| 发明名称 |
FAN ROTOR FOR AN AIRPLANE TURBOJET ENGINE |
| 摘要 |
<p>A fan rotor for an airplane turbojet including locking blade roots in the respective grooves of an airplane turbojet fan rotor. Each blade root is housed in a groove that is closed by a main latch and by an additional latch that is distinct from the main latch and that is spaced apart therefrom by a predetermined distance.</p> |
| 申请公布号 |
EP2427658(B1) |
申请公布日期 |
2015.07.08 |
| 申请号 |
EP20100723700 |
申请日期 |
2010.04.19 |
| 申请人 |
SNECMA |
发明人 |
BUISSON, HERVÉ;GOGA, JEAN-LUC |
| 分类号 |
F04D29/32;F01D5/30 |
主分类号 |
F04D29/32 |
| 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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