| 发明名称 |
ADJUSTABLE GUIDE VANE FOR A TURBOMACHINE |
| 摘要 |
The present invention relates to an adjustable guide vane for a turbomachine, having a vane element (1) and a turning disk (2, 3), which has a first impact chamber (4), in which an impulse element (5) is arranged with play of movement. |
| 申请公布号 |
US2016215651(A1) |
申请公布日期 |
2016.07.28 |
| 申请号 |
US201614992279 |
申请日期 |
2016.01.11 |
| 申请人 |
MTU Aero Engines AG |
发明人 |
Hartung Andreas |
| 分类号 |
F01D25/04;F04D29/66;F04D29/56;F01D9/04;F01D17/14 |
主分类号 |
F01D25/04 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An adjustable guide vane for a turbomachine, having a vane element (1) and a turning disk (2, 3), wherein the turning disk has a first impact chamber (4), in which an impulse element (5) is arranged with play of movement. |
| 地址 |
Munich DE |
