| 摘要 |
<p>The present invention provides a sealing arrangement for sealing around a turbine or compressor blade (2). The arrangement includes casing segments (22) having sealing faces (28) for abutting with opposing sealing faces of circumferentially adjacent casing segments along joints between the segments. The sealing faces (28) on adjacent segments are forced into contact with each other by rotation of each casing segment (22) about a mounting pin (34). To reduce radial leakage, a sealing plate (36) is provided. <IMAGE></p> |
