| 摘要 |
The turbine ring (1) has one-piece ring structure, which is provided with an outer ring (2) having a mounting portion (10) for fixing the turbine ring to a casing portion of a turbomachine. An inner ring (4), which is segmented in the circumferential direction, is provided with multiple inner ring segments (16a,16b) for hot gas guidance, where the inner ring segments are mutually displaced in the circumferential direction. Front sealing segments and rear sealing segments (8a,8b) are spaced apart in the axial direction and extend radially between the inner ring and the outer ring. |
