| 摘要 |
The invention relates to a method of repairing moving blades of a gas turbine, with at least the following steps: a) preparation of a moving blade to be repaired; b) removal of at least one damaged section of a damaged blade tip of the moving blade to be repaired, forming a parting surface; c) successive building up of the, or each, removed section or the entire blade tip on the parting surface of the moving blade by means of a rapid manufacturing process, using three-dimensional CAD structural data on the moving blade. |
