首页> 外国专利> System and method of monitoring blade vibration in a turbine engine

System and method of monitoring blade vibration in a turbine engine

机译:监测涡轮发动机中的叶片振动的系统和方法

摘要

A rotor blade measurement system includes a microwave source (26) and a probe (28). A directional coupler (34) is attached to the source (26) and the probe (28). A detector (36) is attached to the directional coupler (34). The probe directs a microwave signal (30) toward a rotor (20) such that during rotation the rotor blade (22) will pass through the path of the microwave signal (30). As the rotor blade (22) passes, the microwave signal (30) is reflected back to the probe (28). The directional coupler (34) separates the original microwave signal (30) and the reflected signal (32). The detector (36) then determines the energy level of the reflected signal (32). As each rotor blade (22) passes the microwave signal (30) it generates a reflected signal that can be analyzed over time. From the length and shape of the waveform of the reflected signal (32) the amount of twisting and flutter in a rotor blade can be determined.
机译:转子叶片测量系统包括微波源(26)和探针(28)。定向耦合器(34)连接到源(26)和探针(28)。检测器(36)附接到定向耦合器(34)。探针将微波信号(30)引向转子(20),使得在旋转过程中,转子叶片(22)将通过微波信号(30)的路径。随着转子叶片(22)的通过,微波信号(30)被反射回探头(28)。定向耦合器(34)将原始微波信号(30)和反射信号(32)分离。然后,检测器(36)确定反射信号(32)的能级。当每个转子叶片(22)通过微波信号(30)时,它会生成一个反射信号,可以随时间进行分析。根据反射信号(32)的波形的长度和形状,可以确定转子叶片中的扭曲和颤动量。

著录项

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