发明名称 |
Turbine stator vane with root turn purge air hole |
摘要 |
An turbine stator vane for an industrial engine, the vane having a serpentine flow cooling circuit with a first leg located along a leading edge of the vane airfoil and a partition rib separating the first leg from a second leg. A root turn channel connects the first leg to the second leg. A lower end of the partition rib includes a guide vane that directs cooling air from an aft section of the first leg toward a bleed hole for purging an ISSH. A plurality of turning guide ribs located in the aft section of the first leg also directs the cooling air toward the bleed hole. |
申请公布号 |
US8864468(B1) |
申请公布日期 |
2014.10.21 |
申请号 |
US201213458322 |
申请日期 |
2012.04.27 |
申请人 |
Florida Turbine Technologies, Inc. |
发明人 |
Liang George |
分类号 |
F01D5/18 |
主分类号 |
F01D5/18 |
代理机构 |
|
代理人 |
Ryznic John |
主权项 |
1. An air cooled industrial turbine stator vane comprising:
a leading edge region and a trailing edge region; a serpentine flow cooling circuit with a first leg located along the leading edge region of the vane; a partition rib separating the first leg from a second leg of the serpentine flow cooling circuit; a root turn channel connecting the first leg to the second leg of the serpentine flow cooling circuit; a bleed hole located near to a junction between the first leg and the root turn channel that opens into an inter-stage seal housing; and, a lower end of the partition rib having a curvature to direct cooling air from an aft section of the first leg toward the bleed hole. |
地址 |
Jupiter FL US |