| 摘要 |
The invention relates to a device (1) for recontouring a gas turbine blade (2), comprising at least one support (6a, 6b) that is arranged to rest on an edge (3a) of the gas turbine blade (2) during the recontouring, at least one lateral bearing (5a, 5b) that is arranged to bear on the intake and/or pressure side (3b, 3c) of the gas turbine (2) in a lateral direction (7) during the recontouring, and a machining unit (4) by means of which the machining of the gas turbine blade (2) takes place by cutting in a machining direction (8) along the edge (3a), wherein the machining unit (4) is movable in a direction perpendicular to the machining direction (8). |
