Repair process using plasma etching
A repair process includes providing a gas turbine engine article that has an elastomeric coating that has an eroded region, plasma etching the elastomeric coating in the eroded region, and applying an elastomeric repair coating on the eroded region.
1. A repair process comprising:
providing a gas turbine engine article that includes an aluminum alloy substrate and an elastomeric coating disposed on the aluminum alloy substrate, and the elastomeric coating has an eroded region;
plasma etching the elastomeric coating in the eroded region, the plasma etching partially removing a surface portion of the elastomeric coating to create a new bonding surface on the elastomeric coating without removal of the elastomeric coating down to the aluminum alloy substrate; and
applying an elastomeric repair coating on the new bonding surface.
2. The repair process as recited in claim 1 , wherein the gas turbine engine article is a fan blade.
3. The repair process as recited in claim 1 , wherein the elastomeric coating is selected from the group consisting of silicone, urethane, fluoroelastomer, and combinations thereof.
4. The repair process as recited in claim 1 , wherein the plasma etching is conducted under an air, oxygen or argon plasma.
5. The repair process as recited in claim 4 , wherein the plasma etching is conducted for a time from 5 minutes to 60 minutes.
6. The repair process as recited in claim 1 , wherein the plasma etching is conducted for a time from 20 minutes to 60 minutes.
7. The repair process as recited in claim 1 , wherein the elastomeric repair coating on the eroded region is flush with the elastomeric coating adjacent the eroded region.
8. The repair process as recited in claim 1 , wherein the elastomeric repair coating has an interfacial tensile strength with respect to the bonding surface of 1500 pounds per square inch (psi) up to approximately 3400 psi.