Method for manufacturing a turbine engine part by injection of resin under pressure
View Patent ↗A method for manufacturing a thick turbine engine part in a composite material by injection of resin under pressure. A fiber preform is positioned in a mold, a resin composition is injected into the mold, the resin composition is polymerized in the mold so as to obtain the part, and the part is removed from the mold. Prior to the injection of the resin composition, a mold release shim is inserted between the fibrous preform and a wall of the mold, and between the polymerization of the resin composition and the removal of the part from the mold, the mold release shim is extracted.
1. A method for manufacturing a thick turbine engine part in a composite material by injection of resin under pressure, comprising the following steps:
positioning a fiber preform in a mold,
injecting a resin composition into the mold,
polymerizing the resin composition in the mold so as to obtain the part, and
removing the part from the mold, wherein the method further comprises:
prior to the injection of the resin composition, inserting a mold release shim between the fiber preform and a wall of the mold, said mold resin shim having two opposite faces converging towards a second face adapted for being positioned at the bottom of the mold, so as to form with the wall a non-zero draft angle, and
between the polymerization of the resin composition and the removal of the part from the mold, extracting the mold release shim,
wherein the wall of the mold comprises a channel for injecting the resin composition into the mold,
wherein the mold release shim comprises at least one face having at least one guiding groove for guiding the injection resin composition, in order to facilitate circumvention of the mold release shim by the resin composition during the injection step, and
wherein the at least one face having the at least one guiding groove is positioned in front of the injection channel.
2. The manufacturing method according to claim 1 , wherein the at least one guiding groove is flared towards a second face of the mold release shim adapted so as to be placed at a bottom of the mold.
3. The manufacturing method according to claim 1 wherein a guiding groove is also positioned on the mold release shim face in front of the part, and a surface area of the guiding groove of the face in front of the part covers between 30% and 60% of a total surface area of said face.
4. The manufacturing method according to claim 1 , wherein the draft angle is comprised between 7° and 20°.
5. A method for manufacturing a thick turbine engine part in a composite material by injection of resin under pressure, comprising the following steps:
positioning a fiber preform in a mold,
injecting a resin composition into the mold,
polymerizing the resin composition in the mold so as to obtain the part, and
removing the part from the mold,
wherein the method further comprises:
prior to the injection of the resin composition, inserting a mold release shim between the fiber preform and a wall of the mold, said mold resin shim having two opposite faces converging towards a second face adapted for being positioned at the bottom of the mold, so as to form with the wall a non-zero draft angle, and
between the polymerization of the resin composition and the removal of the part from the mold, extracting the mold release shim,
wherein the wall of the mold comprises a channel for injecting the resin composition into the mold,
wherein the mold release shim comprises at least one face having at least one guiding groove for guiding the injection resin composition, in order to facilitate circumvention of the mold release shim by the resin composition during the injection step, and
wherein the at least one guiding groove is flared towards a second face of the mold release shim adapted so as to be placed at a bottom of the mold.
6. The manufacturing method according to claim 5 , wherein the at least one face having the at least one guiding groove is positioned in front of at least one of the injection channel and the part.
7. The manufacturing method according to claim 5 , wherein the draft angle is comprised between 7° and 20°.