首页> 外国专利> Device with concentrated masses for reducing the vibration caused by a lift rotor of a rotorcraft, and hub of a rotor provided with such a device

Device with concentrated masses for reducing the vibration caused by a lift rotor of a rotorcraft, and hub of a rotor provided with such a device

机译:具有减小飞行器的升力旋翼引起的振动的集中质量的装置以及配备有该装置的旋翼毂

摘要

The device has a rod (40) extending longitudinally along a rotation axis of a lift rotor and a hub such that a lower end of the rod is articulated inside a rotor mast of the rotor. A secondary oscillating mass (50) is suspended within a recess (11) of a main oscillating mass (10) along a vertical axis (AX1) perpendicular a horizontal plane (P) by elastic units (60). The secondary oscillating mass is secured to the main oscillating mass in translation in the horizontal plane. An independent claim is also included for a hub for a lift rotor of a rotorcraft, comprising an upper zone integrated to an envelope of a vibration reducing device.
机译:该装置具有沿着提升转子的旋转轴线纵向延伸的杆(40)和毂,使得杆的下端铰接在转子的转子桅杆内。辅助振动块(50)通过弹性单元(60)沿着垂直于水平面(P)的垂直轴(AX1)悬挂在主振动块(10)的凹部(11)内。次级振荡质量块在水平面上平移地固定到主振荡质量块上。还包括一种用于旋翼飞机的升力旋翼的毂的独立权利要求,其包括与减振装置的外壳整合在一起的上部区域。

著录项

  • 公开/公告号EP2253534A1

    专利类型

  • 公开/公告日2010-11-24

    原文格式PDF

  • 申请/专利权人 EUROCOPTER;

    申请/专利号EP20100004036

  • 发明设计人 GIRARD VINCENT;MAZET STEPHANE;

    申请日2010-04-16

  • 分类号B64C27/35;B64C27/32;F16F7/116;

  • 国家 EP

  • 入库时间 2022-08-21 17:56:43

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