发明名称 |
Vibration damper, in particular for an helicopter rotor |
摘要 |
The rotor vibration absorber has a drive shaft (10) and rigid section (6) absorbing vibrations and hydraulic deadening (3) in a cavity. There is a compensation cavity communicating with the viscous fluid deadening cavity. There is a flexible membrane (70) in the fluid deadening cavity and filled with gas. The membrane is a set distance from the internal wall (26). |
申请公布号 |
EP1136354(A4) |
申请公布日期 |
2001.07.16 |
申请号 |
EP20010400567 |
申请日期 |
2001.03.05 |
申请人 |
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发明人 |
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分类号 |
B64C27/00;B64C27/51;F16F1/40;F16F9/10;F16F13/08;F16F13/10;F16F13/18 |
主分类号 |
B64C27/00 |
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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