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FIBER BRAGG GRATING SENSOR SYSTEM FOR MONITORING COMPOSITE AEROSPACE STRUCTURES

机译:用于监测复合航空结构的光纤布拉格光栅传感器系统

摘要

To investigate strain-sensitive characteristics of fiber Bragg grating (FBG) sensors, a minimaludsensing system consisting of multiplex FBG sensors and signal demodulating and processingudinstruments was constructed. FBG sensors were designed with different package structures forudrespectively sensing strain or temperature parameters, and they returnedudmeasurand-dependent wavelengths back to the interrogation system for measurement withudhigh resolution. In this paper, tests were performed on structure samples with step-wiseudincrease of deformations. Both FBG sensing system and strain gages were tested andudcompared. Experimental work proved that the FBG sensing system had a good level ofudaccuracy in measuring the static response of the tested composite structure. Moreover theudadditional advantages such as damp proofing, high sampling rates and real-time inspectionudmake the novel system especially appropriate for load monitoring and damage detection ofudaerospace structures.
机译:为了研究光纤布拉格光栅(FBG)传感器的应变敏感特性,构建了由多重FBG传感器和信号解调与处理仪器组成的最小传感系统。 FBG传感器被设计为具有不同的封装结构,分别用于感测应变或温度参数,并且它们将依赖于测量数的波长返回到询问系统以进行高分辨率的测量。在本文中,对结构样本进行了逐步增加变形的测试。 FBG传感系统和应变计均经过测试和比较。实验工作证明,FBG传感系统在测量被测复合结构的静态响应方面具有良好的准确性。此外,具有防潮,高采样率和实时检查等常规优势,使得该新系统特别适用于载荷监测和宇航结构的损伤检测。

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