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> |