| 摘要 |
A turbine engine sealing arrangement includes a blade array rotatable about an axis (X). The blade array has a plurality of blades (50) extending radially from the axis. A control ring (62) is circumferentially disposed about the blade array. A plurality of tiles (70,74,78) are secured relative to the control ring (62) and configured to establish an axially extending seal with one of the blades (50). |
