| 发明名称 |
TURBOMACHINE BLADE |
| 摘要 |
A blade (1) for a turbomachine, including an impact chamber (2), a single impulse body (3) being situated in the impact chamber, a clearance (S1+S2) between the impulse body and the impact chamber being at least 10 μm and/or at most 1.5 mm in at least one direction. |
| 申请公布号 |
US2014348657(A1) |
申请公布日期 |
2014.11.27 |
| 申请号 |
US201414283985 |
申请日期 |
2014.05.21 |
| 申请人 |
MTU Aero Engines AG |
发明人 |
Stiehler Frank;Hartung Andreas |
| 分类号 |
F01D5/16;B23P15/02 |
主分类号 |
F01D5/16 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A blade for a turbomachine, comprising:
an impact chamber; and a single impulse body situated in the impact chamber, a clearance between the impulse body and the impact chamber being at least 10 μm or at most 1.5 mm in at least one direction. |
| 地址 |
Muenchen DE |
