Experimental Study on Mechanical Properties of X-Cor Sandwich

Article Preview

Abstract:

In this study, by changing Z-pin’s insertion parameters, the X-cor sandwich was prepared with vacuum curing molding process. The effects of Z-pin’s insertion angle, insertion density and diameter on compression, shear and tension properties were studied. The results show that Z-pin’s insertion parameters can significantly affect the mechanical properties of X-cor sandwich. The compression properties of X-cor sandwich are reduced, while shear properties are improved by the increase of Z-pin’s insertion angle. As Z-pin’s insertion angle increases the tension modulus increases while the tension strength firstly increases and secondly decreases. The mechanical properties increase with the increase of Z-pin’s insertion density and diameter. Compared with the foam core sandwich, the mechanical properties of X-cor sandwich are significantly improved in both modulus and strength.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

411-418

Citation:

Online since:

June 2011

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2011 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Li Shunlin, Wang Xingye. Design basics of the composites structures. Wuhan: Wuhan university of technology press, (1993).

Google Scholar

[2] Wo Dingzhu. Complete book of the composites. Beijing: Chemical industry press, 2000: 260-268.

Google Scholar

[3] Freitas G. Z-fiberTM technology and products for enhancing composite design. In: 83rd Meeting of AGARD SMP, Florence: AGARD, (1996).

Google Scholar

[4] Huang Tao, Jiao Guiqiong, Xu Tingting. Research development and application of Z-reinforcement foam core sandwich. Fiber composites, 2005, (3): 19-23.

Google Scholar

[5] Dang Xudan, Xiao Jun, Liyong. Progress of experimental study on mechanical properties of X-cor sandwich structure. Materials engineering, 2008, (6): 76-80.

Google Scholar

[6] Tan Yonggang, Xiao Jun, Li Yong, Yuan Yonghu. Shear property of X-cor sandwich structure. Aerospace materials and technology, 2008, (5): 75-77.

Google Scholar

[7] Sun Xiannian, Zheng Changliang. Advances on modeling through-the-thickness reinforcement of laminated composite by Z-pinning. Acta aeronautica et astronautica sinica, 2006, 27(7): 1194-1202.

Google Scholar

[8] Kay B F. RWSTD airframe technology foundation for the 21st century. In: American Helicopter Society 57th Annual Forum, Washington: American Helicopter Society, (2001).

Google Scholar

[9] Marasco A I, Cartie Denis D R, Partridge I K, et al. Mechanical properties balance in novel Z-pinned sandwich panels: Out-of-plane properties. Composites Part A: Applied Science and Manufacturing, 2006, 37: 295-302.

DOI: 10.1016/j.compositesa.2005.03.029

Google Scholar

[10] Partridge I K, Cartie D D R, Bonnington T. Manufacture and performance of Z-pinned composites. In: ADVANIS, SHONAIKE G, Editors, Advanced Polymeric Materials. USA Florida Boca Raton: CRC Press, 2003, 103-138.

DOI: 10.1201/9780203492901.ch3

Google Scholar

[11] O'brien T K, Paris Isabell. Exploratory investigation of failure mechanisms in transition regions between solid laminates and X-cor truss sandwich. Composite Structures, 2002, 57: 189-204.

DOI: 10.1016/s0263-8223(02)00083-1

Google Scholar

[12] Cartie Denis D, Fleck Norman A. The effect of pin reinforcement upon the through-thickness compressive strength of foam-cored sandwich panels. Composites Science and Technology, 2003, 63: 2401-2409.

DOI: 10.1016/s0266-3538(03)00273-2

Google Scholar

[13] Tian Xu, Xiao Jun, Li Yong. Study on X-cor sandwich structure manufacture and its mechanical performance. Aircraft design, 2004, (3): 22-25.

Google Scholar

[14] Du Long, Jiao Guiqiong, Huang Tao. Shear stiffness prediction of X-shape Z-pinned sandwich structures. Acta mechanica solida sinica, 2007, 28(4): 369-374.

Google Scholar

[15] Du Long, Jiao Guiqiong, Huang Tao, etc. Shear properties of X-Z-pin reinforced foam core sandwich. Acta materiae compositae sinica, 2007, 24(6): 140-146.

Google Scholar

[16] Du Long. A study on mechanical properties of X-cor sandwich. Xi'an: Northwestern polytechnical university, (2007).

Google Scholar

[17] Du Long, Jiao Guiqiong, Huang Tao. Through-thickness compression properties of Z-pin reinforced foam core sandwich. Journal of aeronautical materials, 2008, 28(4): 101-106.

DOI: 10.1177/0021998308099223

Google Scholar

[18] Hao Jijun, Zhang Zuoguang, Zhang Lei, etc. Effects of Z-pin inserting parameters on X-cor sandwich mechanical property. Acta aeronautica et astronautica sinica, 2008, 29(3): 763-768.

Google Scholar

[19] Hao Jijun, Zhang Zuoguang, Limin, etc. Compression property analysis of X-cor sandwich composites. Acta aeronautica et astronautica sinica, 2008, 29(4): 1079-1083.

Google Scholar

[20] Dang Xudan, Tan Yonggang, Xiao Jun, etc. Finite element modeling analysis of compressive modulus about X-cor sandwich. Material engineering, 2009, (1): 50-54.

Google Scholar

[21] Huang Tao, Jiao Guiqiong, Du Long. Experimental study on X-cor reinforced foam core sandwich. Acta aeronautica et astronautica sinica, 2008, 29(6): 1542-1549.

Google Scholar

[22] Li Yong, Xiao Jun, Tan Yonggang, etc. Study on compressive properties of X-cor sandwich structures. Acta aeronautica et astronautica sinica, 2009, 30(3): 557-561.

Google Scholar

[23] Secretariat of fiber reinforced plastics standardization technology committee. Standards collection of the fiber reinforced plastics(FRP). Beijing: China standards press, 1998: 349-549.

Google Scholar