A Pre-Stitching Method to Manufacture Z-Pins Reinforced Woven Ceramic Matrix Composite Laminates

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Z-pins reinforced 2D ceramic matrix composites (CMCs), integratedly designed new materials, are developed to enhance 2D CMCs through-thickness in the form of Z-pins and to ensure significant increase in interlaminar fracture toughness, delamination resistance and impact resistance, and Z-pins reinforced 2D CMCs have much application. A manual pre-stitching method is developed to make holes in the graphite fixture to control Z-pins row spacings and to introduce yarns of 3000 T300 carbon fibers bundle into a preform. Z-pins reinforced woven CMCs for research were manufactured successfully by repeatedly using chemical vapor infiltration (CVI) to infiltrate SiC matrix into woven preform and carbon fiber sutures. It is shown that this method of manufactured Z-pins reinforced woven CMC is feasible.

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117-120

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July 2013

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© 2013 Trans Tech Publications Ltd. All Rights Reserved

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[1] J. E. Master, et al. Impact Fracture and Failure Suppression Using Interleaved Composites. SAMPE Quarterly. 17 (1985) 46-49.

Google Scholar

[2] Jiao Guiqiong, Ning Rongchang, et al. A Study on Interleaved Composites (In Chinese). Aerospace Materials & Technology. 4 (2001) 36-39.

Google Scholar

[3] S Zang, M A Hoisington, and J C Seferis. Particulate Interlayer Toughening of Dicyanate Matrix Composites. Polymer Composites. 14 (1993) 458-466.

DOI: 10.1002/pc.750140603

Google Scholar

[4] Gao Feng, Jiao Guiqiong, et al. Mode II Fracture Toughness of Thermoplastic-Particle Interlayered Composite Laminate (In Chinese). Journal of Northwestern Polytechnical University. 23 (2005) 184-188.

Google Scholar

[5] M. B. Dow, H. B. Dexter. Development of Stitched, Braided and Woven Composite Structures in the ACT Program and at Langley Research Center (1985 to 1997). NASA/TP-97-206234.

Google Scholar

[6] Cheng Xiaoquan, A Al-Mansour, et al. Compression Strength of Stitched Laminates After Low Velocity Impact. Journal of Reinforced Plastics and Composites. 24 (2005) 935-947.

DOI: 10.1177/0731684405048193

Google Scholar

[7] R. Velmurugan, S. Solaimurugan. Improvements in Mode I Interlaminar Fracture Toughness and In-plane Mechanical Properties of Stitched Glass/Polyester Composites. Composites Science and Technology. 67 (2007) 61-69.

DOI: 10.1016/j.compscitech.2006.03.032

Google Scholar

[8] G. Freitas, C. Magee, et al. Fiber Insertion Process for Improved Damage Tolerance in Aircraft Laminates. Journal Advanced Materials. 25 (1994) 36-43.

Google Scholar

[9] I. K. Partridge, D. D. R. Cartié. Delamination Resistant Laminates by Z-fiber Pinning I: Manufacture and Fracture Performance. Composites Part A. 36 (2005) 55-64.

DOI: 10.1016/s1359-835x(04)00180-0

Google Scholar

[10] Wenyi Yan, Hong-Yuan Liu, Yiu-Wing Mai. Numerical Study on the Mode I Delamination Toughness of Z-pinned Laminates. Composites Science and Technology. 63 (2003) 1481-1493.

DOI: 10.1016/s0266-3538(03)00167-2

Google Scholar

[11] Wenyi Yan, Hong-Yuan Liu, Y-W Mai. Mode II Delamination Toughness of Z-pinned Laminates. Composites Science and Technology. 64 (2004) 1937-1945.

DOI: 10.1016/j.compscitech.2004.02.008

Google Scholar

[12] A.P. Mouritz. Review of Z-pinned Composite Laminates. Composites: Part A. 38 (2007) 2383–2397.

DOI: 10.1016/j.compositesa.2007.08.016

Google Scholar