| 发明名称 |
Bladed disk with three-root blades |
| 摘要 |
The blades (10) of a turbine or a compressor are here fixed to the disk (1) by three roots (7, 8 and 9) inserted in the same number of circular grooves (4, 5 and 6). This assembly makes it possible to provide a good distribution of stresses during functioning.
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| 申请公布号 |
US5919032(A) |
申请公布日期 |
1999.07.06 |
| 申请号 |
US19980003635 |
申请日期 |
1998.01.07 |
| 申请人 |
SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION "SNECMA" |
发明人 |
NAUDET, JACKY;POY, CHRISTOPHE |
| 分类号 |
F01D5/26;F01D5/30;(IPC1-7):B63H1/20 |
主分类号 |
F01D5/26 |
| 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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