Process for the vapor phase aluminization of a turbomachine metal part and donor liner and turbomachine vane comprising such a liner
View Patent ↗An aluminization process by vapor phase deposition for high-temperature oxidation protection of a metal turbomachine part. The part including a cavity into which a metal component is introduced and assembled from an opening in the part. A halide is formed by reaction between a halogen and a metal donor containing aluminum, then the halide is transported by a carrier gas in order to come into contact with the metal part, wherein the metal component has first, before the implementation of the process, been surface-enriched with aluminum in order to serve as an aluminum donor.
1. An aluminization process by vapor phase deposition for high-temperature oxidation protection of a metal turbomachine part, the process comprising:
introducing a nozzle guide vane including a hollow blade provided between a first platform and a second platform, a cavity of the hollow blade communicating with a first opening provided in the first platform and with a second opening provided in the second platform;
surface-enriching a perforated liner of substantially cylindrical shape with aluminum in order to serve as an aluminum donor;
inserting the liner inside the cavity of the hollow blade through the first opening;
attaching an upper edge of the liner to an upper edge of the cavity of the hollow blade while leaving a lower edge of the liner free;
forming a halide by reaction between a halogen and the liner containing aluminum; and
transporting the halide by a carrier gas in order to come into contact with said guide vane so as to aluminize surfaces of the cavity of the hollow blade.
2. The process as claimed in claim 1 , wherein the liner is coated with a layer formed by metal deposition.
3. The process as claimed in claim 2 , wherein the metal deposition onto the liner has been carried out by one of the following methods:
SVPA, CVD, PVD, aluminization by pack cementation, thermal spraying, electrodeposition or immersion in a bath.
4. The process as claimed in claim 2 , wherein the layer has a thickness between 10 μm and 150 μm.
5. The process as claimed in claim 4 , wherein the layer has a thickness between 20 and 90 μm.
6. The process as claimed in claim 2 , wherein the layer contains at least 15 wt % of aluminum.
7. The process as claimed in claim 6 , wherein the layer further comprises at least one element selected from Cr, Hf, Y, Zr, Si, Ti, Ta, Pt, Pd, or Ir.
8. The process as claimed in claim 1 , wherein the upper edge of the liner is welded or brazed to the upper edge of the cavity of the hollow blade.
9. The process as claimed in claim 1 , wherein the nozzle guide vane is formed by casting.