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The architecture of the mounting of a power transmission of a rotorcraft, comprising a vibration damper device implementing the shock absorbers laminates

机译:旋翼机动力传动装置的安装结构,包括减振器装置,该减振器装置实现减震器层压板

摘要

The present invention relates to an architecture of the assembly to the edge of a rotorcraft of a main power transmission is carried by the suspension mast of a main rotor and supported by a chassis by means of a vibration damper device implementing the laminated dampers (12). The laminated dampers (12) comprise a body (16) with laminated armatures (17,18) at its axial end faces. At least one of the reinforcements (17,18) comprises a stop (19) of axial bearing radially sliding of the reinforcements (17,18) against one another in the case of excessive wear of the laminated body (16), said bearing limiting the travel of the pivoting of the main gearbox to a predetermined wear threshold of the body (16 laminated).
机译:本发明涉及一种到主动力的旋翼飞行器的边缘的组件的结构,该组件的结构由主旋翼的悬挂杆支撑,并通过实现叠片阻尼器(12)的减振器装置由底盘支撑。 。叠片阻尼器(12)包括在其轴向端面上具有叠片电枢(17,18)的主体(16)。加强件中的至少一个(17,18)包括止动件(19),该止动件在层叠体(16)过度磨损的情况下使加强件(17,18)彼此径向地轴向滑动。主变速箱枢轴转动到车身的预定磨损阈值(16层叠)的行程。

著录项

  • 公开/公告号FR3006022B1

    专利类型

  • 公开/公告日2015-06-05

    原文格式PDF

  • 申请/专利权人 EUROCOPTER;

    申请/专利号FR20130001158

  • 发明设计人 BASTIEN DIRIONG;MATHIEU LEGRAND;

    申请日2013-05-21

  • 分类号F16D3/56;B64C27/00;

  • 国家 FR

  • 入库时间 2022-08-21 14:54:19

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