Process for manufacturing a multiperforated composite part
A method of fabricating a multi-perforated part out of composite material includes positioning a sand-blasting mask on a preform including a fiber texture impregnated with a polymerized ceramic-precursor resin, the mask having a plurality of openings corresponding to the perforations to be made in the preform; projecting abrasive particles at high speed against the surface of the mask so as to perforate the preform exposed in the openings of the mask; and pyrolyzing the multi-perforated preform so as to form a ceramic matrix in the multi-perforated fiber texture.
1. A method of fabricating a multi-perforated part out of composite material, the method comprising the following steps:
positioning a sand-blasting mask on a preform comprising a fiber texture impregnated with a polymerized ceramic-precursor resin, said sand-blasting mask having a plurality of openings corresponding to perforations to be made in the preform;
projecting abrasive particles at high speed against the surface of the sand-blasting mask so as to perforate the preform exposed in said openings of said sand-blasting mask; and
pyrolyzing the multi-perforated preform so as to form a ceramic matrix in the multi-perforated fiber texture.
2. A method according to claim 1 , wherein after heat treatment of the pyrolyzing step the method includes a step of densifying the multi-perforated preform, performed by chemical vapor infiltration of silicon carbide.
3. A method according to claim 1 , wherein the abrasive particles are grains of silicon carbide of angular shape with sharp edges.
4. A method according to claim 1 , wherein the abrasive particles are projected against the surface of the sand-blasting mask at an angle lying in the range 45° to 60°.
5. A method of fabricating a multi-perforated part out of composite material, the method comprising the following steps:
placing a sand-blasting mask on a preform comprising a fiber texture containing refractory oxide particles, said sand-blasting mask including a plurality of openings corresponding to perforations to be made in the preform;
projecting abrasive particles at high speed against the surface of the sand-blasting mask so as to perforate the preform exposed in the openings of said sand-blasting mask; and
sintering the refractory oxide particles so as to form a refractory oxide matrix in the multi-perforated preform.
6. A method according to claim 5 , wherein after heat treatment of the sintering step the method includes a step of densifying the multi-perforated preform, performed by chemical vapor infiltration of silicon carbide.
7. A method according to claim 5 , wherein the abrasive particles are grains of white corundum or of silicon carbide of angular shape with sharp edges.
8. A method according to claim 5 , wherein the abrasive particles are projected against the surface of the sand-blasting mask at an angle lying in the range 45° to 60°.