首页> 外国专利> Vibration insulator for helicopter; has two force conduction points connected by insulator that generates dynamic counter oscillations, which are transmitted by spring system

Vibration insulator for helicopter; has two force conduction points connected by insulator that generates dynamic counter oscillations, which are transmitted by spring system

机译:直升机用隔振器;有两个通过绝缘子连接的力传导点,可产生动态的反振荡,并通过弹簧系统传递

摘要

The insulator (20) has two force conduction points (21,22) connected by an insulator that absorbs high-frequency vibrations on either point and generates dynamic counter oscillations. A spring system (25) is arranged parallel to the insulator and swivels outwards in proportion to the counter oscillations. A damper unit is also coupled to the insulator. The damper unit coupled to the insulator has a damping constant selected so that the counter oscillations are transmitted undamped to both force conduction points, but so that static or quasistatic external forces are only transmitted by the spring system. The spring system conducts the external forces and matches the damping unit. An Independent claim is included for a helicopter including the vibration insulator.
机译:绝缘体(20)具有通过绝缘体连接的两个力传导点(21,22),该绝缘体吸收任一点上的高频振动并产生动态反振荡。弹簧系统(25)平行于绝缘体布置并且与反振荡成比例地向外旋转。阻尼器单元也耦合到绝缘体。耦合到绝缘子上的阻尼器单元具有一个选定的阻尼常数,以使反振荡不受阻尼地传递到两个力传导点,但是静态或准静态外力仅通过弹簧系统传递。弹簧系统传导外力并匹配阻尼单元。包含防振器的直升机包括独立索赔。

著录项

  • 公开/公告号DE10001159A1

    专利类型

  • 公开/公告日2001-07-26

    原文格式PDF

  • 申请/专利权人 LIEBHERR-AEROSPACE LINDENBERG GMBH;

    申请/专利号DE2000101159

  • 发明设计人 WEISS KLAUS;HAUSY WERNER;

    申请日2000-01-13

  • 分类号B64C27/32;B06B1/06;F16F9/46;

  • 国家 DE

  • 入库时间 2022-08-22 01:10:00

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号