发明名称 |
Gas Turbine |
摘要 |
The gas turbine comprises a compressor, a combustion chamber (2), a guide vane row (3) and a rotor airfoil row. The guide vane row (3) comprises a plurality of guide vane airfoils comprising a blade (7) and an inner platform (8). The ratio between the pitch (P) and the leading edge diameter (D) of the guide vane airfoils is between 6.3-7.6 and the ratio between the platform length (L) and the leading edge diameter (D) of the guide vane airfoils is between 4.0-5.5.
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申请公布号 |
EP2299057(A1) |
申请公布日期 |
2011.03.23 |
申请号 |
EP20090169493 |
申请日期 |
2009.09.04 |
申请人 |
ALSTOM TECHNOLOGY LTD |
发明人 |
STEPHAN, BRUNO;KRUECKELS, JOERG;SOMMER, THOMAS |
分类号 |
F01D5/14;F01D9/02;F01D9/04 |
主分类号 |
F01D5/14 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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