| 发明名称 |
TURBOMACHINE CENTRE BLADE COMPRISING A CURVED PORTION |
| 摘要 |
A turbomachine compressor blade of main radial orientation with respect to a main axis of the turbomachine. The blade includes a radially internal root portion, a radially external tip portion, a radially intermediate portion, a curved portion tangentially in a direction, and at least one straight portion on the root portion and/or on the tip portion. |
| 申请公布号 |
US2014248144(A1) |
申请公布日期 |
2014.09.04 |
| 申请号 |
US201214349000 |
申请日期 |
2012.10.11 |
| 申请人 |
SNECMA |
发明人 |
Cellier Damien;Dufresne Alicia Lise, Julia;Pelletrau Philippe Pierre Marcel, Marie;Perrot Vincent Paul, Gabriel;Rios Jean-Francois Antoine, Christian;Villaines Laurent Christophe, Francis |
| 分类号 |
F04D29/66;F04D29/40 |
主分类号 |
F04D29/66 |
| 代理机构 |
|
代理人 |
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| 主权项 |
|
| 地址 |
Paris FR |
