Experimental study on interfacial adhesive properties between twisted z-pin and laminates

被引:10
作者
Wang, Xiao-Xu [1 ]
Chen, Li [1 ]
Jiao, Ya-Nan [1 ]
Li, Jia-Lu [1 ]
机构
[1] Key Laboratory of Advanced Textile Composite Materials Ministry of Education, Institute of Composites, Tianjin Polytechnic University, Tianjin
来源
Guti Huojian Jishu/Journal of Solid Rocket Technology | 2014年 / 37卷 / 06期
关键词
Interfacial adhesive property; Laminate composite; Pull-out test; Twisting; Z-pin;
D O I
10.7673/j.issn.1006-2793.2014.06.022
中图分类号
O63 [高分子化学(高聚物)]; TQ31 [高分子化合物工业(高聚物工业)];
学科分类号
070305 ; 0805 ; 080501 ; 080502 ; 081704 ;
摘要
Five types of twisted z-pins(the twist degree are 1, 2, 2.5, 3 and 4 n/cm respectively) were prepared by means of draw forming from small-cavity mold and twisting before resin curing. Appearances of various twisted z-pins were observed, and the tensile properties of various twisted z-pins were tested. The interfacial adhesive properties between z-pins and laminates were characterized through single z-pin pull-out tests. The results show that twisting makes the stems of the z-pins distorted, the more twist degree is, the more distortion is. Twisting makes the tensile strength and the elongation reduce by about 50%, and the tensile modulus decreases by 30%. However, twisting improves the interfacial adhesive properties between z-pins and laminates significantly. The more the twist degree is, the higher the interfacial sheer strength τd, the maximum frictional force Ff, and the pull-out energy Wp are. With the increase of twist degree, the debonding location shifts from the F-R meso-interface between its fiber and resin of z-pin to the R-R meso-interface between the outer resin of z-pin and the resin of laminates. For the z-pin with twist degree of 3 n/cm, the τd is improved by 61%, Ff and Wp are all tripled. ©, 2014, Journal of Solid Rocket Technology. All right reserved.
引用
收藏
页码:856 / 862
页数:6
相关论文
共 15 条
[1]  
Mouritz A.P., Review of z-pinned composites laminates, Composites A, 38, 12, pp. 2383-2397, (2007)
[2]  
Freitas G., Fusco T., Campbell T., Et al., Z-Fibre technology and products for enhancing composite design, Proceedings of the 83rd Meeting of the AGARD SMP Conference on Bolted/bonded Joints in Polymeric Composites, (1996)
[3]  
Marasco A.I., Analysis and evaluation of mechanical performance of reinforced sandwich structures: X-CorTM and K-CorTM, (2005)
[4]  
Park Y.B., Lee B.H., Kweon J.H., Et al., The strength of composite bonded T-joints transversely reinforced by carbon pins, Composites Stuctures, 94, 2, pp. 625-634, (2012)
[5]  
Freitas G., Magee C., Dardzinski P., Et al., Fiber insertion process for improved damage tolerance in aircraft laminates, Journal of Advanced Material, 25, 4, pp. 36-43, (1994)
[6]  
Partridge I.K., Cartie D.D.R., Bonnington T., Manufacture and performance of z-pinned composites, Advanced Polymeric Composites, pp. 103-139, (2003)
[7]  
Partridge I.K., Cartie D.D.R., Delamination resistant laminates by Z-Fiber pinning: Part I manufacture and fracture performance, Composites: Part A, 36, 1, pp. 55-64, (2005)
[8]  
Cartie D.D.R., Troulis M., Partridge I.K., Delamination of Z-pinned carbon fibre reinforced laminates, Composites Science and Technology, 66, pp. 855-861, (2006)
[9]  
Liu H.Y., Yan W.Y., Yu X.Y., Experimental study on z-pinned DCB mode I delamination, Proceedings of the International Conference on Structural Integrity and Fracture, pp. 229-234, (2004)
[10]  
Chang P., Mouritz A.P., Cox B.N., Properties and failure mechanisms of pinned composite lap joints in monotonic and cyclic tension, Composites Science and Technology, 66, 13, pp. 2163-2176, (2006)