| 发明名称 |
CONNECTION SYSTEM FOR AIRCRAFT PROPELLER BLADES |
| 摘要 |
The invention relates to a connection system for connecting a ring which carries aircraft propeller blades to a turbine which the ring surrounds. Brackets extend between the ring and the turbine and accommodate thermal expansion of the turbine without significant deformation. |
| 申请公布号 |
GB9012432(D0) |
申请公布日期 |
1990.07.25 |
| 申请号 |
GB19900012432 |
申请日期 |
1990.06.04 |
| 申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
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| 分类号 |
B64C11/12;B64C11/02;B64D29/00;F01D5/02;F01D5/30 |
主分类号 |
B64C11/12 |
| 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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