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Device with distributed 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:具有减小的质量的用于减小由旋翼机的提升旋翼引起的振动的装置以及设置有这种装置的旋翼的毂

摘要

The device (1) has a support (10) secured in rotation around a rotation axis (AX) of a lift rotor. Main oscillating masses (22) are distributed around the support by being connected to the support through a deformable unit (30), where each main mass is provided with recesses (21', 22'). Each main mass is forced to move only in a horizontal plane (P) by the deformable unit. Each main mass is provided with secondary oscillating masses (41, 42) suspended within the recesses by elastic units (50) so as to move in a direction perpendicular to the horizontal plane. An independent claim is also included for a hub for a lift rotor of a rotorcraft, comprising an upper part integrated to a support of a vibration reducing device.
机译:装置(1)具有支撑件(10),支撑件(10)绕提升转子的旋转轴(AX)旋转。主振荡质量块(22)通过可变形单元(30)连接到支撑件上,从而在支撑件周围分布,其中每个主质量块都设有凹槽(21',22')。可变形单元迫使每个主质量仅在水平面(P)中移动。每个主质量块均具有通过弹性单元(50)悬挂在凹部内的次级振荡质量块(41、42),以在垂直于水平面的方向上移动。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,其包括集成到减振装置的支撑件上的上部。

著录项

  • 公开/公告号EP2253535A1

    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EP20100004046

  • 发明设计人 GIRARD VINCENT;

    申请日2010-04-16

  • 分类号B64C27/35;B64C27/00;B64C27/32;F16F7/116;

  • 国家 EP

  • 入库时间 2022-08-21 17:56:43

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