发明名称 |
Turbine rotor cooling flow system |
摘要 |
Disclosed herein is an apparatus comprising a disk coverplate for a turbine rotor, the disk coverplate comprising a plurality of cooling holes, wherein the distance between the centers of any two adjacent cooling holes is greater than twice the average diameter of the two adjacent cooling holes. A method to control turbine cooling air flow is also disclosed. |
申请公布号 |
US8277169(B2) |
申请公布日期 |
2012.10.02 |
申请号 |
US20050155399 |
申请日期 |
2005.06.16 |
申请人 |
RIAHI ARDESHIR;BORNS FREDERICK G.;AGARWAL VIVEK;HONEYWELL INTERNATIONAL INC. |
发明人 |
RIAHI ARDESHIR;BORNS FREDERICK G.;AGARWAL VIVEK |
分类号 |
F01D5/08 |
主分类号 |
F01D5/08 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|