| 发明名称 |
COOLING PASSAGES FOR INNER CASING OF A TURBINE EXHAUST |
| 摘要 |
An inner casing assembly for a turbine including: an annular inner casing including cooling passages, wherein each passage extends through a wall of the inner casing from a source of cooling fluid to an outer surface of the wall of the inner casing, and struts extending outward from the outer surface of the inner casing wherein the cooling passages are arranged on the inner casing such that a pair of the cooling passages is on opposite sides of each of the struts, and the cooling passages in each pair are equidistant to the corresponding strut. |
| 申请公布号 |
US2015361809(A1) |
申请公布日期 |
2015.12.17 |
| 申请号 |
US201414301507 |
申请日期 |
2014.06.11 |
| 申请人 |
General Electric Co. |
发明人 |
SOUNDIRAMOURTY Sendilkumaran;PAKKALA SRINIVAS |
| 分类号 |
F01D9/06 |
主分类号 |
F01D9/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An inner casing assembly for a turbine comprising:
an annular inner casing including cooling passages, wherein each passage extends through a wall of the inner casing from a source of cooling fluid to an outer surface of the wall of the inner casing, and struts extending outward from the outer surface of the inner casing, wherein the cooling passages are arranged on the inner casing such that a pair of the cooling passages is on opposite sides of each of the struts, and the cooling passages in each pair are equidistant to the corresponding strut. |
| 地址 |
Schenectady NY US |
