发明名称 |
High-pressure turbine stator ring for a turbine engine |
摘要 |
The present invention relates to the high-pressure turbine stator ring of a turbo engine that is fastened to the stator by tightening means that limit leaks to a minimum.These means mainly comprise a tightening grip (40) that grips the curved section of a downstream leg (35V) of each spacer section (30) that is fastened to the turbine casing (1) of the stator by a curved downstream flange (23V) of each ring section (20).Application to the fastening of the high-pressure turbine stator ring of a turbo engine.
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申请公布号 |
US6200091(B1) |
申请公布日期 |
2001.03.13 |
申请号 |
US19990330063 |
申请日期 |
1999.06.11 |
申请人 |
SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION "SNECMA" |
发明人 |
BROMANN ALAIN MARC LUCIEN;DE VERDUZAN LéOPOLD JEAN MARIE;MAREY DANIEL JEAN |
分类号 |
F01D11/08;F01D11/18;F01D25/24;(IPC1-7):F01D11/08 |
主分类号 |
F01D11/08 |
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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