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Thermal characterization of defects in aircraft structures via spatially controlled heat a

机译:通过空间控制热量a对飞机结构中的缺陷进行热表征

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Abstract: Recent advances in thermal imaging technology have spawned a number of new thermal NDE techniques that provide quantitative information about flaws in aircraft structures. Thermography has a number of advantages as an inspection technique. It is a totally noncontacting, nondestructive, imaging technology capable of inspecting a large area in a matter of a few seconds. The development of fast, inexpensive image processors have aided in the attractiveness of thermography as an NDE technique. These image processors have increased the signal to noise ratio of thermography and facilitated significant advances in post- processing. The resulting digital images enable archival records for comparison with later inspections thus providing a means of monitoring the evolution of damage in a particular structure. The National Aeronautics and Space Administrations's Langley Research Center has developed a thermal NDE technique designed to image a number of potential flaws in aircraft structures. The technique involves injecting a small, spatially controlled heat flux into the outer surface of an aircraft. Images of fatigue cracking, bond integrity and material loss due to corrosion are generated from measurements of the induced surface temperature variations. This paper presents a discussion of the development of the thermal imaging system as well as the techniques used to analyze the resulting thermal images. Spatial tailoring of the heat coupled with the analysis techniques represent a significant improvement in the detectability of flaws over conventional thermal imaging. Results of laboratory experiments on fabricated crack, disbond and material loss samples are presented to demonstrate the capabilities of the technique. An integral part of the development of this technology is the use of analytic and computational modeling. The experimental results are compared with these models to demonstrate the utility of such an approach. !4
机译:摘要:热成像技术的最新进展催生了许多新的热NDE技术,这些技术可提供有关飞机结构缺陷的定量信息。热成像作为检查技术具有许多优点。它是一种完全非接触,非破坏性的成像技术,能够在几秒钟内检查大面积区域。快速,廉价的图像处理器的发展有助于将热成像技术作为NDE技术的吸引力。这些图像处理器提高了热成像的信噪比,并促进了后处理的重大进步。生成的数字图像使档案记录能够与以后的检查进行比较,从而提供了一种监视特定结构中损坏演变的方法。美国国家航空航天局的兰利研究中心已开发出一种热能无损检测技术,旨在对飞机结构中的许多潜在缺陷进行成像。该技术涉及将较小的,受空间控制的热通量注入飞机的外表面。测量引起的表面温度变化会产生疲劳裂纹,粘结完整性和由于腐蚀引起的材料损失的图像。本文讨论了热成像系统的发展以及用于分析最终热图像的技术。与传统的热成像技术相比,热量的空间调整与分析技术相结合可显着改善缺陷的可检测性。提出了关于制造的裂纹,脱粘和材料损失样品的实验室实验结果,以证明该技术的功能。这项技术发展不可或缺的一部分是分析和计算模型的使用。将实验结果与这些模型进行比较,以证明这种方法的实用性。 !4

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