| 摘要 |
Systems and methods for providing localized heat treatment of gas turbine components (200) are provided. In this regard, an exemplary method includes: identifying an area of a gas turbine component (200) to which localized heat treatment is to be performed; positioning a resistance heating element (100), sized and shaped to transfer heat to the area, adjacent the area; electrically coupling a current-limiting power controller to the resistance heating element (100), and locally heating the area using the resistance heating lement (100), with power being provided to the resistance heating element via the current-limiting power controller. |
