| 发明名称 |
Rotor blade platform of a gas turbine engine |
| 摘要 |
<p>A rotor blade (62) for a gas turbine engine (10) includes a platform section (66) between a root section (64) and an airfoil section (68), the platform section (66) having a non-axisymmetric surface contour.</p> |
| 申请公布号 |
EP2372102(A2) |
申请公布日期 |
2011.10.05 |
| 申请号 |
EP20110161072 |
申请日期 |
2011.04.04 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
PRAISNER, THOMAS J.;GROVER, ERIC A. |
| 分类号 |
F01D11/00;F01D5/14;F01D5/22 |
主分类号 |
F01D11/00 |
| 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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