| 发明名称 |
LOCK LINK MECHANISM FOR TURBINE VANES |
| 摘要 |
A lock link for locking variable stage stator vanes in a compressor includes a substantially planar body portion having a slot formed on one edge and a narrow neck portion extending away from an opposite edge, the narrow neck portion adapted to seat in a corresponding slot in an adjacent lock link attached to an adjacent vane; and a profiled opening in the substantially planar body portion adapted to receive a key provided on a vane stem to prevent relative rotation between the vane and the lock link. |
| 申请公布号 |
US2015098813(A1) |
申请公布日期 |
2015.04.09 |
| 申请号 |
US201314048724 |
申请日期 |
2013.10.08 |
| 申请人 |
General Electric Company |
发明人 |
JARRETT, JR. Harry McFarland;Velampati Jayakrishna;Lammas Andrew John;Cribley Laurie Ann;Deshmukh Saurabh |
| 分类号 |
F01D9/04 |
主分类号 |
F01D9/04 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A lock link for locking variable stage stator vanes in a compressor stator comprising:
a substantially planar body portion having a slot formed on one edge and a narrow neck portion extending away from an opposite edge, said narrow neck portion adapted to seat in a corresponding one of said slots in an adjacent lock link; a profiled opening in said substantially planar body portion; and at least one inwardly projecting load tab. |
| 地址 |
Schenectady NY US |
