| 摘要 |
In one embodiment, a system includes a turbine engine (10) that includes a turbine stage including a turbine rotor (42) having multiple blades (40) disposed in a first annular arrangement. The turbine engine (10) also includes multiple cover plates (54) disposed in a second annular arrangement along interfaces between the turbine rotor (42) and the blades (40). The turbine engine (10) further includes multiple lugs (60) coupled to the turbine stage and a first ring (74) coupled to the lugs (60) to hold the cover plates (54) to the turbine stage. |
