performed at least through a first face (la) or a first edge (la ') of said fibrous texture (1), and c drainage by a piece of porous material (5) from the liquid medium of the slip having penetrated the fibrous texture (1), the piece of porous material having a thickness greater than or equal to 0.1 mm, the drainage being carried out at least through a second face (lb) or a second th edge of the fibrous texture (1) different from the first face (la) or the first edge (1a '), said piece of porous material (5) also making it possible to retain the powder of refractory particles (20) in the porosity the fibrous texture (1) to obtain a fibrous preform loaded with refractory particles (20).
公开号:FR3030505A1
申请号:FR1463286
申请日:2014-12-23
公开日:2016-06-24
发明作者:Cabre Catherine Billotte;Nicolas Droz;Ludovic Liais;Michael Podgorski;Edu Ruiz;Sylvain Turenne
申请人:Safran SA;SNECMA SAS;
IPC主号:
专利说明:

[0001] BACKGROUND OF THE INVENTION The invention relates to methods for manufacturing composite material parts comprising a fibrous preform and a refractory ceramic matrix. The present invention relates to a method of manufacturing a piece of thermostructural composite material having a ceramic matrix (CMC), that is to say having a fibrous reinforcement formed from refractory ceramic fiber fibers whose porosity is filled by a matrix also refractory ceramic material, the invention particularly relates to a method of manufacturing a piece of the type Oxide / Oxide. 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 the layers thus arranged are then compacted using a counter mold or a vacuum cover. In the case where a vacuum cover is used, the pre-impregnated layers can for example be autoclaved (pre-impregnated type "CMO" method). The filled preform thus obtained is then subjected to sintering so as 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 make other pieces of ceramic matrix composite material (CMC). In this case, the fibrous layers may be made from silicon carbide (SiC) or carbon (C) fibers and may be impregnated with a slurry loaded with carbide (eg SiC), boride (by example of T1B2), nitride (for example Si3N4) or oxide, for example alumina or zirconia. However, this type of production method can only achieve pieces of ceramic matrix composite material having a small thickness and two-dimensional (2D) fibrous reinforcement. The mechanical characteristics of these composite materials are very different depending on the directions inherent in the structure of the reinforcement. More specifically, these materials have a low mechanical resistance to delamination and out-of-plane forces. 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 aspiration "APS", make it possible to penetrate a loaded suspension in the fibrous texture whose thickness can reach several tens of millimeters depending on the intended applications. However, in the context of producing a piece of ceramic matrix material, these methods have certain disadvantages. Indeed, the impregnation of a fibrous texture of complex geometry and of great thickness may not be achieved by an infusion type process because this type of process may not achieve a sufficient pressure gradient to obtain good impregnation of the entire texture. The method of the APS type does not, for its part, to finely control the amount of matrix introduced into the preform or the surface conditions. If the RTM process can be used to impregnate a fibrous texture with a loaded slurry, it nevertheless requires the implementation of a step of elimination (evacuation and / or evaporation) of the liquid medium of the slurry so as not to leave solid charges in the preform before sintering. This additional step results in an increase in the time of implementation of the method. Moreover, this step of elimination of the liquid medium can lead to a loss of particles and / or to a modification of the distribution of the latter in the preform and thus to the appearance of macro porosities in the final material because of lack of matrix in some places. It should also be taken into account that, in the RTM processes employing a slurry injection step, it may be necessary to limit the volume ratio of refractory ceramic particles present in the slurry in order to maintain a sufficient viscosity. low to allow a homogeneous injection of the slip. This constraint may lead to having to repeat the injection step of the slip and, consequently, the elimination step of the liquid medium in order to eventually obtain the desired volume ratio of the matrix. The limitation of the volume content of refractory ceramic particles in the slip can therefore lead to a complexification of the manufacturing range.
[0002] There is therefore a need to simplify processes for producing preforms loaded with refractory particles for forming composite material parts having a desired matrix volume ratio. There is still a need for fast and reliable processes for manufacturing composite material parts having the desired properties from a thick fibrous texture and / or complex geometry. OBJECT AND SUMMARY OF THE INVENTION For this purpose, the invention proposes, according to a first aspect, a method of manufacturing a fiber preform loaded with refractory ceramic particles comprising the following steps: a) placement of a fibrous texture comprising refractory ceramic fibers in a mold cavity defined by a mold and against a mold, b) injection of a slip, comprising a powder of refractory ceramic particles present in a liquid medium, in the porosity of the fibrous texture present in the cavity molding, the injection being carried out at least through a first face or a first edge of said fibrous texture, and c) drainage by a piece of porous material of the liquid medium of the slip having penetrated into the fibrous texture the piece of porous material having a thickness greater than or equal to 0.1 mm, the drainage being effected at least through a second face or a second edge of the fibrous texture different from the first face or the first edge, said piece of porous material also making it possible to retain the powder of refractory particles in the porosity of the fibrous texture in order to obtain a fiber preform loaded with refractory particles. An edge designates one side of the fibrous texture extending along the thickness thereof (ie along the smaller dimension of the fibrous texture), the sides of the fibrous texture which are not edges are called "faces". For example, in the case where the fibrous texture is in the form of a plate, it has two opposite faces ("front" and "back") and one or more edges. In the case where the fibrous texture is intended to constitute the fibrous reinforcement of a blade, the edges of the fibrous texture will be intended to constitute the leading edge and the trailing edge of the blade and the faces of the texture fibrous are going to be intended to constitute the intrados or the extrados of the dawn. The thickness of the piece of porous material corresponds to its smallest dimension. By using a piece of porous material making it possible to selectively drain the liquid medium from the slip, the method according to the invention makes it possible to eliminate the liquid medium from the slip introduced into the fibrous texture while retaining in the fibrous texture the ceramic solid particles. refractory. Due to the use of the porous material part allowing the selective elimination of the liquid medium, the invention advantageously makes it possible to obtain an accumulation of refractory particles in the fibrous texture. The invention thus makes it possible to successfully use processes in which the slip is injected into the porosity of a fibrous texture and which requires the use of relatively low-loaded slip materials while allowing a degree of charge to be obtained. refractory ceramic particles high in texture and, therefore, a high matrix volume ratio after sintering of these particles. The method according to the invention thus makes it possible to obtain in a simple manner thermostructural composite material parts having improved mechanical properties. During step b), the slip is injected into the molding cavity through one or more injection ports. During step c), the drainage of the liquid medium is carried out through at least one outlet vent. The drainage of step c) is carried out by applying a pressure difference between the injection port and the outlet vent. This pressure difference can be applied by various means, and for example by injection under pressure of the slip during step b) and / or by pumping at the outlet vent and / or by applying a pressure of compaction on the fibrous texture by the mold and against the mold. It is advantageous to perform a single injection phase of the slip. Alternatively, one can perform a first phase of injection of the slip, interrupt the injection of the slip then perform a second phase of injection of the slip. In an exemplary embodiment, the mold may constitute a rigid support on which the fibrous texture is present and the counter-mold may be rigid.
[0003] In other words, in this case, the mold and the counter-mold do not deform during the implementation of the method according to the invention. Such an embodiment advantageously makes it possible to manufacture a piece of composite material of precise shape imposed by the shape of the mold and the counter-mold. Such a control of the shape of the part to be manufactured is advantageous especially when it is intended to be used in the aeronautical field. In an exemplary embodiment, the mold may constitute a rigid support on which the fibrous texture is present and the against-mold may be deformable.
[0004] In an exemplary embodiment, the piece of porous material may be present between the mold and the fibrous texture or between the counter-mold and the fibrous texture. In an exemplary embodiment, the piece of porous material may constitute all or part of the mold or counter-mold.
[0005] In an exemplary embodiment, the against-mold may exert pressure on the fibrous texture during and / or after step b). The application of such a pressure on the fibrous texture advantageously makes it possible to accelerate the impregnation of the fibrous texture with the slip and to accelerate the drainage of the liquid medium.
[0006] In an exemplary embodiment, the fibrous texture can be compacted between the mold and the counter-mold during and / or after step b). In other words, in this case, the fibrous texture is in a compacted form between the mold and the counter-mold during and / or after step b) due to the application of a compaction pressure by the against mold.
[0007] In addition to the advantage described above relating to the application of a pressure on the fibrous texture, the fact of compacting the fibrous texture advantageously makes it possible to reach a target thickness for it and consequently to reach a target thickness for the piece of composite material to obtain.
[0008] In an exemplary embodiment, the compaction pressure can be applied before step b) and then be maintained during step b). Alternatively, step b) can be initiated first and then the compaction pressure can be applied after the start of step b) and then maintained.
[0009] The pressure exerted by the counter-mold on the fibrous texture can be obtained by applying a fluid (gas or liquid) on the counter-mold, the fluid being introduced into a chamber, the counter-mold being located between the chamber and the molding cavity. During step c), a pumping at the sottie vent may be performed to suck all or part of the liquid medium present in the porosity of the fibrous texture. Alternatively or in combination, it is possible during step c) to heat the liquid medium present in the porosity of the fibrous texture in order to evaporate it through the second face or the second edge of the fibrous texture and through the piece of porous material. In an exemplary embodiment, the injection of the slip can be carried out during step b) through a plurality of different zones of the outer surface of the fibrous texture. In an exemplary embodiment, the slip can during step b) be injected through a plurality of injection ports opening into different areas of the mold cavity. Alternatively or in combination, a slip stream distribution element may be present in the molding cavity, said distribution element defining a plurality of pores in which the slip flows during step b) to join the first face or the first edge of the fibrous texture.
[0010] Such an embodiment makes it possible to perform a multi-point injection in the fibrous texture and consequently to obtain in a homogeneous and faster manner a homogeneous distribution of the refractory ceramic particles in the fibrous texture.
[0011] In an exemplary embodiment, injection of the slip may be performed on a first side of the fibrous texture and drainage of the liquid medium may be effected from a second side of the fibrous texture opposite to the first side. In an exemplary embodiment, the slip may be injected during step b) at least through an edge of the fibrous texture and the drainage may be carried out in step c) at least through a face of the fibrous texture. In an exemplary embodiment, the slip may be injected during step b) at least through a first face of the fibrous texture and the drainage may be carried out in step c) at least through a second face of the fibrous texture different from the first face. In an exemplary embodiment, the slip may have, prior to step b), a volume content of ceramic refractory particles less than or equal to 40%. The use of a slurry having such a volume ratio of refractory ceramic particles advantageously makes it possible to improve the injection capacity of the slip by limiting its viscosity. Thus, the viscosity of the slip before step b) may advantageously be less than or equal to 150 mPa.s-1, or even 60 mPa.s-1. The viscosity of the slip is measured using a Brookfield type viscometer at a temperature of 20 ° C. In an exemplary embodiment, the slip may comprise an organic binder.
[0012] The use of an organic binder in the slip is advantageous because it makes it possible to improve the hold of the raw material (dried injected preform before sintering the refractory ceramic particles), which is advantageous especially when the fibrous texture has a complex geometry. The use of an organic binder is also advantageous in order to maintain the volume content of fibers by improving the control of the thickness after the injection of the slip.
[0013] Moreover, the slip used may be free of a pre-ceramic polymer such as precursors of polysilane-based ceramic material. Alternatively, the slip may comprise a pre-ceramic polymer. In an exemplary embodiment, the refractory particles may be the only solid phase present in the slip used. In an exemplary embodiment, the fibrous texture may comprise a plurality of refractory oxide fibers and the refractory particles may be of refractory oxide.
[0014] The present invention also relates to a method for manufacturing a composite material part comprising the following step: d) sintering the refractory ceramic particles present in the fibrous preform obtained after carrying out a process as described above in order to forming a refractory matrix in the porosity of said preform. The part obtained after sintering may, for example, constitute a turbomachine blade. It is possible before the sintering step to demold the filled preform obtained at the end of step c) and place it in an oven in which the sintering will be performed. BRIEF DESCRIPTION OF THE DRAWINGS Other features 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: FIGS. 1 and 2 show schematically and partially the configuration obtained following the implementation of different steps of a first exemplary method according to the invention, - Figure 3 shows, schematically and partially, the configuration obtained. during injection and drainage in a variant of the process according to the invention in which a "poly-flex" type process is used, - FIG. 4 represents, in a schematic and partial manner, the configuration obtained during injection and drainage in an alternative method according to the invention, and - Figure 5 shows, schematically and partially, the configuration obtained penda injection and drainage in an alternative process according to the invention.
[0015] DETAILED DESCRIPTION OF EMBODIMENTS FIG. 1 shows the configuration obtained after implementation of step a) in a first exemplary method according to the invention. As illustrated in FIG. 1, a fibrous texture 1 comprising refractory ceramic fibers is present in a molding cavity 2. The fibrous texture 1 may be produced in a known manner by weaving using a Jacquard loom or shuttle on which a bundle of warp or strand wires has been arranged in a plurality of layers, the warp threads being tied by weft threads 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.
[0016] The method according to the invention can be 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.
[0017] 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.
[0018] 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 can be 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 fibrous texture intended to form the fibrous reinforcement of the composite material part may comprise fibers chosen from: alumina fibers, mullite fibers, silica fibers, aluminosilicate fibers, borosilicate fibers, silicon carbide fibers, carbon fibers and mixtures of such fibers. The fibrous texture used can for example be made by 2D weaving or by 3D weaving (stacking 2D strata or 3D weaving). The fibrous texture can also be made by stacking several fibrous structures obtained by 3D weaving. The fibrous texture used may, for example, comprise a plurality of Nextel 61OTM alumina wires.
[0019] The molding cavity 2 is delimited by a mold 3 and a counter-mold 4. In the example illustrated, the mold 3 and the counter-mold 4 are rigid. The mold 3 constitutes a rigid support on which the fibrous texture 1 is present during the injection and drainage steps b) and c). The mold 3 comprises lateral walls 3a and 3b delimiting the molding cavity 2. In the example illustrated, the device 10 in which the fibrous texture 1 is present is closed in its lower part by the mold 3 and is closed in its part. upper by the against-mold 4 forming a cover closing the device 10. The mold 3 and against the mold 4 are used to size the preform and thus the part to obtain and adjust the fiber volume ratio in the room to obtain .
[0020] The counter-mold 4 comprises a plurality of injection ports 15 of the slip through which the slip is intended to be injected in order to penetrate the porosity of the fibrous texture 1 through the first face 1a of the fibrous texture 1 In the example illustrated in FIG. 1, the slip is intended to be injected through a plurality of injection ports 15 opening into different areas of the molding cavity. However, it is not beyond the scope of the invention when the slip is injected through a single injection pore. The mold 3 comprises, meanwhile, a single outlet port 16 of the liquid medium of the slurry. Of course, it is not beyond the scope of the invention when a plurality of output vents are implemented. In the example illustrated, the piece of porous material 5 is present in the molding cavity 2 between the mold 3 and the fibrous texture 1. The piece of porous material 5 is present between the outlet vent 16 and the fibrous texture 1 In the example illustrated, the piece of porous material 5 is present in contact with the mold 3 and in contact with the second face 1b of the fibrous texture 1 through which the drainage of the liquid medium of the slurry is intended to be carried out. . The second face 1b of the fibrous texture 1 is, in the example illustrated in FIG. 1, situated on the side opposite to the first face 1a through which the slip is intended to penetrate into the texture 1. The piece of porous material 5 may for example be made of microporous polytetrafluoroethylene (PTFE) such as "microporous PTFE" products sold by the company PorexC). For example, the PM 0130 material sold by the company PorexC) having a pore size of between 1 μm and 2 μm can be used for producing the porous material part 5. In the example shown, the piece of porous material 5 extends along the entire second face 1b and completely covers the outlet vent 16. It is not beyond the scope of the present invention when the piece of material porous 5 extends along only a portion of the second face 1b and completely covers the outlet vent 16. In a variant not shown, the piece of porous material can extend along the entire second face and extend beyond it. The piece of porous material 5 allows drainage of the liquid medium of the slip outside the fibrous texture 1 and its evacuation through the outlet vent 16 due to the application of a pressure gradient between the vent 16 and the injection ports 15. The piece of porous material 5 has a thickness greater than or equal to 0.1 mm. For example, the piece of porous material 5 may have a thickness greater than or equal to 1 mm, or even several millimeters. The average porosity level of the porous material part 5 can be about 30%. The average pore size (D 50) of the porous material part 5 may for example be between 1 μm and 2 μm.
[0021] In an exemplary embodiment, the piece of porous material 5 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 piece of composite material to obtain. Before implementation of step b), a compaction pressure for compacting the fibrous texture 1 between the mold 3 and the counter-mold 4 can be applied, this compaction pressure can be maintained during step b). Alternatively, the compaction pressure may be applied after the start of injection of the slip (i.e. after the start of step b)) and can then be maintained. In particular, the compaction pressure can be applied once the injection of the slurry is complete and can then be maintained. For example, the fibrous texture may during and / or after step b) be subjected to a compaction pressure less than or equal to 15 bar, for example 7 bar. The fibrous texture may during and / or after step b) be subjected to a compaction pressure greater than or equal to 0.3 bar. The application of a compaction pressure can be used to compact the texture to help drain the liquid medium and reach a target thickness for the fiber preform without damaging it.
[0022] As mentioned above, the compaction pressure can be applied by a fluid applied to the counter-mold 4 on the opposite side to the molding cavity 2. FIG. 2 illustrates the configuration obtained during the injection of the slip and drainage of the liquid medium. The slip has been injected through the injection ports 15 to penetrate the fibrous texture 1 through the first face 1a of the fibrous texture 1. The refractory particles present in the slip are intended to allow the formation of a refractory ceramic matrix in the porosity of the fibrous texture 1. 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 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 step b), be between 25% and 40%. The refractory ceramic particles may comprise a material chosen from: alumina, mullite, silica, aluminosilicates, alurninophosphates, carbides, borides, nitrides and mixtures of such materials.
[0023] 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. 2, the refractory ceramic particles 20 are present after injection of the slip into the porosity of the fibrous texture 1. The arrows 21 represent the movement of the slip injected into the fibrous texture 1. The arrows 22 represent they the movement of the liquid medium of the slip sucked by the piece of porous material 5. The counter-mold 4 exerts pressure on the fibrous texture 1 during and / or after step b) to accelerate the drainage of the liquid medium . Pumping may, in addition, be carried out at the outlet vent 16 during step c), 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 step c) 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 5 makes it possible to retain in the fibrous texture 1 the refractory ceramic particles 20 initially present in the slip and that all or part of these particles 20 are deposited by filtration in the fibrous texture 1. injection and drainage steps performed, a fibrous preform is obtained which is filled with refractory ceramic particles, for example particles of refractory ceramic oxide, for example alumina.
[0024] The preform obtained is then dried and then demolded, the preform can retain after demolding the shape adopted in the molding cavity, for example its shape adopted after comaction between the mold and against the mold. 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 Oxide / Oxide composite 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 any 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). There is shown in Figure 3 an alternative embodiment in which the counter-mold 4 'is deformable. Pressure is exerted on the deformable against-mold 4 'in order to maintain the deformable against-mold 4' against the first face 1a of the fibrous texture 1. As described above, the counter mold 4 'can exert a pressure on the fibrous texture 1 during the process. FIG. 3, as described above, also shows the presence of refractory particles in the porosity of the fibrous texture 1 as well as the drainage of the liquid medium from the injected slip (arrows 22). FIG. 4 shows an alternative embodiment in which a slip stream distribution element 30 here in the form of a grid is present between the first face 1a of the fibrous texture 1 and the injection port 15. This distribution element 30 is in contact with the first face 1a of the fibrous texture 1. This distribution element 30 defines a plurality of pores 31 in which the slip flows during the injection to reach the first face of the texture. fibrous 1. The pores 31 may or may not be evenly spaced along the first side of the fibrous texture 1. The distribution element 30 can as shown define at least two or even at least three pores 31. Such a mode embodiment advantageously makes it possible to accelerate the obtaining of a uniform distribution of the refractory particles in the fibrous texture 1. Of course, it is possible to couple the implementation of such a repair element. in that the slip is injected through a plurality of injection ports opening into different areas of the molding cavity. The other details relating to the method implemented described above are applicable to this embodiment. In particular, in a non-illustrated variant, a deformable counter mold 4 'is used instead of the rigid counter mold 4. FIG. 5 shows a variant embodiment in which the mold 3 forming a support for the fibrous texture 1 comprises sidewalls 3a and 3b through which injection of the slip is carried out. The injection is carried out through edges 1 'of the fibrous texture 1. The slip is injected under pressure into the fibrous texture 1. In the example illustrated in FIG. 5, the liquid medium is discharged through the face 1b. superior fibrous texture. Thus, in the case of Figure 5, the injection and drainage are not on two opposite sides of the fibrous texture. In this case, the slip is injected through an edge 1 'of the fibrous texture and the liquid medium is discharged through the upper face 1b of the fibrous texture 1.
[0025] The expression "comprising / containing / including a" should be understood as "containing / containing / including at least one". The expression "understood between ... and ..." or "from ... to ..." must be understood as including the boundaries.
权利要求:
Claims (16)
[0001]
REVENDICATIONS1. A method of manufacturing a fibrous preform loaded with refractory ceramic particles (20) comprising the steps of: a) placing a fibrous texture (1) comprising refractory ceramic fibers in a molding cavity (2) delimited by a mold ( 3) and a counter-mold (4; 4 '), b) injecting a slip, comprising a powder of refractory ceramic particles (20) present in a liquid medium, in the porosity of the fibrous texture (1) present in the molding cavity (2), the injection being carried out at least through a first face (1a) or a first edge (la ') of said fibrous texture (1), and c) drainage by a piece in porous material (5) of the liquid medium of the slip having penetrated into the fibrous texture (1), the piece of porous material having a thickness greater than or equal to 0.1 mm, the drainage being carried out at least through a second face (lb) or a second edge of the texture fibrous (1) different from the first face (1a) or the first edge (la '), said porous material piece (5) further allowing the refractory particle powder (20) to be retained in the porosity of the fibrous texture ( 1) to obtain a fibrous preform loaded with refractory particles (20).
[0002]
2. Method according to claim 1, characterized in that the mold (3) constitutes a rigid support on which the fibrous texture (1) is present and the against-mold (4) is rigid.
[0003]
3. Method according to claim 1, characterized in that the mold (3) constitutes a rigid support on which the fibrous texture (1) is present and the counter-mold (4 ') is deformable.
[0004]
4. Method according to any one of claims 1 to 3, characterized in that the piece of porous material (5) is present between the mold (3) and the fibrous texture (1) or between the counter-mold (4; ') and the fibrous texture (1).
[0005]
5. Method according to any one of claims 1 to 3, characterized in that the piece of porous material (5) constitutes all or part of the mold (3) or counter-mold (4).
[0006]
6. Method according to any one of claims 1 to 5, characterized in that the against-mold (4) exerts pressure on the fibrous texture (1) during and / or after step b).
[0007]
7. Method according to claim 6, characterized in that the fibrous texture (1) is compacted between the mold (3) and the counter-mold (4) during and / or after step b).
[0008]
8. Method according to any one of claims 1 to 7, characterized in that the injection of the slip is carried out in step b) through a plurality of different areas of the outer surface of the fibrous texture (1).
[0009]
Method according to claim 8, characterized in that a slip stream distribution element (30) is present in the molding cavity (2), said distribution element (30) defining a plurality of pores (31) in wherein the slip flows during step b) to join the first face (la) or the first edge (1 ') of the fibrous texture (1).
[0010]
10.Procédé according to any one of claims 1 to 9, characterized in that the injection of the slurry is performed on a first side of the fibrous texture and the drainage of the liquid medium is performed on a second side of the fibrous texture opposite the first side.
[0011]
11.Procédé according to any one of claims 1 to 9, characterized in that the slip is injected during step b) at least through an edge (la ') of the fibrous texture and in that the drainage is performed in step c) at least through a face (lb) of the fibrous texture.
[0012]
12. Method according to any one of claims 1 to 11, characterized in that the slip is injected during step b) at least through a first face (1a) of the fibrous texture and in that the drainage is carried out in step c) at least through a second face (lb) of the fibrous texture different from the first face (1a).
[0013]
13.Procédé according to any one of claims 1 to 12, characterized in that the slip has, before step b), a volume content of refractory ceramic particles (20) less than or equal to 40%.
[0014]
14.Procédé according to any one of claims 1 to 13, characterized in that the slip has an organic binder.
[0015]
15.Procédé according to any one of claims 1 to 14, characterized in that the fibrous texture (1) comprises refractory oxide fibers and in that the refractory particles are refractory oxide.
[0016]
16. A method of manufacturing a composite material part comprising the following step: d) sintering the refractory particles (20) present in the fibrous preform obtained after carrying out a method according to any one of claims 1 to To form a refractory matrix in the porosity of said preform.
类似技术:
公开号 | 公开日 | 专利标题
FR3030505B1|2019-07-12|PROCESS FOR PRODUCING A FIBROUS PREFORM CHARGED WITH REFRACTORY CERAMIC PARTICLES
EP3359506B1|2022-02-09|Process for the manufacturing of a ceramic composite part by injection of a loaded slurry in a porous mould
FR3050454B1|2019-07-12|PROCESS FOR MANUFACTURING A COMPOSITE MATERIAL PART BY INJECTING A BARBOTIN CHARGED WITH FIBROUS TEXTURE
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
WO2019058050A1|2019-03-28|Method for injecting a loaded suspension into a fibrous texture and method for producing a part from composite material
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
WO2019197757A1|2019-10-17|Method for producing a part made from a composite material by means of the injection of a laden ceramic slurry into a fibrous structure
WO2020234550A1|2020-11-26|Method for producing a part from composite material by injecting a loaded slip into a fibrous texture
WO2018234669A1|2018-12-27|Process for manufacturing a composite material part having one or more local thickness variations
WO2020074813A1|2020-04-16|Method for manufacturing a part made of composite material with compliance control
WO2021005282A2|2021-01-14|Method for producing a part from composite material by injecting a filled slip into a fibrous texture
同族专利:
公开号 | 公开日
CA2972170A1|2016-06-30|
US10239795B2|2019-03-26|
CN107206624A|2017-09-26|
EP3237660B1|2018-12-05|
US20170369382A1|2017-12-28|
WO2016102839A1|2016-06-30|
EP3237660A1|2017-11-01|
FR3030505B1|2019-07-12|
引用文献:
公开号 | 申请日 | 公开日 | 申请人 | 专利标题
FR2326275A1|1975-10-01|1977-04-29|Gremigni Giuseppe|Moulds for asbestos cement tile production by pressure injection - have drain holes for water evacuation with tile sandwiched by elastic filters|
US5436042A|1994-03-11|1995-07-25|The Carborundum Company|Ceramic fiber-reinforced composite articles and their production|
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|
EP2181974A1|2008-10-31|2010-05-05|AVIO S.p.A.|Method for the production of components made of ceramic-matrix composite material|
FR2958933A1|2010-04-20|2011-10-21|Onera |PROCESS FOR PRODUCING A CERAMIC MATRIX COMPOSITE PIECE|WO2019058069A1|2017-09-21|2019-03-28|Safran Ceramics|Method for manufacturing a part using cmc|
WO2019068996A1|2017-10-03|2019-04-11|Safran Ceramics|Production in composite material of a lobed structure of a flow mixer|
FR3072672A1|2017-10-24|2019-04-26|Safran Ceramics|INSTALLATION FOR DEPOSITING A LOADED FISHING MECHANISM|
WO2020128364A1|2018-12-21|2020-06-25|Safran Ceramics|Tool and method for manufacturing a composite-material part by means of a liquid process|
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|
CN112895115A|2021-01-14|2021-06-04|北京建筑大学|Combined BFRP-FRCM composite layer steel mold and using method thereof|US5316462A|1993-02-18|1994-05-31|William Seemann|Unitary vacuum bag for forming fiber reinforced composite articles|
US5489408A|1993-03-08|1996-02-06|Agency Of Industrial Science & Technology|Method for producing ceramics reinforced with three-dimensional fibers|
CN102896782B|2011-07-29|2014-12-24|深圳光启高等理工研究院|Preparation method of medium substrate|
CN102700203B|2012-06-15|2014-10-29|哈尔滨工业大学|Preparation method of carbon fiber composite material laminated plate with piezoelectric damping|
WO2014204672A1|2013-06-20|2014-12-24|GKN Aerospace Services Structures, Corp.|Method for infusing resin into a composite laminate|
CN103979918B|2014-05-30|2016-06-01|秦菊霞|A kind of fiber reinforcement fireproof heated board and preparation technology thereof|US10144065B2|2015-01-07|2018-12-04|Kennametal Inc.|Methods of making sintered articles|
FR3041890B1|2015-10-05|2017-11-24|Snecma|PROCESS FOR MANUFACTURING A COMPOSITE MATERIAL PART BY INJECTING A BARBOTIN CHARGED IN A POROUS MOLD|
ITUB20160498A1|2016-01-27|2017-07-27|Consiglio Nazionale Ricerche|Composite materials based on C / SiC fibers with ultra-refractory matrix with high toughness and resistance to ablation|
US11065863B2|2017-02-20|2021-07-20|Kennametal Inc.|Cemented carbide powders for additive manufacturing|
FR3063725B1|2017-03-07|2019-04-12|Safran Ceramics|METHOD FOR PRODUCING A CONSOLIDATED FIBROUS PREFORM|
FR3067960B1|2017-06-23|2022-01-14|Safran Ceram|METHOD FOR MANUFACTURING A FIBROUS PREFORM LOADED WITH PARTICLES|
FR3071257B1|2017-09-19|2021-08-20|Safran Ceram|PROCESS FOR INJECTING A SUSPENSION LOADED IN A FIBROUS TEXTURE AND PROCESS FOR MANUFACTURING A PART FROM COMPOSITE MATERIAL|
FR3071245B1|2017-09-21|2019-09-20|Safran Ceramics|METHOD FOR INJECTING A BARBOTIN CHARGED WITH FIBROUS TEXTURE|
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|
DE112020001416T5|2019-03-25|2021-12-09|Kennametal Inc.|ADDITIVE MANUFACTURING TECHNIQUES AND THEIR APPLICATIONS|
US20210355038A1|2020-05-12|2021-11-18|Goodrich Corporation|Methods and systems for in-plane slurry infiltration of composite preforms|
法律状态:
2015-12-15| PLFP| Fee payment|Year of fee payment: 2 |
2016-06-24| PLSC| Publication of the preliminary search report|Effective date: 20160624 |
2016-12-05| PLFP| Fee payment|Year of fee payment: 3 |
2017-11-21| PLFP| Fee payment|Year of fee payment: 4 |
2018-02-02| CD| Change of name or company name|Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170719 Owner name: SAFRAN, FR Effective date: 20170719 |
2019-11-20| PLFP| Fee payment|Year of fee payment: 6 |
2020-11-20| PLFP| Fee payment|Year of fee payment: 7 |
2021-11-18| PLFP| Fee payment|Year of fee payment: 8 |
优先权:
申请号 | 申请日 | 专利标题
FR1463286A|FR3030505B1|2014-12-23|2014-12-23|PROCESS FOR PRODUCING A FIBROUS PREFORM CHARGED WITH REFRACTORY CERAMIC PARTICLES|
FR1463286|2014-12-23|FR1463286A| FR3030505B1|2014-12-23|2014-12-23|PROCESS FOR PRODUCING A FIBROUS PREFORM CHARGED WITH REFRACTORY CERAMIC PARTICLES|
CA2972170A| CA2972170A1|2014-12-23|2015-12-18|Method for manufacturing a fibrous preform filled with refractive ceramic particles|
US15/538,982| US10239795B2|2014-12-23|2015-12-18|Method of fabricating a fiber preform filled with refractory ceramic particles|
EP15823672.9A| EP3237660B1|2014-12-23|2015-12-18|Process for the manufacturing of a fibrous preform loaded with ceramic refractory particles|
CN201580075954.1A| CN107206624A|2014-12-23|2015-12-18|The method of fiber preform of the manufacture filled with refractory ceramic particles|
PCT/FR2015/053621| WO2016102839A1|2014-12-23|2015-12-18|Method for manufacturing a fibrous preform filled with refractive ceramic particles|
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