Paper
28 March 2005 Quantitative thermal imaging analysis of aircraft materials: through skin sensing
Author Affiliations +
Abstract
Thermal non-destructive testing (NDT) is commonly used for assessing aircraft structures. This research work evaluates the potential of pulsed -- transient thermography for locating fixtures beneath aircraft skins in order to facilitate accurate automated assembly operations. Representative aluminium and carbon fibre aircraft skin-fixture assemblies were modelled using thermal modelling software. The assemblies were also experimentally investigated with an integrated pulsed thermographic evaluation system, as well as using a custom built system incorporating a miniature un-cooled camera. Modelling showed that the presence of an air gap between skin and fixture significantly reduced the thermal contrast developed, especially in aluminium. Experimental results show that fixtures can be located to accuracies of 0.5 mm.
© (2005) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Nicolas P. Avdelidis, L. J. Nelson, and D. P. Almond "Quantitative thermal imaging analysis of aircraft materials: through skin sensing", Proc. SPIE 5782, Thermosense XXVII, (28 March 2005); https://doi.org/10.1117/12.592437
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KEYWORDS
Skin

Aluminum

Thermography

Modeling

Cameras

Miniature imaging systems

Thermal modeling

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