Turbomachine blade and method for the manufacture of same
A blade of a turbomachine includes a blade body of composite material having a fiber reinforcement having a three-dimensional weave and densified by a matrix, the reinforcement having a first part extended by a second, end, part including two segments separated from each other; and an insert having a pi-shaped section, the insert having a platform part and two longitudinal flanges separated from each other, the platform part including a housing delimited by a bottom wall and a rim, the bottom wall including an opening communicating with the space between the two flanges, the first part of the fiber reinforcement being clamped between the two flanges of the insert, the segments of the second part of the fiber reinforcement being folded against the bottom wall of the housing.
1. Blade of a turbomachine comprising:
a blade body of composite material having a fiber reinforcement having a three-dimensional weave and densified by a matrix, the fiber reinforcement having a longitudinal direction corresponding to the longitudinal direction of the blade and having, in this longitudinal direction, a first part extended by a second, end, part, the second part comprising two segments separated from each other from the junction between the first and second parts to a free end of the fiber reinforcement; and
an insert having a pi-shaped section, the insert having a platform part extending perpendicularly to the longitudinal direction, and two longitudinal flanges separated from each other by a space, the platform part comprising a housing delimited by a bottom wall and a rim, the bottom wall including an opening communicating with the space between the two flanges,
the first part of the fiber reinforcement of the blade body being clamped between the two flanges of the insert, the segments of the second part of the fiber reinforcement being folded on either side of the first part against the bottom wall of the housing of the insert.
2. The blade according to claim 1 , further comprising an insert present between the segments of the second part of the fiber reinforcement at the junction between said segments.
3. The blade according to claim 1 , further comprising at least one mounting hole extending through the insert and a segment of the second part of the fiber reinforcement.
4. The blade according to claim 1 , further comprising a glue film between the fiber reinforcement of the blade body and the insert.
5. The blade according to claim 1 , wherein the fiber reinforcement of the blade body comprises carbon fibers.
6. The blade according to claim 1 , wherein the blade body matrix is an organic matrix or a ceramic matrix.
7. The blade according to claim 1 , wherein the insert is of composite material having matrix-densified fiber reinforcement.
8. The blade according to claim 1 , wherein the insert is of a metallic material.
9. The blade according to claim 8 , further comprising a ply of glass fibers between the fiber reinforcement of the blade body and the insert.
10. The blade according to claim 1 , wherein the insert is present throughout the transverse dimension of the blade body.
11. The blade according to claim 1 , comprising a plurality of inserts on the same end of the blade body.
12. The blade according to claim 1 , constituting an aeronautical outlet guide vane of a turbomachine.
13. Aeronautical turbomachine comprising a blade according to claim 1 .
14. Method of manufacturing a turbine engine blade comprising: a blade body of composite material having a fiber reinforcement densified by a die, the blade body extending in accordance with a longitudinal direction corresponding to the longitudinal direction of the blade; and an insert having a pi-shaped section, the insert having a part of the platform extending perpendicularly to the longitudinal direction, and two longitudinal flanges separated from each other by a space, the platform part comprising a housing delimited by a bottom wall and a rim, the bottom wall comprising an opening communicating with the bottom space between the two flanges, the method comprising:
forming by three-dimensional weaving of a fiber preform intended to form the fiber reinforcement of the blade body of the blade, the preform having a longitudinal direction corresponding to the longitudinal direction of the blade to be produced and having, in this longitudinal direction, a first part extended by a second, end, part, the second part comprising two segments separated from each other from the junction between the first and the second part to a free end of the preform,
inserting the fiber preform in the opening of the insert so that the first part of the preform is sandwiched between the flanges of the insert and that the segments of the second part protrude from the bottom wall of the housing,
folding of each segment of the second part of the fiber preform on either side of the first part to fold against the bottom wall of the housing in order to obtain a blade blank,
placing of the blade blank in the cavity of a mold having the shape of the blade to be produced,
injecting a resin into the cavity of the mold in which the blade blank is present in order to impregnate the blank with resin, and
heat treating the impregnated blank in order to transform the resin and obtain the blade.
15. The method according to claim 14 , further comprising compacting the first and second parts of the fiber preform prior to insertion of the fiber preform into the opening of the insert.