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结构调制型长周期光纤光栅温度传感器研究

李媛媛 田甜 陈文焕 马一巍 赵磊 耿涛

航空科学技术2024,Vol.35Issue(4):67-73,7.
航空科学技术2024,Vol.35Issue(4):67-73,7.DOI:10.19452/j.issn1007-5453.2024.04.009

结构调制型长周期光纤光栅温度传感器研究

Study on Structurally Modulated Long-period Fiber Grating Temperature Sensor

李媛媛 1田甜 1陈文焕 1马一巍 1赵磊 2耿涛1

作者信息

  • 1. 哈尔滨工程大学 纤维集成光学教育部重点实验室,黑龙江 哈尔滨 150001
  • 2. 航空工业西安飞行自动控制研究所,陕西 西安 710065
  • 折叠

摘要

Abstract

The temperature monitoring of fuel system is very important for the safety,performance and reliability of aircraft.In this paper,a long-period fiber grating sensor based on laser etching method is proposed and tested,which can be used for temperature monitoring of aircraft fuel system.By demodulating the resonant peak wavelength variation of fiber grating,the precise measurement of ambient temperature can be realized.Experimental results show that this sensor has a temperature sensitivity of 83.1pm/℃and achieves a strain response of 0.32pm/με.Due to the characteristics of flexibility,corrosion resistance and electromagnetic interference resistance for the optical fibers,the proposed sensor can be flexibly installed in the complex structure of the aircraft,which has the ability to improve the safety and reliability of the aircraft.

关键词

光纤传感/温度监测/保偏光纤/长周期光纤光栅

Key words

optical fiber sensing/temperature monitoring/polarization-maintaining fiber/long-period fiber grating

分类

航空航天

引用本文复制引用

李媛媛,田甜,陈文焕,马一巍,赵磊,耿涛..结构调制型长周期光纤光栅温度传感器研究[J].航空科学技术,2024,35(4):67-73,7.

基金项目

航空科学基金(201608P6003) Aeronautical Science Foundation of China(201608P6003) (201608P6003)

航空科学技术

1007-5453

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