| 发明名称 |
Turbine blade with platform cooling |
| 摘要 |
A cooled turbine blade for a gas turbine engine having a platform cooling supply channel that supplies cooling air to a plurality of cooling holes in the surface of the blade platform adjacent the trailing edge of the blade.
|
| 申请公布号 |
US6210111(B1) |
申请公布日期 |
2001.04.03 |
| 申请号 |
US19980217144 |
申请日期 |
1998.12.21 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
LIANG GEORGE P. |
| 分类号 |
F01D5/12;F01D5/18;(IPC1-7):F01D5/18 |
主分类号 |
F01D5/12 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
|
| 地址 |
|
