The Fabrication and Microstructure Analysis of Carbon Fiber Composites with Interlaminar Reinforcement

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This paper adopts a flow-punched technology for laminated composite which combines jet-flow and carbon fiber piercing technology. The jet-flow-based preform forming experiment system is constructed, and jet flow technology is used to prepare the interlaminar reinforced carbon fiber composite materials. The reinforced carbon fiber bundle is shot into the microstructure of the laminated composite in all directions and laminated carbon fiber becomes an entire, and then it is treated by vacuum and curing process. This paper provides a technological approach to improve the quality of the laminated composite preform.

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59-63

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November 2016

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© 2017 Trans Tech Publications Ltd. All Rights Reserved

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[1] J. J. Liu, T. H. Li, Study on fiber and damage of composite fabric made by needle punched carbon cloth and web, J. Carbon Techniques. 27(5) (2008)13-15.

Google Scholar

[2] A. Lacombe, 3D Novoltex and Naxeco Caron—Carbon Nozzle Extensions: matured, industrials and Available technologies to reduce programmatic and technical risks and to increase performance of 1auncher upper stage engines, Aiaa/asme/sae/asee Joint Propulsion Conference & Exhibit. (2008).

DOI: 10.2514/6.2008-5236

Google Scholar

[3] R. Zheng. R.L. Ji, Progress in studies on the technology of preparing preform of carbon composite by needle punched, J. Carbon, 01(2011) 33-37.

Google Scholar

[4] S. L. Wang, S. Lei and J. Zhou, Mathematical model for determination of strand twist angle and diameter in stranded wire helical springs, Journal of Mechanical Science and Technology, 24 (6) (2010) 1203-1210.

DOI: 10.1007/s12206-010-0333-4

Google Scholar

[5] Z. M. Qiu, Solid rocket motor material and craft, Aerospace publishing house, Beijing, (1995).

Google Scholar

[6] E. Fitzer, L. M. Manocha, Carbon Reinforcements and Carbon/Carbon composites, April (1998).

DOI: 10.1007/978-3-642-58745-0

Google Scholar

[7] M. Montaudon, Novoltex textures for thermostructural materials, Joint Propulsion Conference, (1991).

DOI: 10.2514/6.1991-1848

Google Scholar

[8] M. J. Evans, R. Fisher and K. A. Williams, Ultra-high performance carbon composites, USP 5503893 (1996).

Google Scholar

[9] P. W. Sheehan and R. S. Liew. Process for forming fibrous structures with predetermined Z-fiber distributions, USP 6237203 (2001).

Google Scholar

[10] W. D. Thompson, T.W. Sundburg and D.R. Snyder. Apparatus and technique for making carbon brake discs, USP 6083436 (2000).

Google Scholar

[11] X. Xiong, B.Y. Huang, Investigation of braking properties of carbon-carbon composites [D]. Central South University, 2004. 6.

Google Scholar

[12] H. M. Huang, Thermo chemical ablation of spherical cone during re-entry. J. Journal of Harbin Institute of Technology, 18(1) (2001)18—22.

Google Scholar

[13] A. L. Ji, H. J. Li, The development and application of needle preform. J. Carbon techniques, 12(3) (2010) 23-27.

Google Scholar

[14] J. J. Liu, T. H. Li, Z. B. Zhao, et al, Investigation on structure and thermal properties of C/C compo site reinforced by needle punching composite fabric, J, Journal of Solid Rocket Technology, 29(1) (2006) 60-62.

Google Scholar