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Damage analysis during full-scale testing of F-15 airframe using arrays of optical fiber sensors

机译:使用光纤传感器阵列F-15机身的全尺度测试损伤分析

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We discuss fatigue test results using extrinsic Fabry-Perot interferometric (EFPI) strain gages on a F-15 fighter within a full-scale test frame at the Structures Test Facility, Wright Patterson Air Force Base, Ohio. A linear array of EFPI sensors were surface-mounted to the trailing edge of the F-15 wing to monitor strain concentration along the inboard flap hinge. Two types of EFPI strain gages and strain gage support systems were employed; linearized output from the standard, differential EFPI sensor system determined dynamic strain on the flap hinge during the application of load, whereas, absolute EFPI strain sensors were implemented to measure residual strain or cracks in the aluminum hinge.
机译:在结构测试设施的全尺度测试框架内,在F-15战斗机上使用外在的法布里 - 珀罗干涉管(EFPI)应变计,在结构测试设施中,俄亥俄州的全规模测试框架,讨论疲劳试验结果。用线性阵列的EFPI传感器表面安装到F-15机翼的后缘,以沿着内侧挡板铰链监测应变浓度。采用两种类型的EFPI应变计和应变计支持系统;从标准的线性化输出,差分EFPI传感器系统确定了载荷期间襟翼铰链上的动态应变,而绝对EFPI应变传感器被实施以测量铝合金铰链中的残留应变或裂缝。

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