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 |
|