发明名称 Simplified anti-vibration suspension for helicopter
摘要 The suspension comprises three inclined bars (8) each articulated (9,14) on the transmission box (2) and the structure (1) by a rigid lever (11). The lever supports a swinging mass (12) and is also pivoted on the structure. Each inclined bar has a traction bar (15) articulated (16,18) on the transmission box and the structure. The corresponding lever is articulated on the structure by pivoting on the lower end part of the corresponding traction bar.
申请公布号 FR2777861(A1) 申请公布日期 1999.10.29
申请号 FR19980005094 申请日期 1998.04.23
申请人 EUROCOPTER FRANCE 发明人 CERTAIN NICOLAS PIERRE GEORGES
分类号 B64C27/00;F16F7/10;F16F15/00;F16F15/02;(IPC1-7):B64C27/00;F16F15/04;F16F15/28 主分类号 B64C27/00
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