发明名称 |
TURBINE BLADE HAVING A CONSTANT THICKNESS AIRFOIL SKIN |
摘要 |
A turbine blade is provided for a gas turbine comprising: a support structure comprising a base defining a root of the blade and a framework extending radially outwardly from the base, and an outer skin coupled to the support structure framework. The skin has a generally constant thickness along substantially the entire radial extent thereof. The framework and the skin define an airfoil of the blade. |
申请公布号 |
WO2011019412(A2) |
申请公布日期 |
2011.02.17 |
申请号 |
WO2010US24350 |
申请日期 |
2010.02.17 |
申请人 |
SIEMENS ENERGY, INC.;MARRA, JOHN, J. |
发明人 |
MARRA, JOHN, J. |
分类号 |
F01D5/18;F01D5/14;F01D5/30 |
主分类号 |
F01D5/18 |
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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