发明名称 Sealing structure for a pivoting blade of a gas turbine
摘要 A sealing structure for a gas turbine blade which pivots about a pivot shaft. A split ring is located in a groove on the shaft, in which the ring can be embedded and held by a bush. When the blade is fitted, the bush abuts against a wall of the stator, slides on the pivot shaft and frees the ring, which expands and forms the seal. The invention relates to gas turbines where the stator blades have a variable setting.
申请公布号 US5324165(A) 申请公布日期 1994.06.28
申请号 US19930058760 申请日期 1993.05.10
申请人 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION "SNECMA" 发明人 CHARBONNEL, JEAN-LOUIS;NAUDET, JACKY S.
分类号 F01D9/02;F01D11/00;F01D17/16;F02C7/28;F04D29/08;F04D29/32;(IPC1-7):F01D17/16 主分类号 F01D9/02
代理机构 代理人
主权项
地址