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NDE OF IMPACT DAMAGE IN SANDWICH STRUCTURES USING ULTRASONIC, THERMOGRAPHY AND LASER SHEAROGRAPHY

机译:超声,热成像和激光剪切成像技术对夹层结构的冲击损伤无损检测

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摘要

In this paper, the capabilities of thermal and vacuum shearography and pulsed thermography are compared with conventional pulse-echo and through-transmission ultrasonic methods using honeycomb composite samples with simulated defects as well as real impact damage. It is shown that the pulse-echo ultrasonic can detect skin delamination while the through-transmission ultrasonic can detect the total impact damage but cannot distinguish between the delamination and the core damage. Similarly vacuum shearography can identify the total damage while pulsed thermography and thermal shearography only show the skin delamination but not the core damage when the sample is in the "dry" condition. However, when moisture is allowed to penetrate into the honeycomb core, it is possible to detect the core damage using these methods. It is also shown that reference samples containing Teflon and other inserts that are developed for the calibration of ultrasonic equipment may not be appropriate for thermography or shearography techniques.
机译:在本文中,将热,真空剪切成像和脉冲热成像的能力与使用模拟缺陷以及实际冲击损伤的蜂窝状复合材料样品的常规脉冲回波和透射超声方法进行了比较。结果表明,脉冲回波超声可以检测到皮肤分层,而直通超声可以检测到总的冲击损伤,但不能区分分层和核心损伤。类似地,真空切变成像可以识别出总的损坏,而脉冲热成像和热切变成像仅显示出皮肤的分层,而当样品处于“干燥”状态时则不显示芯层的破坏。然而,当允许水分渗透到蜂窝状芯中时,可以使用这些方法检测芯的损坏。还表明,包含特氟隆和其他用于校准超声设备的嵌件的参考样品可能不适用于热成像或剪切成像技术。

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  • 会议地点 Seattle WA(US)
  • 作者单位

    National Research Council Canada, Institute for Aerospace Research Ottawa, ON, Canada, K1A 0R6 marc.genest@nrc-cnrc.gc.ca;

    rnNational Research Council Canada, Institute for Aerospace Research Ottawa, ON, Canada, K1A 0R6;

    rnNational Research Council Canada, Institute for Aerospace Research Ottawa, ON, Canada, K1A 0R6;

    rnNational Research Council Canada, Institute for Aerospace Research Ottawa, ON, Canada, K1A 0R6;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 工程材料学;
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