Turbine assembly for disk cooling circuit with sealing device for Aviation Turbine

摘要

The invention relates to a turbine assembly for an aircraft turbine, which comprises a disk (...) (...) (...) (...) (...) (...) (...) with rotating blades,A device for holding a blade axially on a disc comprises an axial retaining member (32), a blade axial retaining member (33), a blade axial retaining member (33), a blade axial retaining member (33), a blade axial retaining member (34), and a blade axial retaining member (33, 33)And a sealing device including at least one sealing element (48), the sealing device comprises a first part d ', the first part d' is fastened to the disc (17) and l''''''''''''''''''''''（And a sealing part extending to the side wall by extending to the side wall (33) to connect with the side wall (33)