| 摘要 |
A sealing element (22) for a gas turbine (1), which is provided with at least one rotor ring (2) and at least a plurality of rotor blades (3) radially arranged about the rotor ring (2) and having an end portion (7) fixed to the rotor ring (2), is provided with a wall (23), which is adapted to be coupled to the rotor ring (2) and to at least one rotor blade (3), has an external face (24) adapted to be arranged in contact with a hot working fluid in the gas turbine (1) and an internal face (25) adapted to be arranged in contact with a cooling fluid of the gas turbine (1), and a gap (29), which is adapted to be travelled through by the cooling fluid. |
