首页> 外国专利> Flexbeam helicopter rotor with improved snubber-vibration damper between the torque tube and the flexible spar member

Flexbeam helicopter rotor with improved snubber-vibration damper between the torque tube and the flexible spar member

机译:Flexbeam直升机旋翼,在扭矩管和柔性翼梁部件之间具有改进的减振阻尼器

摘要

The flexbeam helicopter rotor has an improved snubber-vibration damper (52, 53) for positioning the flexbeam spar (22) relative to the torque tube (28), wherein the snubber-damper (52, 53) is an elastomeric bearing having a spherical and a flat portion (64, 70), and whose laminates (80, 82, 76, 78) are continuous, selectively preloaded and of selected material to provide increased fatigue life, size reduction, reduced laminate stress concentration, and reduced critical design stress in the snubber-vibration damper.
机译:柔性梁直升机旋翼具有改进的缓冲器减振器(52、53),用于相对于扭矩管(28)定位柔性梁翼梁(22),其中,缓冲器阻尼器(52、53)是具有球形的弹性体轴承。扁平部分(64、70),其叠层(80、82、76、78)是连续的,有选择地预加载并由选定的材料制成的,以延长疲劳寿命,减小尺寸,减小叠层应力集中并减小临界设计应力在减振器中。

著录项

  • 公开/公告号EP0451084B1

    专利类型

  • 公开/公告日1995-03-01

    原文格式PDF

  • 申请/专利权人 UNITED TECHNOLOGIES CORP;

    申请/专利号EP19910630019

  • 发明设计人 BYRNES FRANCIS EDWARD;DANNA FRANK PAUL;

    申请日1991-03-27

  • 分类号B64C27/51;B64C27/33;B64C27/35;

  • 国家 EP

  • 入库时间 2022-08-22 04:13:50

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