| 发明名称 |
ROTOR ARRANGEMENT FOR A TURBOMACHINE AND COMPRESSOR |
| 摘要 |
The present invention relates to a rotor arrangement (100) for a turbomachine, having a rotor with a first rotor stage (1), a shaft (3), and a first hub (5) for joining the first rotor stage (1) to the shaft (3). The first hub (5) has a balancing device (30) for balancing the first rotor stage (1). In addition, the present invention relates to a compressor. |
| 申请公布号 |
US2016326877(A1) |
申请公布日期 |
2016.11.10 |
| 申请号 |
US201615133406 |
申请日期 |
2016.04.20 |
| 申请人 |
MTU Aero Engines AG |
发明人 |
Boewing Stefan |
| 分类号 |
F01D5/02;F01D25/00;F04D29/32;F01D5/06;F01D5/34;F04D29/70 |
主分类号 |
F01D5/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A rotor arrangement (100) for a turbomachine, comprising:
a rotor with a first rotor stage (1), a shaft (3), and a first hub (5) for joining the first rotor stage (1) to the shaft (3), wherein the first hub (5) has a balancing device (30) for balancing the first rotor stage (1). |
| 地址 |
Munich DE |
