| 发明名称 |
COOLING STRUCTURE FOR A GAS TURBINE |
| 摘要 |
In a cooling structure for a gas turbine, cooling air diffusion holes are formed from inner surface to outer surface of a platform so as to open from high pressure side blade surface of a moving blade offset in a direction toward low pressure side blade surface of adjacent moving blade confronting the high pressure side blade surface, in a direction of primary flow.
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| 申请公布号 |
CA2366726(A1) |
申请公布日期 |
2002.07.09 |
| 申请号 |
CA20022366726 |
申请日期 |
2002.01.08 |
| 申请人 |
MITSUBISHI HEAVY INDUSTRIES, LTD. |
发明人 |
TORII, SHUNSUKE;KUWABARA, MASAMITSU;TOMITA, YASUOKI;KUBOTA, JUN;AOKI, HIROYUKI |
| 分类号 |
F01D5/18;F01D9/02;F01D25/12;(IPC1-7):F01D25/12 |
主分类号 |
F01D5/18 |
| 代理机构 |
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