| 摘要 |
<p>In one embodiment, a system includes a turbine engine that includes a rotor (42) including multiple blades (40). The turbine engine also includes a shroud (54) disposed about the blades (40). The shroud (54) includes multiple segments (64) engaged with one another via mating teeth (70, 72, 74, 76). The mating teeth (70, 72, 74, 76) are oriented in an axial direction (35) along a longitudinal axis of the turbine engine.</p> |
