首页> 外国专利> Monolithic blade, a rotorcraft rotor fitted with such a monolithic blade, and an associated rotorcraft

Monolithic blade, a rotorcraft rotor fitted with such a monolithic blade, and an associated rotorcraft

机译:整体式桨叶,装配有这种整体式桨叶的旋翼航空器旋翼以及相关的旋翼航空器

摘要

A monolithic blade of a rotorcraft rotor, the blade comprising at least locally an airfoil zone having a pressure side face and a suction side face. The invention is remarkable in that the blade has a root zone including a finger with a spherical bearing surface arranged at a root end of the blade, a recess suitable for receiving a laminated spherical bearing, and a flexible portion having a preferred direction of deformation in bending about a flapping axis of the blade, the flexible portion being arranged between the finger and the recess.
机译:旋翼飞机旋翼的整体式叶片,该叶片至少局部地包括具有压力侧面和吸力侧面的翼型区。本发明的显着之处在于,叶片具有根部区域,该根部区域包括指状件,该指状件具有布置在叶片根部端的球形支承表面;适合于容纳叠层球形轴承的凹槽;以及柔性部分,其具有优选的变形方向。围绕刀片的拍动轴线弯曲,挠性部分布置在指状物和凹部之间。

著录项

  • 公开/公告号US10301014B2

    专利类型

  • 公开/公告日2019-05-28

    原文格式PDF

  • 申请/专利权人 AIRBUS HELICOPTERS;

    申请/专利号US201715594961

  • 发明设计人 ANDRE AMARI;JACQUES GAFFIERO;

    申请日2017-05-15

  • 分类号B64C27/48;B64C27/635;B64C27/473;

  • 国家 US

  • 入库时间 2022-08-21 12:14:09

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