A system (100) and method for inspecting fan blade clearances in a fan casing (210) are presented. The method includes manually installing a bracket (230) that includes a laser module (235) and an inclinometer (236) to a fan rotor (215) that when rotated p...

The gas turbine comprises a turbine and a compressor with a compressor casing (14), whereby the compressor for the cooling of the turbine has a tapping line(16) for the bleed of compressed or partially compressed air. The tapping line has a shut-off device...