| 发明名称 |
TURBINE ENGINE TIP CLEARANCE CONTROL SYSTEM WITH ROCKER ARMS |
| 摘要 |
An assembly is provided for a turbine engine with an axial centerline. This turbine engine assembly includes a blade outer air seal segment, a linkage, a rocker arm and an actuation device. The linkage is attached to the blade outer air seal segment. The rocker arm includes a first arm and a second arm engaged with the linkage. The actuation device is engaged with the first arm. The actuation device is configured to pivot the rocker arm and thereby radially move the blade outer air seal segment. |
| 申请公布号 |
US2016356169(A1) |
申请公布日期 |
2016.12.08 |
| 申请号 |
US201514731140 |
申请日期 |
2015.06.04 |
| 申请人 |
United Technologies Corporation |
发明人 |
Duguay Brian;Davis Timothy M. |
| 分类号 |
F01D11/22 |
主分类号 |
F01D11/22 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An assembly for a turbine engine with an axial centerline, comprising:
a blade outer air seal segment; a linkage attached to the blade outer air seal segment; a rocker arm including a first arm and a second arm engaged with the linkage; and an actuation device engaged with the first arm, the actuation device configured to pivot the rocker arm and thereby radially move the blade outer air seal segment. |
| 地址 |
Hartford CT US |
