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 CA2276238(A1) 申请公布日期 1999.12.25
申请号 CA19992276238 申请日期 1999.06.23
申请人 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION "SNEC MA" 发明人 BROMANN, ALAIN MARC LUCIEN;DE VERDUZAN, LEOPOLD JEAN MARIE;MAREY, DANIEL JEAN
分类号 F01D11/08;F01D11/18;F01D25/24;(IPC1-7):F01D9/04 主分类号 F01D11/08
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