SHROUD FOR ROTATING BLADES OF A TURBO MACHINE, AND TURBO MACHINE
The invention relates to a shroud for rotating blades of a turbo machine, in particular a gas turbine. Said shroud (10) is arranged along the circumference of a row of several rotating blades (14, 50) disposed on a rotor (12) and has at least one separation gap (16, 16′, 16″) along the circumference...
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