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出 处:《Transactions of Nanjing University of Aeronautics and Astronautics》1997年第2期126-130,共5页南京航空航天大学学报(英文版)
基 金:航空科学基金
摘 要:This paper presents an optical sensor technique used in the damage evaluation which is formed by structurally integrated fiber optic reticulate sensors embedded in the composite materials. The fibers are processed by chemical method and their outsides are peeled to form particles of irregular distribution and they differ in size, so the slight disturbance range of stochastic wall are formed in fibers. According to the characteristics of power loss of waveguide mode caused by slight disturbance of stochastic wall and radiative mode transmission, the range of slight disturbance of stochastic wall may be served as the sensitive range of the sensor. On the basis of theory of slight disturbance of stochastic wall of planar optical waveguide, the relation between the corrosion time and the opposite power loss by experiments is investigated. In this paper, the measurement results of object of SIFORS are also presented. The results show that the optical sensor technique may be used in the damage evaluation of an aircraft.提出并研究一种构成光纤传感网络埋入复合材料内部用于损伤探测的光纤传感技术.对光纤进行化学处 理,剥去光纤外层在纤芯表面形成无规则分布、大小不一的微粒,在光纤形成随机壁微扰区.根据随机壁微扰导致导模与辐射模的模转换引起功率损耗的特性,随机壁微扰区就可以为敏感区.本文根据平面波导随机壁微扰理论并实验研究了腐蚀时间与相对功率损耗的关系.最后给出内含光纤传感网络试件的实测结果.结果表明,本文提出的光纤传感技术可用于复合材料损伤探测,为监测飞行器飞行时的载荷及损伤结果提供一种测试方法.
关 键 词:composite materials optical fibers optical fiber sensor planar optical waveguide stochastic wall slight disturbance damage evaluation
分 类 号:TP212[自动化与计算机技术—检测技术与自动化装置]
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