Abstract: With a method for finish-machining the blade tips of rotor wheels made in BLISK design, the rotor wheel or multi-stage compressor rotor (1), is machined—blade by blade and stage by stage—at the blade tips (2) by a conical cutter (5) whose cutting edge (6) is oriented tangentially to the outside surface of the rotor wheel/compressor rotor and routed on the blade tip essentially along the centerline thereof, with the cutting force being introduced perpendicular to the tool axis and in the stiffest direction of the blade (3), i.e. the centerline (11) of the blade cross-section and the perpendicular axis extending from the centerline. The cutting action and the force introduction of the conical cutter at the blade tip allow production of blade tips with a geometrically precisely defined edge without setting the respective blades into vibration.

Abstract: An arrangement for the repair of BLISK blades damaged at their leading and trailing edges by use of laser deposition welding, includes a laser source and laser optics for generating a focused laser beam (26) and a powder line (35) connected to a powder reservoir for supplying metal powder to be melted by the laser beam to the weld area. A modular, tubularly elongated welding apparatus (7) with a connection module (13) which is connected to a laser source and in which the entering laser beam is deflected in longitudinal direction and parallelized, and to the one side of the connection module (13) is connected to a camera module for a CCD camera (12) enabling the precise positioning of the welding apparatus and the deposition of the molten metal powder on the respective blade to be monitored and controlled.

Abstract: A method and an apparatus for repairing gas-turbine blisks uses an endoscope 15 provided with processing optics featuring a flexible light guide arrangement 16. A laser source 9 is connected to a flexible optical fiber arrangement 10, with a filler material feeder 7 for supplying welding flux via a flexible line 8, with a water supply 11 connected to a flexible line 12, and with an inert gas supply 13 connected to a flexible line 16 for supplying inert gas, with the flexible lines 8, 12, 14, the flexible light guide arrangement 16 and the flexible optical fiber arrangement 10 being combined to form a flexible long repair implement 17 at least at its distal end areas.

Abstract: With a method for finish-machining the blade tips of rotor wheels made in BLISK design, the rotor wheel or multi-stage compressor rotor (1), is machined—blade by blade and stage by stage—at the blade tips (2) by a conical cutter (5) whose cutting edge (6) is oriented tangentially to the outside surface of the rotor wheel/compressor rotor and routed on the blade tip essentially along the centerline thereof, with the cutting force being introduced vertically to the tool axis and in the stiffest direction of the blade (3), i.e. the centerline (11) of the blade cross-section and the vertical axis extending from the centerline. The cutting action and the force introduction of the conical cutter at the blade tip allow production of blade tips with a geometrically precisely defined edge without setting the respective blades into vibration.

Abstract: An arrangement for the repair of BLISK blades damaged at their leading and trailing edges by use of laser deposition welding, includes a laser source and laser optics for generating a focused laser beam (26) and a powder line (35) connected to a powder reservoir for supplying metal powder to be melted by the laser beam to the weld area. A modular, tubularly elongated welding apparatus (7) with a connection module (13) which is connected to a laser source and in which the entering laser beam is deflected in longitudinal direction and parallelized, and to the one side of the connection module (13) is connected to a camera module for a CCD camera (12) enabling the precise positioning of the welding apparatus and the deposition of the molten metal powder on the respective blade to be monitored and controlled.

Abstract: A method and an apparatus for repairing gas-turbine blisks uses an endoscope 15 provided with processing optics featuring a flexible light guide arrangement 16. A laser source 9 is connected to a flexible optical fiber arrangement 10, with a filler material feeder 7 for supplying welding flux via a flexible line 8, with a water supply 11 connected to a flexible line 12, and with an inert gas supply 13 connected to a flexible line 16 for supplying inert gas, with the flexible lines 8, 12, 14, the flexible light guide arrangement 16 and the flexible optical fiber arrangement 10 being combined to form a flexible long repair implement 17 at least at its distal end areas.