发明名称 |
Gas turbine stationary blade |
摘要 |
The gas turbine stationary blade comprises a stationary blade section provided therein with a passage for cooling air, an inner shroud for supporting the stationary blade section on the side of a discharge port of the cooling air, and a plurality of segments each of which includes at least one stationary blade section and at least one inner shroud. A flow passage is pulled out from the discharge port of the cooling air, and the flow passage is introduced to a front edge corner section of the inner shroud and is extended rearward along a side edge of the inner shroud.
|
申请公布号 |
US2003012647(A1) |
申请公布日期 |
2003.01.16 |
申请号 |
US20020189413 |
申请日期 |
2002.07.08 |
申请人 |
MITSUBISHI HEAVY INDUSTRIES LTD. |
发明人 |
SHIOZAKI SHIGEHIRO;KUWABARA MASAMITSU;TOMITA YASUOKI |
分类号 |
F01D9/02;F01D5/18;F01D9/04;F01D11/00;(IPC1-7):F01D1/02
/30;(IPC1-7):D06M13/00 |
主分类号 |
F01D9/02 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|