| 摘要 |
<p>A method for repairing a gas turbine component (10) comprises the steps of: €¢ identifying on said gas turbine component (10) a worn out location, where said gas turbine component (10) is damaged; €¢ removing said damaged location, thereby creating a missing zone (18); €¢ manufacturing an insert, which fits into said missing zone (18); €¢ putting said insert into said missing zone (18); €¢ adjusting said insert in said gas turbine component (10); and €¢ joining said adjusted insert to said gas turbine component (10).</p> |
