| 摘要 |
An exemplary embodiment of the invention is directed to a turbine engine (10) having a circumferential casing (22) with a circumferentially extending slot (28) formed in an inner wall (30). A radially inwardly facing fin-ring (33) is disposed in the slot (28) and has a radially inwardly projecting fin (44) extending axially there across. A radially inwardly extending stator blade (34) has a base (36) and an airfoil (38). The base (36) is disposed in the casing slot (28), radially inwardly of the fin-ring (33). A complementary base slot (46) is disposed in the stator blade base (36) and is configured to receive the fin (44) therein for the transfer of a circumferential force, applied to the stator blade (34), to the fin-ring (33). |
