Author:
Chulkov A. O.,Vavilov V. P.,Nesteruk D. A.,Shagdyrov B. I.
Abstract
Abstract
A self-propelled thermal flaw detector has been developed for testing large-sized flat parts by means of thermal scanning that provides higher efficiency and test performance than conventional thermal testing scheme over individual zones. The flaw detector is designed to detect delaminations, impact damage, and foreign inclusions in composite materials and can be used to test for corrosion in metal shells, providing continuous monitoring with a performance of up to 20 m2/h.
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science
Reference19 articles.
1. Oswald-Tranta, B., Comparative study of thermal contrast and contrast in thermal signal derivatives in pulse thermography, NDT & E Int., 2017, vol. 91, pp. 36–46.
2. Shepard, S.M., Flash thermography of aerospace composites 2. Thermographic signal reconstruction, Mater. Eval., 2007, vol. 65, pp. 690–696.
3. Ibarra-Castanedo, C., Genest, M., Servais, P., Maldague, X., and Bendada, A., Qualitative and quantitative assessment of aerospace structures by pulsed thermography, Nondestr. Test. Eval., 2007, vol. 22, pp. 199–215.
4. Maldague, X. and Marinetti, S., Pulse phase infrared thermography, J. Appl. Phys., 1996, vol. 79, pp. 2694–2698.
5. Gordiyenko, E.Y., Nondestructive testing of composite materials of aircraft elements by active thermography, Nauka Innovatsii, 2018, vol. 14, pp. 39–50.
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