基于预拉伸基片式FBG的工字梁载荷测试
作者:
作者单位:

作者简介:

通讯作者:

基金项目:

教育部“长江学者和创新团队”发展计划基金资助项目(IRT1212);北京市重大科技计划基金资助项目 (Z151100003615010)

伦理声明:



Joist Load Test Based on Prestretching Substrate FBG Sensor
Author:
Ethical statement:

Affiliation:

Funding:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
    摘要:

    对工字梁载荷测试与基片式光纤光栅传感器受力进行有限元分析仿真,制作并封装加载确定的预拉伸力的基片式光纤光栅传感器。在材料拉伸机(MTS)上进行预拉伸基片式光纤光栅传感器标定与裸光纤光栅传感器对比测试实验,得到预拉伸制作工艺传感器提高了测量范围、应变灵敏度为0.95 pm/με、线性度0.996、传递效率为83.5%。将其应用到飞机机翼工字梁上测试,同时电阻应变计监测最大应变,得到很好的测试效果,与仿真结果相吻合,对飞机机翼载荷标定具有重要意义。

    Abstract:

    The finite element analysis simulation of the joist load testing and the substrate FBG sensor was performed in this paper.The substrate FBG sensor with certain prestretching force loaded was fabricated and packaged.The experiment on the calibration was carried out to compare the prestretching substrate FBG sensor with the bare FBG sensor in MTS.The results showed that the measurement range of the sensor fabricated the prestretching process was improved,the strain sensitivity was of 0.95 pm/με,linearity was 0.996,and the transfer efficiency was 83.5%. The load testing was applied to the joist of airplane wing,while using the resistance strain gauge was used to monitor the maximum strain,good test results were obtained and consistent with the simulation results,which was of great significance for the calibration of aircraft wing loading.

    参考文献
    相似文献
    引证文献
引用本文

鹿利单, 闫光, 刘锋, 祝连庆.基于预拉伸基片式FBG的工字梁载荷测试[J].压电与声光,2017,39(4):619-623. LU Lidan, YAN Guang, LIU Feng, ZHU Lianqing. Joist Load Test Based on Prestretching Substrate FBG Sensor[J]. PIEZOELECTRICS AND ACOUSTOOPTICS

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
历史
  • 收稿日期:
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2017-08-14
  • 出版日期: