发明名称 |
Gas turbine |
摘要 |
The turbine has a combustion chamber (10) with inner and outer walls (12, 13) comprising respective downstream end parts (12a, 13a). The end parts are arranged against respective inner and outer platforms of vanes (21) of a high pressure turbine nozzle (20). Connection screws (25,27) are radially installed in vanes by passing through holes formed in the end parts, where the screws connect the nozzle to the end parts. |
申请公布号 |
EP1607682(B1) |
申请公布日期 |
2016.06.08 |
申请号 |
EP20050291174 |
申请日期 |
2005.06.01 |
申请人 |
SNECMA |
发明人 |
AUMONT, CAROLINE;CONETE, ERIC;DE SOUSA, MARIO CÉSAR;HERNANDEZ, DIDIER HIPPOLYTE |
分类号 |
F01D9/02;F01D9/04;F23R3/60 |
主分类号 |
F01D9/02 |
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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