Patent ID: 6962484

Claim:
A moving blade, cast in one piece, for a turbomachine, comprising: an aerodynamically shaped profile body having a radially outer end including an integrally molded shroud band which projects beyond the profile body in the circumferential direction and which has radially on the outside an integrally molded fin which extends in a circumferential direction along the shroud band and which, at least in a region of the shroud band in which the profile body runs, has a base portion connected to the shroud band, a transitional portion adjoining the base portion radially, circumferentially, or both, and a sealing portion adjoining the transitional portion radially, circumferentially, or both; an axially measured wall thickness decreasing in the transitional portion from the base portion to the sealing portion; and at least one depression which reduces the wall thickness of the base portion integrally molded on the outside of the base portion.