| 发明名称 |
TURBINE BUCKET AND METHOD FOR BALANCING A TIP SHROUD OF A TURBINE BUCKET |
| 摘要 |
The present application and the resultant patent provide a turbine bucket for a gas turbine engine. The turbine bucket may include an airfoil, a tip shroud positioned radially outward from the airfoil, and a seal rail positioned radially outward from the tip shroud and extending in a generally tangential direction from a first end to a second end of the tip shroud. The seal rail may include a maximum axial thickness at a location positioned between the first end and the second end and offset from the airfoil in the generally tangential direction. The present application and the resultant patent further provide a gas turbine engine and a method for balancing a tip shroud of a turbine bucket of a gas turbine engine. |
| 申请公布号 |
US2015233258(A1) |
申请公布日期 |
2015.08.20 |
| 申请号 |
US201414185161 |
申请日期 |
2014.02.20 |
| 申请人 |
General Electric Company |
发明人 |
Kareff Spencer Aaron;Piersall Matthew Robert;Werner Danielle |
| 分类号 |
F01D5/30 |
主分类号 |
F01D5/30 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A turbine bucket for a gas turbine engine, the turbine bucket comprising:
an airfoil; a tip shroud positioned radially outward from the airfoil; and a seal rail positioned radially outward from the tip shroud and extending in a generally tangential direction from a first end to a second end of the tip shroud, wherein the seal rail comprises a maximum axial thickness at a location positioned between the first end and the second end and offset from the airfoil in the generally tangential direction. |
| 地址 |
Schenectady NY US |
