Equivalent wave field transform applied to pulse thermography in carbon composite samples

Author(s):  
Meir Gershenson
2017 ◽  
Vol 112 ◽  
pp. 427-438 ◽  
Author(s):  
Zoubir Acem ◽  
Damien Brissinger ◽  
Anthony Collin ◽  
Gilles Parent ◽  
Pascal Boulet ◽  
...  

2017 ◽  
Vol 2017 (3) ◽  
pp. 107-116
Author(s):  
Rafał Szymański ◽  
Mateusz Zięba

Abstract The paper presents the manufacturing technology and quality control of samples made of composite materials intended, inter alia, for aircraft elements. The samples are made from carbon fiber reinforced prepreg in a polymer matrix which is commonly used in the aerospace industry. The authors described the dimensional requirements for samples made of composite materials for strength testing, and the main stages of production which have a direct impact on the quality of composite samples. Also presented is the technological process of producing flat carbon composite panels for composite samples, cutting the produced panels with a CNC plotter, cutting the samples on a conventional milling machine, and surface treatment of the samples on a surface grinder. The machining parameters that were experientially found to be optimal for the milling and grinding of carbon samples are specified as well. Finally, the method of quality control of the ready composite samples is described and solutions are presented to improve the production of high-quality samples.


2016 ◽  
Vol 821 ◽  
pp. 385-391
Author(s):  
Michal Petrů ◽  
Martina Syrovátková ◽  
Martina Novotná

Composite structures are now increasingly used for their properties in all areas of industrial production where high specific strength is demanded. They gradually replace metal parts and components not only because they are lighter, but above all for their comparable and in many ways even better mechanical properties. Knowledge of behavior of simple synergies between the fibres and the matrix allows the prediction of behavior of complex components and their application in practice. The subject of this article is a description of an experiment and numerical model, that compares the mechanical properties of carbon fiber composite with the values obtained using analytical models. Carbon composite samples were studied in laboratory conditions through Barrier test (ie. Crash test).


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