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Infrared Thermal Wave Nondestructive Technology on the Defect in the Shell of Solid Rocket Motor

机译:红外热波无损检测技术对固体火箭发动机壳体缺陷的影响

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Based on the active infrared thermography nondestructive testing (NDT) technology, which is an emerging method and developed in the areas of aviation, spaceflight and national defence, the samples including glass fiber flat bottom hole sample, glass fiber inclusion sample and steel flat bottom hole sample that the shell materials of Solid Rocket Motor (SRM) were heated by a high energy flash lamp. The subsurface flaws can be detected through measuring temperature difference between flaws and materials. The results of the experiments show that: 1) the technique is a fast and effective inspection method, which is used for detecting the composites more easily than the metals. And it also can primarily identify the defect position and size according to the thermal image maps. 2) A best inspection time at when the area of hot spot is the same with that of defect is exited, which can be used to estimate the defect size. The bigger the defect area, the easier it could be detected and also the less of the error for estimating defect area. 3). The infrared thermal images obtained from experiments always have high noise, especially for metal materials due to high reflectivity and environmental factors, which need to be further processed.
机译:基于主动红外热成像无损检测(NDT)技术,该技术是在航空,航天和国防领域新兴的方法,开发的样品包括玻璃纤维平底孔样品,玻璃纤维夹杂物样品和钢制平底孔样品样本表明,固体火箭发动机(SRM)的外壳材料是由高能闪光灯加热的。可以通过测量缺陷和材料之间的温差来检测表面缺陷。实验结果表明:1)该技术是一种快速有效的检测方法,比金属更易于检测复合材料。并且它还可以根据热图像图主要识别缺陷的位置和大小。 2)退出了热点区域与缺陷区域相同的最佳检查时间,可以用来估计缺陷的大小。缺陷面积越大,越容易被检测到,并且用于估计缺陷面积的误差也越小。 3)。从实验中获得的红外热图像始终具有高噪声,特别是对于金属材料,由于其高反射率和环境因素,需要进一步处理。

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