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The device of the attenuation of the vibrations to the rotor of helicopter

机译:衰减对直升机旋翼的振动的装置

摘要

The damper consists of a rotary suspended member (20) situated on the underside of the rotor blade support arm on a vertical axle (24). The suspended member has a vertical axis of rotation (B1) which is offset relative to the axis (A1) of its suspension axle and situated closer to the suspended member's centre of inertia. The damper is equipped with a regulator to adjust the distance between the two axes (A1, B1), comprising a spacer plate with a series of apertures for fixing pegs. In addition, the weight of the suspended member can be varied by means of a disc (36) bolted to its underside.
机译:减震器由位于转子叶片支撑臂下侧的垂直轴(24)上的旋转悬挂部件(20)组成。悬挂构件具有垂直的旋转轴线(B1),该垂直旋转轴线相对于其悬挂轴的轴线(A1)偏移并且位于更靠近悬挂构件的惯性中心的位置。阻尼器配备有一个调节器,用于调节两个轴(A1,B1)之间的距离,包括一个带有一系列用于固定销钉的孔的隔板。另外,可通过螺栓连接到其下侧的盘(36)来改变悬挂构件的重量。

著录项

  • 公开/公告号FR2733483B1

    专利类型

  • 公开/公告日1997-07-04

    原文格式PDF

  • 申请/专利权人 EUROCOPTER FRANCE;

    申请/专利号FR19950005071

  • 发明设计人 BRUNO ROBERT GUIMBAL;

    申请日1995-04-27

  • 分类号B64C27/51;

  • 国家 FR

  • 入库时间 2022-08-22 03:12:21

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