| 发明名称 |
Aerofoil blade in particular that constituting a vane of turbine engine fan and compressor |
| 摘要 |
An airfoil (14) having a barrel shaped leading edge between a root (20) and a tip (22), and forward aerodynamic sweep at the tip. <IMAGE> |
| 申请公布号 |
PL201181(B1) |
申请公布日期 |
2009.03.31 |
| 申请号 |
PL20000344738 |
申请日期 |
2000.12.21 |
| 申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
DECKER JOHN JARED;BREEZE-STRINGFELLOW ANDREW;STEINMETZ GREGORY TODD;SZUCS PETER NICHOLAS |
| 分类号 |
F01D5/14;F02K3/00;F04D29/32;F04D29/38 |
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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