Repair of a coating on a turbine component

Abstract

A method is provided for repairing an area of damaged coating on a component of a turbine module in a gas turbine engine, the component formed of a base material having a diffusion coating applied to the base material. The repair may be accomplished in place by directly heating the area to which a touch-up coating material has been applied with a hot gas plasma without the need to place the component in an oven for curing and heat treatment of the touch-up coating applied to the damaged area.

1 . A turbine vane for a gas turbine engine, the turbine vane formed of a base material having a diffusion coating of an aluminide coating material thereon including an area of damaged aluminide coating repaired by:
 blending the area of damaged aluminide coating with an area of undamaged aluminide coating surrounding the area of damaged aluminide coating by grit blasting;   applying an aluminide touch-up coating material to the blended area; and   curing the aluminide touch-up coating applied to the blended area by heating the aluminide touch-up coating to a first temperature with a hot gas plasma stream generated by a portable microplasma spray coating apparatus.   
     
     
         2 . A turbine vane as recited in  claim 1  further comprising directly heating the blended area to which the aluminide touch-up coating has been applied to a second temperature with the hot gas plasma stream generated by the portable microplasma spray coating apparatus, the second temperature being higher than the first temperature. 
     
     
         3 . A turbine vane as recited in  claim 2  wherein the step of heating the blended area to which the aluminide touch-up coating material has been applied with the hot gas plasma stream generated by the portable microplasma spray coating apparatus comprises the step of heating the blended area to which the aluminide touch-up coating material has been applied with the hot gas plasma stream generated by the portable microplasma spray coating apparatus having a gas nozzle and a powder coating injector, the powder coating injector being deactivated during the heating step. 
     
     
         4 . A turbine vane as recited in  claim 1  further comprising the step of abrading said grit-blasted area with an abrasive device. 
     
     
         5 . A turbine vane as recited in  claim 1  wherein the step of applying an aluminide touch-up coating material to the blended area comprises applying a slurry including the aluminide touch-up coating material to the blended area. 
     
     
         6 . A turbine vane as recited in  claim 1  wherein the step of applying an aluminide touch-up coating material to the blended area comprises applying a tape carrying the aluminide touch-up coating material to the blended area. 
     
     
         7 . A turbine vane as recited in  claim 1  further comprising controlling a temperature of the hot gas plasma stream by adjusting a gas feed rate of the portable microplasma spray coating apparatus.