| 发明名称 |
Stator assembly for the fan of a multi-flow turbo-jet engine |
| 摘要 |
The radially outer end of the aerofoil portion of each vane of a stator assembly for the fan of a turbo-jet engine is bent at right angles and is inserted in a slot-like opening provided in an outer ring which is fixed to the casing via screws in conjunction with spacers each of which has a foot which partly overlaps the adjacent opening.
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| 申请公布号 |
US4820120(A) |
申请公布日期 |
1989.04.11 |
| 申请号 |
US19870063431 |
申请日期 |
1987.06.18 |
| 申请人 |
SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION "S.N.E.C.M.A." |
发明人 |
FEUVRIER, THIERRY;FORESTIER, ALEXANDRE |
| 分类号 |
F01D9/04;(IPC1-7):F01D9/02 |
主分类号 |
F01D9/04 |
| 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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