| 发明名称 |
Sealing component for reducing secondary airflow in a turbine system |
| 摘要 |
A sealing component for reducing secondary airflow in a turbine system includes a first end segment configured to be disposed between, and retained in a radial direction by, a first land on a first rotor disk and a first turbine bucket platform operatively coupled to the first rotor disk. Also included is a second end segment configured to be disposed between, and retained in a radial direction by, a second land on a second rotor disk and a second turbine bucket platform operatively coupled to the second rotor disk. Further included is a main body portion extending axially from the first end segment to the second end segment. |
| 申请公布号 |
US9404376(B2) |
申请公布日期 |
2016.08.02 |
| 申请号 |
US201314064461 |
申请日期 |
2013.10.28 |
| 申请人 |
General Electric Company |
发明人 |
Potter Brian Denver;Liotta Gary Charles |
| 分类号 |
F01D11/00 |
主分类号 |
F01D11/00 |
| 代理机构 |
|
代理人 |
Cusick Ernest G.;Landgraff Frank A. |
| 主权项 |
1. A sealing component for reducing secondary airflow in a turbine system comprising:
a first end segment configured to be disposed between, and retained in a radial direction by, a first land on a first rotor disk and a first turbine bucket platform operatively coupled to the first rotor disk; a second end segment configured to be disposed between, and retained in a radial direction by, a second land on a second rotor disk and a second turbine bucket platform operatively coupled to the second rotor disk.; and a main body portion extending axially from the first end segment to the second end segment. |
| 地址 |
Schenectady NY US |
