发明名称 Vibration damper and in particular frequency adapter for a helicopter blade
摘要 The device comprises two rigid elements 1a, 1b, 2 and an elastomer mass 10 interposed therebetween so as to be deformed when the elements move relative to each other in a longitudinal direction. The device includes a closed space with a restriction element 16 defining two chambers 23, 24 whose volumes vary inversely upon movement of the chamber walls, the two chambers being interconnected by one or more passages, the empty space being filled with a viscous fluid material so as to produce a damping effect in the passages. Application to helicopter blade frequency adapters.
申请公布号 US4566677(A) 申请公布日期 1986.01.28
申请号 US19830502236 申请日期 1983.06.08
申请人 VIBRACHOC 发明人 LE PIERRES, GILDAS
分类号 B64C27/51;F16F9/30;(IPC1-7):F16F9/14 主分类号 B64C27/51
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