| 发明名称 |
Speed reducer for aviation engine |
| 摘要 |
The hub 18 of the propeller is fixed to the hollow motor pinion 8 by a long elastic screw 19. There is only one bolt to be undone in order to dismantle the propeller; this bolt cannot work loose and it makes it possible to keep the thin part of the pinion under compression pre-stress. <IMAGE>
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| 申请公布号 |
FR2547551(A1) |
申请公布日期 |
1984.12.21 |
| 申请号 |
FR19830009799 |
申请日期 |
1983.06.14 |
| 申请人 |
GIRONNET BERNARD |
发明人 |
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| 分类号 |
B64D35/00;F16D1/06;F16H57/02;F16H57/021;(IPC1-7):B64D35/00;F16H1/06 |
主分类号 |
B64D35/00 |
| 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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