首页> 外国专利> Hollow shaft as rotor mast of helicopter has device provided inside cavity of hollow shaft for detecting cracks in shaft and connected to analyzing and indicating unit

Hollow shaft as rotor mast of helicopter has device provided inside cavity of hollow shaft for detecting cracks in shaft and connected to analyzing and indicating unit

机译:中空轴作为直升机的旋翼桅杆,在中空轴的空腔内设有用于检测轴中裂纹的装置,并与分析指示装置相连

摘要

A device(10) is provided inside the cavity of the hollow shaft for detecting cracks in the shaft(1) and is connected to an analyzing and indicating unit(23). The device has at least two sealing means(12,13) for sealing the hollow shaft against atmosphere, and the sealed shaft cavity(19) is overpressurized with gas relative to the outside atmosphere and a gas pressure change in the cavity is sensed by a pressure sensor(22) which sends a signal to the analyzing and indicating unit.
机译:在空心轴的腔体内设置有用于检测轴(1)中的裂纹的装置(10),该装置(10)连接至分析和指示单元(23)。该装置具有至少两个用于使空心轴相对于大气密封的密封装置(12,13),并且密封的轴腔(19)相对于外部气体被气体过度加压,并且腔中的气压变化由传感器感应到。压力传感器(22),它向分析和指示单元发送信号。

著录项

  • 公开/公告号DE19944412A1

    专利类型

  • 公开/公告日2001-04-05

    原文格式PDF

  • 申请/专利权人 EUROCOPTER DEUTSCHLAND GMBH;

    申请/专利号DE1999144412

  • 发明设计人 SEIDL WERNER;GERGELY PETER;

    申请日1999-09-16

  • 分类号B64D35/00;B64D43/00;B64C27/04;

  • 国家 DE

  • 入库时间 2022-08-22 01:10:18

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