| 摘要 |
A method for repairing a turbine engine component (10) is provided. The method broadly comprises the steps of providing a turbine engine component (10) having an airfoil portion (16), applying a coating (15) to the airfoil portion (16), and restoring a tip portion (18), a chord, and surfaces (17,19) of the airfoil portion (16) to original dimensions in a single operation. A system for repairing the turbine engine component is also described. |
