Method for manufacturing a refractory part made of composite material
A method of fabricating a part out of composite material, includes forming a fiber texture from refractory fibers; placing the texture in a mold having an impregnation chamber including in its bottom portion a part made of porous material, the impregnation chamber being closed in its top portion by a deformable impermeable diaphragm separating the impregnation chamber from a compacting chamber; injecting a slip containing a powder of refractory particles into the impregnation chamber; injecting a compression fluid into the compacting chamber, to force the slip to pass through the texture; draining the liquid of the slip via the porous material part, while retaining the powder of refractory particles inside the texture so as to obtain a fiber preform filled with refractory particles; drying the fiber preform; unmolding the preform; and sintering the refractory particles present in the preform in order to form a refractory matrix in the preform.
1. A method of fabricating a part out of composite material, the method comprising:
forming a fiber texture from refractory fibers;
placing the fiber texture in a mold having an impregnation chamber including in its bottom portion a part made of porous material on which a first face of said texture rests, the impregnation chamber being closed in its top portion by a deformable impermeable diaphragm placed facing a second face of the fiber texture, said diaphragm separating the impregnation chamber from a compacting chamber;
injecting a slip containing a powder of refractory particles into the impregnation chamber between the second face of the fiber texture and the diaphragm; injecting a compression fluid into the compacting chamber, the fluid exerting pressure on the diaphragm to force the slip to pass through the fiber texture; draining, via the porous material part, the liquid of the slip that has passed through the fiber texture while retaining the powder of refractory particles inside said texture by means of said part of porous material so as to obtain a fiber preform filled with refractory particles;
drying the fiber preform;
unmolding the fiber preform; and
sintering the refractory particles present in the fiber preform in order to form a refractory matrix in said preform.
2. A method according to claim 1 , wherein the porous material part is rigid and presents a shape matching the shape of the composite material part that is to be made.
3. A method according to claim 1 , wherein the porous material part is deformable, and the bottom of the mold presents a shape corresponding to the shape of the composite material part that is to be made, the porous material part taking on the shape of the bottom of the mold.
4. A method according to claim 1 , wherein, during the step of forming the fiber texture, the yarns are woven with a three-dimensional weave.
5. A method according to claim 1 , wherein the fiber texture is made by stacking plies woven using a two-dimensional weave, the texture presenting a thickness of at least 0.5 mm.
6. A method according to claim 1 , wherein the yarns of the preform are formed by fibers made up of one or more of the following materials: alumina, mullite, silica, an aluminosilicate, a borosilicate, silicon carbide, and carbon.
7. A method according to claim 5 , wherein the refractory particles are made of a material selected from: alumina, mullite, silica, an aluminosilicate, an aluminophosphate, zirconia, a carbide, a boride, and a nitride.
8. A method according to claim 1 , wherein the composite material part that is obtained constitutes a turbine engine blade.