| 摘要 |
Shrouds (102) and shroud assemblies (100) for gas turbine engines are provided. A shroud includes a shroud body (110). The shroud body includes a forward surface, a rear surface axially spaced from the forward surface, an inner surface extending between the forward surface and the rear surface, and an outer surface extending between the forward surface and the rear surface and radially spaced from the inner surface. The shroud further includes a flange (120) extending from the shroud body, and a bore hole (130) defined in the flange. The bore hole (130) extends generally circumferentially through the flange between a first opening (132) and a second opening (134). |
