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 发明人
分类号 B64C27/00;B64C27/51;F16F1/40;F16F9/10;F16F13/08;F16F13/10;F16F13/18 主分类号 B64C27/00
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