The Influence of Processing Parameters on the Void Content and Compressive Strength of Carbon Fibre-Epoxy Laminates

Article Preview

Abstract:

This research addresses the influence of various processing parameters on the post cure quality of carbon fibre composites. Four processing parameters were investigated in the study, in terms of their impact on void content and overall compressive strength. The first parameter distinguishes between laminates cured in a vacuum oven and those cured in an autoclave under high positive pressure. The second parameter describes the impact on voids of differing fibre architectures, comparing a unidirectional fibre structure to that of woven cloth. Thirdly, the influence of compaction during manufacture is analysed and lastly, variation in cure temperature was tested to determine its effect on final laminate quality. The quality of the cured laminate samples was assessed from visual inspection, and in terms of compressive strength and void fraction calculated by Micro-CT X-ray Tomography. The results show that autoclave-cured samples feature significant quality improvements in terms of void fraction and compressive strength when compared to oven-cured samples. Unidirectional laminates incur higher sensitivity to void inclusion than cloth laminates due to the influence of fibre wrinkling. Compaction has no effect on laminate strength; it does however reduce variability in certain cases. Temperature affects different fibre structures in different ways, these being highly dependent on curing method. Finally, it was discerned that curing by autoclave was the dominant processing parameter. Thus, regardless of other manufacturing techniques, the autoclave samples featured almost zero voids and were consequently of the highest quality.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

243-246

Citation:

Online since:

July 2011

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2011 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Kelly, A. and C. Zweben Comprehensive Composite Materials - Test Methods, Nondestructive Evaluation, and Smart Materials. Oxford, Elsevier Science Ltd (2000).

Google Scholar

[2] Brookes, R.E., Kirkman, D.J. DTA Technical Note - Factors affecting void content and compressive strength of carbon epoxy structures, Defence Technology Agency, New Zealand, 3/(2009).

Google Scholar

[3] Rubin, A.M., Jerina, K.L. Evaluation of porosity in composite aircraft structures, Mechanics of Composite Materials, volume 30, No. 6, 1994. (1994).

Google Scholar

[4] Liu, L., Zhang, B., Wang, D., Wu, Z. Effects of Cure Cycles on Void Content and Mechanical Properties on Composite Laminates., Composite Structures 73(3): 303-309. (2006).

DOI: 10.1016/j.compstruct.2005.02.001

Google Scholar

[5] Oliver, P., Cottu, J. P. and Ferret, B. Effects of Cure Cycle Pressure and Voids on some Mechanical Properties of Carbon/epoxy Laminates., Composites 30(6): 505-515. (1994).

DOI: 10.1016/0010-4361(95)96808-j

Google Scholar

[6] Ghiorse, R. A Comparison of Void Measurement Methods for Carbon/Epoxy Composites. Army Lab Command, (Material Technology Lab, Watertown MA). (1991).

Google Scholar

[7] Sturgess, D. Analysis of Void Content in CFRC's by Non-Destructive Micro-CT. Part IV project report, 2008-CM31 (2008).

Google Scholar