| 摘要 |
A turbine shroud segment (136, 236, 336, 36) of a turbine shroud (124, 224, 24, 324) for use in a turbine (16) of a gas turbine engine (10) is disclosed herein. The turbine shroud segment (136, 236, 336, 36) includes a carrier segment (138, 38) and a blade track segment (140, 240, 340, 40). The carrier segment (138, 38) includes metallic materials. The blade track segment (140, 240, 340, 40) includes ceramic matrix composite materials. A seal is arranged between the carrier segment (138, 38) and the blade track segment (140, 240, 340, 40). |
