| 发明名称 |
COMPRESSOR BLADE WITH FORWARD SWEEP AND DIHEDRAL |
| 摘要 |
An airfoil for use as rotor blades in compressors for turbomachines, such as gas turbine engines. The airfoil includes increased forward sweep and forward dihedral effective to reduce losses generated by interaction of tip clearance flow, secondary flows and passage shocks.
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| 申请公布号 |
US2010054946(A1) |
申请公布日期 |
2010.03.04 |
| 申请号 |
US20080204034 |
申请日期 |
2008.09.04 |
| 申请人 |
OROSA JOHN;MONTGOMERY MATTHEW |
发明人 |
OROSA JOHN;MONTGOMERY MATTHEW |
| 分类号 |
F01D5/14 |
主分类号 |
F01D5/14 |
| 代理机构 |
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代理人 |
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| 地址 |
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