发明名称
摘要 A vibration absorber includes a hub arranged for rotation during operation about an aixs, a mass encircling the hub and a plurality of resilient arms extending in a spaced-apart spiral pattern between the hub and the mass so that the mass rotates with the hub in a plane of rotation perpendicular to the axis and is capable of equal resilient deflection in any direction within its plane of rotation. In operation the absorber operates as a spring mass device and finds particular application in damping vibrations in a helicopter rotor due to the facility to simultaneously cancel vibration forces of different frequencies.
申请公布号 FR2339107(B1) 申请公布日期 1983.08.19
申请号 FR19770001396 申请日期 1977.01.19
申请人 WESTLAND AIRCRAFT LTD 发明人
分类号 F16F15/12;B64C27/00;B64C27/32;B64C27/51;F16F15/121;F16F15/133;(IPC1-7):16F15/12;64C27/32 主分类号 F16F15/12
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