首页> 外文会议>Instrumentation in Aerospace Simulation Facilities, 1999. ICIASF 99. 18th International Congress on >An optical technique for detecting fatigue cracks in aerospacestructures
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An optical technique for detecting fatigue cracks in aerospacestructures

机译:用于检测航空航天疲劳裂纹的光学技术结构

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The development of a field-deployable non-intrusive optical-basedcrack-detection and measurement system based ontemperature-sensitive-paint (TSP) technology is described. The TSPdeveloped is based on a platinum porphyrin immobilized in asol-gel-derived thin film. For this test, the TSP is deposited on top ofan aluminum plate that is then subjected to dynamic fatigue through theuse of an electrodynamic shaker. Detection of cracks in the aluminum isaccomplished by monitoring the changes in the surface temperature of theplate as it was excited at its resonant frequency. Visualization andmeasurement of the cracks is easily accomplished in near real time usingthis method. Finally, this method is compared with conventionalthermography, and the results indicate that for aluminum, thesurface-temperature change was below the resolution of conventionalinstrumentation
机译:基于现场可部署的非侵入式光学系统的开发 裂纹检测与测量系统 描述了温度敏感涂料(TSP)技术。 TSP 研发的产品基于固定在 溶胶凝胶衍生的薄膜。对于此测试,TSP存放在 铝板,然后通过 使用电动振动筛。检测铝中的裂纹是 通过监测表面温度的变化来完成 板在共振频率下被激发。可视化和 裂纹的测量很容易通过近实时的方式完成 这种方法。最后,将该方法与常规方法进行比较 热成像,结果表明,对于铝, 表面温度变化低于常规分辨率 仪器仪表

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