发明名称 |
Sealing arrangement between stator blades and rotor of a high pressure turbine |
摘要 |
<p>The high pressure gas turbine has a turbine disk (1) with running paddles (2) and guide paddles (3). A side zone (5) is formed between the turbine disk and a guide paddle rim (4). A seal (8) is formed in the axial direction between the guide paddle platform (6) and the running paddle platform (7) as a labyrinth seal, radially outwards against a main gas channel (9). Alternatively, the seal can use bristles.</p> |
申请公布号 |
EP1471211(A3) |
申请公布日期 |
2006.12.13 |
申请号 |
EP20040008612 |
申请日期 |
2004.04.08 |
申请人 |
ROLLS-ROYCE DEUTSCHLAND LTD & CO KG |
发明人 |
FRIEDL, WINFRIED-HAGEN;AU, JOERG |
分类号 |
F01D11/00;F02C7/28 |
主分类号 |
F01D11/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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