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.
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
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