Browse > Article
http://dx.doi.org/10.7234/composres.2019.32.1.065

Manufacture of 3D Textile Preform and Study on Mechanical Properties of Composites  

Jo, Kwang-Hoon (Composites Research Division, Korea Institute of Materials Science)
Klapper, Vinzenz (Composites Research Division, Korea Institute of Materials Science)
Kim, Hyeon-Woo (R&D Institute, Songwol Technologies)
Lee, Jeong-Woon (R&D Institute, Songwol Technologies)
Han, Joong-Won (R&D Institute, Songwol Technologies)
Byun, Joon-Hyung (Composites Research Division, Korea Institute of Materials Science)
Joe, Chee-Ryong (School of Mechanical Engineering, Changwon National University)
Publication Information
Composites Research / v.32, no.1, 2019 , pp. 65-70 More about this Journal
Abstract
The aircraft composites wing parts are usually integrated with adhesive or fastener. These laminated composites have weak interlaminar strength, which can lead to delamination. In order to compensate the disadvantages of laminated composites, it is possible to improve the strength, durability, shock and fatigue resistance by reinforcing the fiber in the thickness direction. In addition, using a single structure near-net-shape saves the manufacturing time and the number of fasteners, thus can reduce the overall cost of the composite parts. In this study, compression test, tensile test and open-hole tensile test are carried out for three structural architecture of 3D (three-dimensional) textile preforms: orthogonal(ORT), layer-to-layer(LTL) and through-the-thickness(TTT) patterns. Among these, the orthogonal textile composite shows the highest Young's modulus and strength in tensile and compression. The notch sensitivity of the orthogonal textile composite was the smallest as compared with UD (unidirectional) and 2D (two-dimensional) fabric laminates.
Keywords
3D textile; Delamination; Preform; Mechanical properties;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
연도 인용수 순위
1 Nguyen, V.P., Kerfriden, P., and Boardas, S.P.A., "Two- and Three-dimensional Isogeometric Cohesive Elements for Composite Delamination Analysis," Journal of Composite: Part B, Vol. 60, 2014, pp. 193-212.   DOI
2 Kim, S.J., and Hwang, I.H., "Study on Through the Thickness Stresses in the Corner Radius of a Laminated Composite Structure," Journal of the Korean Society for Aeronautical and Space Sciences, Vol. 41, No. 8, 2013, pp. 665-672.   DOI
3 Byun, J.H., Song, S.W., Lee, C.H., Um M.K., and Hwang B.S., "Impact Properties of Laminated Composites with Stitching with Stitching Fibers," Journal of Composite Structures, Vol. 76, 2006, pp. 21-27.   DOI
4 Visrolia, A., and Meo, M., "Multiscale Damage Modelling of 3D Weave Compsite by Asymptotic Homogenization," Journal of Composite Structures, Vol. 95, 2013, pp. 105-113.   DOI
5 Byun, J.H., Lee, S.K., and Um, M.K., "Fabrication of 3D Textile Preforms by Multi-layer Weaving," Proceedings of Korea Society for Composite Materials, 1997, pp. 212-217.
6 Mouritz, A.P., and Cox, B.N., "A Mechanistic Interpretation of the Comparative in-plane Mechanical Properties of 3D Woven, Stitched and Pinned Composites," Journal of Composites: Part A, Vol. 41, 2010, pp. 709-728.   DOI
7 Dai, S., Cunningham, P.R., Marshall, S., and Silva, C., "Open Hole Quasi-static and Fatigue Characterization of 3D Woven Composites," Journal of Composite Structure, Vol. 131, 2015, pp. 765-774.   DOI
8 A. International, ASTM D5766 Standard Test Method for Open-hole Tensile Strength of Polymer Matrix Composite Laminates, 2018.
9 O'Higgins, R.M., McCarthy, M.A., and McCarthy, C.T., "Comparison of Open Hole Tension Characteristics of High Strength Glass and Carbon Fibre-reinforced Composite Materials," Journal of Composites Science and Technology, Vol. 68, 2008, pp. 2770-2778.   DOI
10 Arief Yudhanto, Naoyuki Watanabe, Yukata Iwahori, and Hikaru Hoshi, "The Effects of Stitch Orientation on the Tensile and Open Hole Tension Properties of Carbon/epoxy Plain Weave Laminates," Journal of Material and Design, Vol. 35, 2012, pp. 563-571.   DOI