| 发明名称 |
Aircraft fan blade damping apparatus |
| 摘要 |
Disclosed is apparatus to prevent vibration of a pinned root fan blade during low speed revolution of the blade comprising a damping device which extends between the airfoil of the blade and the engine structure.
|
| 申请公布号 |
US5205714(A) |
申请公布日期 |
1993.04.27 |
| 申请号 |
US19920852833 |
申请日期 |
1992.03.16 |
| 申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
SHAH, SAMIR I.;THEMUDO, RAMON;EVEN-NUR, MICHAEL |
| 分类号 |
B64C11/04;F01D5/26 |
主分类号 |
B64C11/04 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
|
| 地址 |
|
