发明名称 |
TURBINE BLADE FOR A GAS TURBINE ENGINE |
摘要 |
A turbine blade for a gas turbine engine may include a platform, an airfoil extending above the platform, and a root structure extending below the platform. The root structure may extend from a forward face to an aft face and include a shank region proximate the platform and a lower portion distal to the platform. The forward face of the shank region may project outward from the forward face of the lower portion. |
申请公布号 |
US2014119917(A1) |
申请公布日期 |
2014.05.01 |
申请号 |
US201213665536 |
申请日期 |
2012.10.31 |
申请人 |
SOLAR TURBINES INCORPORATED;SOLAR TURBINES INCORPORATED |
发明人 |
TARCZY JEFFREY EUGENE;FAULDER LESLIE JOHN |
分类号 |
F01D5/22;F01D11/00 |
主分类号 |
F01D5/22 |
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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