Method and device for machining the blade tips of a compressor rotor of a gas turbine
Abstract:
A method and a device for processing blade tips of a mounted compressor rotor of a gas turbine. The compressor rotor includes a blade row with blades to be processed, and a blade row with blades that are not to be processed. The blade row not to be processed is accommodated in a stationary protective housing, which encloses the blade row. The blade row to be processed is processed by a processing machine during a rotation of the compressor rotor.
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