| 发明名称 |
Gas turbine |
| 摘要 |
An outer shape of a section in the longitudinal direction at a leading edge of the strut is an aerofoil whose thickness is gradually increased along a flow direction of the combustion gas to prevent reduction of turbine efficiency caused by a shock wave generated at the strut of the exhaust diffuser.
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| 申请公布号 |
US7410343(B2) |
申请公布日期 |
2008.08.12 |
| 申请号 |
US20050196388 |
申请日期 |
2005.08.04 |
| 申请人 |
MITSUBISHI HEAVY INDUSTRIES, LTD. |
发明人 |
WAKAZONO SUSUMU;ISHIZAKA KOUICHI;YURI MASANORI;TAKAHASHI RONALD |
| 分类号 |
F01D25/30;F04D29/04;F01D25/16;F02C7/20 |
主分类号 |
F01D25/30 |
| 代理机构 |
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代理人 |
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