Metal structural reinforcement for a composite turbine engine blade

1. A structural reinforcement for a composite blade of a turbine engine, the reinforcement being for adhesively bonding to a leading edge of said blade and presenting over its full height a section that is substantially V-shaped, having a base that is extended by two lateral flanks, said base comprising at least one housing extending along a longitudinal direction of said structural reinforcement, the reinforcement including, mounted in said at least one housing, an assembly of a plurality of bundles of fibers defining fiber content that varies along the full height of said housing.

2. The structural reinforcement according to claim 1 , wherein the fibers making up the fiber bundles are held in position by rings arranged at least at each end of said fiber bundles.

3. The structural reinforcement according to claim 2 , wherein said rings present diameters that increase with increasing number of fiber bundles that they serve to hold together.

4. The structural reinforcement according to claim 1 , wherein it is made up of two portions for welding together, said at least one housing for receiving said fiber bundles being formed by joining together two mutually-facing grooves that are formed in respective ones of said two portions, the grooves being joined together during welding.

5. The structural reinforcement according to claim 4 , wherein said housing includes a diameter that varies in successive stages to match the diameter of the fiber bundle it receives.

6. The structural reinforcement according to claim 1 , wherein said assembly of a plurality of fiber bundles includes at least two concentric fiber bundles, a tubular bundle having a first length and an annular bundle covering part of the first fiber bundle and having a second length that is shorter than said first length, so as to define a first fiber content over an overlap length of the first and second fiber bundles, and a second fiber content over a remaining length.

7. The structural reinforcement according to claim 6 , wherein said overlap length is formed by said second length and said remaining length is formed by said first length minus said second length.

8. The structural reinforcement according to claim 6 , wherein said assembly of fiber bundles comprises four concentric fiber bundles, an annular fourth fiber bundle having a fourth length covering a portion of an annular third fiber bundle having a third length, itself covering a portion of said second fiber bundle having a second length, so as to define third and fourth fiber contents along the overlap lengths of the third and fourth fiber bundles, respectively.

9. The structural reinforcement according to claim 1 , wherein said housing forms a closed space.

10. A turbine engine blade including structural reinforcement according to claim 1 .

11. A turbine engine including at least one blade according to claim 10 .