Method for injecting a loaded slurry into a fibrous texture
11255203 · 2022-02-22
Assignee
Inventors
- Nicolas EBERLING-FUX (MOISSY-CRAMAYEL, FR)
- Eddy Goullianne (Moissy-Cramayel, FR)
- William Ros (Moissy-Cramayel, FR)
Cpc classification
B28B19/0092
PERFORMING OPERATIONS; TRANSPORTING
C04B2235/5228
CHEMISTRY; METALLURGY
C04B2235/616
CHEMISTRY; METALLURGY
F23R3/007
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2300/6033
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29C70/48
PERFORMING OPERATIONS; TRANSPORTING
B28B13/021
PERFORMING OPERATIONS; TRANSPORTING
C04B2235/5436
CHEMISTRY; METALLURGY
F01D9/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C04B35/573
CHEMISTRY; METALLURGY
C04B35/58
CHEMISTRY; METALLURGY
B28B19/00
PERFORMING OPERATIONS; TRANSPORTING
F01D5/282
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C04B2235/3418
CHEMISTRY; METALLURGY
C04B2235/5232
CHEMISTRY; METALLURGY
F02K1/82
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C04B35/80
CHEMISTRY; METALLURGY
C04B2235/3217
CHEMISTRY; METALLURGY
F23R2900/00018
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B28B23/0006
PERFORMING OPERATIONS; TRANSPORTING
F01D5/284
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C04B2235/3463
CHEMISTRY; METALLURGY
C04B2235/5445
CHEMISTRY; METALLURGY
International classification
F01D5/28
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B28B23/00
PERFORMING OPERATIONS; TRANSPORTING
C04B35/80
CHEMISTRY; METALLURGY
B28B19/00
PERFORMING OPERATIONS; TRANSPORTING
B29C70/48
PERFORMING OPERATIONS; TRANSPORTING
F01D5/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D9/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02K1/82
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D25/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B28B13/02
PERFORMING OPERATIONS; TRANSPORTING
C04B35/58
CHEMISTRY; METALLURGY
C04B35/573
CHEMISTRY; METALLURGY
Abstract
A method for manufacturing a part made of composite material includes injecting into a fibrous texture a slurry including at least one powder of refractory ceramic particles suspended in a liquid phase, filtering the liquid phase of the slurry and retaining the powder of refractory ceramic particles inside the texture so as to obtain a fibrous preform loaded with refractory ceramic particles, densifying the fibrous texture by treatment of the refractory ceramic particles present in the fibrous texture in order to form a refractory matrix in the texture. The method further includes, before injecting the slurry under pressure, pre-saturating the fibrous texture with a carrier fluid consisting in injecting into said texture a carrier fluid.
Claims
1. A method for manufacturing a part made of composite material comprising the following steps: forming a fibrous texture from refractory ceramic fibers, placing the fibrous texture in a mold cavity of an injection tooling, injecting under pressure and into the fibrous texture, placed in the mold cavity, a slurry including at least one powder of refractory ceramic particles or particles of a refractory ceramic precursor suspended in a liquid phase, filtering the liquid phase of the slurry using a filter of porous material provided with the mold cavity and retaining the powder of refractory ceramic particles or particles of a refractory ceramic precursor inside said fibrous texture so as to obtain a fibrous preform loaded with refractory ceramic particles or particles of a refractory ceramic precursor, densifying the fibrous texture by treatment of the refractory ceramic particles present in the fibrous texture in order to form a refractory matrix in said texture, wherein, after the step of placing the fibrous texture in the mold cavity of the injection tooling and before the step of injecting the slurry under pressure, the method comprises a step of pre-saturating the fibrous texture with a carrier fluid consisting of a liquid, the pre-saturating step consisting of injecting said carrier fluid into said fibrous texture while placed inside the mold cavity, said carrier fluid being filtered with said liquid phase of the slurry during the filtering, and wherein the injection tool comprises means for regulating a flow rate such that the step of pre-saturating the fibrous texture inside the mold cavity comprises regulating the flow rate of the injection of the carrier fluid.
2. The method according to claim 1, wherein the carrier fluid corresponds to the liquid phase of the slurry.
3. The method according to claim 1, wherein the carrier fluid pre-saturation step and the slurry injection step are performed continuously.
4. The method according to claim 1, wherein the pre-saturation step is stopped when pressure in the mold cavity reaches a predetermined pressure value.
5. The method according to claim 1, wherein, during the pre-saturation step, the carrier fluid is injected at a first determined flow rate and wherein, during the slurry injection step, said slurry is injected at a second determined flow rate similar to or different from the first flow rate.
6. The method according to claim 1, wherein, during the fibrous texture formation step, yarns are woven in a three-dimensional or multilayer weaving.
7. The method according to claim 1, wherein yarns of the fibrous texture are formed of fibers made of one or several of the following materials: alumina, mullite, silica, an aluminosilicate, a borosilicate, silicon carbide and carbon.
8. The method according to claim 1, wherein the refractory ceramic particles are made of a material chosen from: alumina, mullite, silica, an aluminosilicate, an aluminophosphate, zirconia, a carbide, a boride and a nitride.
9. The method according to claim 1, wherein the part made of composite material obtained constitutes a turbomachine vane, an after-body part, a combustion chamber, a flap, a post-combustion arm, a turbine ring, a mixer or a distributor.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) 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:
(2)
(3)
(4)
(5)
DETAILED DESCRIPTION OF EMBODIMENTS
(6) The method for manufacturing a part made of composite material in particular of the Oxide/Oxide or CMC type according to the present invention begins with the achievement of a fibrous texture 10 intended to form the reinforcement of the part.
(7) The fibrous structure is achieved in a known manner by weaving by means of a Jacquard-type loom on which a bundle of warp yarns or strands has been disposed in a plurality of layers, the warp yarns being bonded by weft yarns or vice versa. The fibrous texture can be achieved by stacking of plies or folds obtained by two-dimensional weaving (2D) or unidirectional sheets (UD) of yarns or cables or multidirectional sheets (nD) obtained by superimposition of several sheets UD in different directions and bonding of the UD sheets together, for example by sewing, by chemical bonding agent or by needling.
(8) The fibrous texture can also be achieved directly in a single piece by three-dimensional (3D) weaving. By “two-dimensional weaving” is meant here a conventional weaving mode by which each weft yarn passes from one side to the other of yarns of a single warp layer or vice versa. In the case of the injection of a loaded slurry in 2D fibrous textures, namely textures obtained by stacking of 2D plies or folds, the invention is particularly suitable for 2D textures of significant thickness, that is to say 2D fibrous textures having a thickness of at least 0.5 mm, preferably at least 1 mm.
(9) By “three-dimensional weaving” or “3D weaving” or even “multilayer weaving”, is meant here a weaving mode by which at least some of the weft yarns bind warp yarns on several layers of warp yarns or vice versa in a weaving corresponding to a weave which can be in particular chosen from one of the following weaves: interlock, multi-canvas, multi-satin and multi-twill.
(10) By “interlock weave or fabric”, is meant here a 3D-weave, whose each layer of warp yarns binds several layers of weft yarns with all the yarns of the same warp column having the same movement in the plane of the weave.
(11) By “multi-canvas weave or fabric”, is meant here a 3D-weaving with several layers of weft yarns, whose basic weave of each layer is equivalent to a weave of the conventional canvas type but with some points of the weave that bind the layers of weft yarn together.
(12) By “multi-satin weave or fabric”, is meant here a 3D-weaving with several layers of weft yarns, whose basic weave of each layer is equivalent to a weave of the conventional satin type but with some points of the weave that bind the layers of weft yarns together.
(13) By “multi-twill weave or fabric”, is meant here a 3D-weaving with several layers of weft yarns whose basic weave of each layer is equivalent to a weave of the conventional twill type but with some points of the weave that bind the layers of weft yarns together.
(14) The 3D textures, or textures formed by stacking of 2D plies or UD sheets, have a complex geometry in which it is difficult to introduce and evenly distribute suspended solid particles. The method of the invention is very well adapted for the introduction of a loaded slurry in 3D woven fibrous textures.
(15) The yarns used to weave the fibrous texture intended to form the fibrous reinforcement of the part made of composite material can be in particular formed of fibers made of one of the following materials: the alumina, the mullite, the silica, an aluminosilicate, a borosilicate, silicon carbide, carbon or a mixture of several of these materials.
(16) In the example described here, the fibrous texture 10 is achieved by 3D-weaving between a plurality of yarns of SiC fibers, the texture being consolidated after weaving by a chemical vapor infiltration of SiC. The fibrous texture 10 is here intended to form the fibrous reinforcement of a part made of SiC/SiC composite material (SiC fiber reinforcement densified by a SiC matrix).
(17)
(18) More specifically, the carrier fluid injection system here consists of a reservoir 141 containing a carrier fluid FP and whose outlet duct 144 is connected to the inlet of a peristaltic pump 142. The outlet of the peristaltic pump 142 is connected to the injection port 1120 by ducts 145 and 146 between which a valve 143 is interposed. The loaded slurry injection system 150 here consists of an injection pot 151 which delimits a chamber 1510 containing a loaded slurry BC, the injection pot 151 being further equipped with a piston 1511 and, opposite said piston, a discharge opening 1512 connected to the injection port 1120 by ducts 153 and 154 between which a valve 152 is interposed.
(19) Once the fibrous texture 10 is achieved, it is placed in the injection tooling 100 which allows, as explained below, depositing refractory ceramic particles or particles of a refractory ceramic precursor within the fibrous texture.
(20)
(21) The pre-saturation step ends when the carrier fluid saturation in the fibrous texture is considered complete, that is to say when the pressure in the mold cavity 113 (pressure loss of the carrier fluid injection system) reaches a stability threshold, for example 600 millibars. The measurement of the achievement of the pressure stability threshold at the end of the pre-saturation step can be carried out by means of a pressure sensor 160, for example a pressure gauge, placed at the injection port 1120 of the injection tooling 100. The measurement of the pressure in the mold cavity can also be carried out with pressure sensors placed on the surface of the mold cavity (not represented in
(22) Once the pre-saturation step is completed, the step of injecting the loaded slurry BC into the fibrous texture 10 is carried out as illustrated in
(23) During this step, the loaded slurry BC is injected into the mold cavity 113 under a monitored pressure or flow rate. During this step, the carrier fluid injection system 140 is inoperative, the peristaltic pump 142 being stopped and the valve 143 being closed. On the side of the loaded slurry injection system 150, the slurry BC is delivered at a regulated flow rate into the injection port 1120 by the injection pot 151, the valve 152 being open, the slurry BC being here injected at a minimum flow rate of 2 cm.sup.3/min. The regulation of the flow rate is controlled by the piston 1511 of the injection pot 151 so as to deliver the loaded slurry at a flow rate lower than the carrier fluid injection flow rate. In
(24) As illustrated in
(25) Once the injection and filtration steps have been carried out, a fibrous preform loaded with refractory ceramic particles, in this case SiC particles, is obtained. The obtained preform is then dried and demolded, the preform being able to retain after demolding the form adopted in the mold cavity.
(26) The preform is then densified by a treatment of the particles present in the preform. In the case of oxide particles for example, the treatment consists in subjecting the particles to a sintering heat treatment, for example under air at a temperature comprised between 1000° C. and 1200° C. in order to sinter the particles and thus form a refractory ceramic matrix in the porosity of the fibrous preform. In the case of SiC particles, as in the example described here, the SiC particles are impregnated with silicon by infiltration of the preform with melt silicon (MI “Melt Infiltration” process) so as to form a SiC matrix. This gives a part made of composite material, here SiC/SiC 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 throughout the fibrous reinforcement.
(27)
(28) In
(29) The method of the invention is not limited to the injection of a slurry comprising SiC particles suspended in water. More generally, the slurries used can be a suspension including refractory ceramic particles having an average particle size comprised between 0.1 μm and 10 μm. The volume content of refractory ceramic particles in the slurry can, before injection, be comprised between 1% and 50%, preferably between 20% and 35% by volume. The refractory ceramic particles may include a material chosen from: the alumina, the mullite, the silica, the aluminosilicates, the aluminophosphates, the carbides, the borides, the nitrides and mixtures of such materials. Depending on their basic composition, the refractory ceramic particles can, in addition, be mixed with particles of alumina, zirconia, aluminosilicate, a rare-earth oxide, rare-earth silicate (which can for example be used in environmental or thermal barriers) or any other filler making it possible to make functional the composite material part to be obtained, such as carbon black, graphite or silicon carbide.
(30) The liquid medium or phase of the slurries can, for example, also include an aqueous phase having an acidic pH (i.e. a pH less than 7) and/or an alcoholic phase including for example ethanol. The slurry may include an acidifier such as nitric acid and the pH of the liquid medium may for example be comprised between 1.5 and 4. The slurry may, in addition, include an organic binder such as polyvinyl alcohol (PVA) which is in particular soluble into water. More generally, the slurry may comprise: a carrier fluid, a dispersant (e.g. suitable pH), a binder (e.g. PVA), a plasticizer (e.g. PVA), an anti-foaming agent, a wetting agent.
(31) A part made of CMC composite material other than Oxide/Oxide material can be obtained in the same way by achieving the fibrous texture with fibers of silicon carbide and/or carbon and by using a slurry loaded with carbide particles (for example SiC, B.sub.4C or TiC), boride (for example TIB.sub.2), nitride (for example Si.sub.3N.sub.4), or silicide (for example TiSi.sub.2).