Process for preparing a substrate for thermal spraying of a metal coating
View Patent ↗A method of preparing a substrate to receive a metal coating deposited by thermal spraying, the method including the following steps: a) depositing a layer of adhesive on the zone to be coated, the layer having a uniform thickness greater than 10 μm and less than 100 μm; b) before the adhesive dries, cold spraying a metal powder onto the zone to be coated, so that powder particles become embedded at least in part in the layer of adhesive; and c) drying the adhesive in which the powder particles remain held captive, thereby forming an undercoat suitable for receiving a metal coating deposited by thermal spraying. The method is applicable to protecting the leading edges of fan blades.
1. A preparation method for preparing a zone of a substrate to be coated, the method comprising:
a) depositing a layer of adhesive on the zone of the substrate to be coated, the layer having a uniform thickness greater than 10 μm and less than 100 μm;
b) after depositing the layer of adhesive but before the adhesive cures, cold spraying metal powder particles onto the layer of adhesive on the zone of the substrate to be coated, so that the metal powder particles become partially embedded in said layer of adhesive; and
c) curing the layer of adhesive in which said powder particles are partially embedded, thereby forming an undercoat;
wherein the substrate with the layer of adhesive deposited thereon is subjected to motion to counter adhesive creeping over the zone of the substrate to be coated, said motion being continued during b) and c), and
wherein at the end of b), more than 70% and less than 95% of a surface area of the zone of the substrate to be coated is covered in the metal powder particles.
2. A method according to claim 1 , wherein the layer of adhesive has a thickness greater than 10 μm and less than 50 μm.
3. A method according to claim 1 , wherein said layer of adhesive has a thickness less than a mean diameter d 50 of the metal powder particles.
4. A method according to claim 1 , wherein said layer of adhesive is formed by an epoxy adhesive comprising a resin and a curing agent.
5. A method according to claim 1 , wherein prior to a), a roughness of the surface of the substrate in the zone to be coated is made uniform.
6. A method according to claim 1 , further comprising subjecting the undercoat to finishing by removing non-glued metal powder particles.
7. A method according to claim 1 , further comprising depositing a metal coating on the undercoat by thermal spraying, thereby forming a metal protective layer on the zone of substrate to be coated.
8. A method according to claim 1 , wherein the substrate is made of an organic matrix composite.
9. A method according to claim 8 , wherein the organic matrix composite comprises carbon fibers and resin.
10. A method according to claim 9 , wherein the substrate is an airfoil and the zone of the substrate to be coated is a leading edge of the airfoil.
11. A method according to claim 10 , wherein:
said layer of adhesive has a thickness that is 30%-95% of a mean diameter d 50 of the metal powder particles;
at the end of b), more than 70% and less than 95% of a surface area of the leading edge of the airfoil is covered in the metal powder particles; and
the metal powder particles have a particle sphericity factor that is less than 0.75, and a form factor of 1.5 to 3.
12. A method according to claim 11 , wherein:
said layer of adhesive has a thickness that is 40%-80% of a mean diameter d 50 of the metal powder particles; and
the metal powder particles have a particle sphericity factor that is less than 0.60, and a form factor of 1.8 to 2.
13. A method according to claim 12 , further comprising depositing a metal coating on the undercoat by thermal spraying, thereby forming a metal protective layer on the zone of substrate to be coated.
14. A method according to claim 11 , further comprising depositing a metal coating on the undercoat by thermal spraying, thereby forming a metal protective layer on the zone of substrate to be coated.
15. A method according to claim 8 , further comprising depositing a metal coating on the undercoat by thermal spraying, thereby forming a metal protective layer on the zone of substrate to be coated.
16. A method according to claim 1 , wherein the zone of the substrate to be coated is a leading edge of an airfoil.
17. A method according to claim 1 , wherein:
said layer of adhesive has a thickness that is 30%-95% of a mean diameter d 50 of the metal powder particles;
at the end of b), more than 70% and less than 95% of a surface area of the zone of the substrate to be coated is covered in the metal powder particles; and
the metal powder particles have a particle sphericity factor that is less than 0.75, and a form factor of 1.5 to 3.