Study on Failure Characteristics of Typical Rivet Connections of C/SiC Composites

Article Preview

Abstract:

The technologic characteristics of typical C/SiC rivet connecting unit by chemical vapor infiltration(CVI) is discussed. It is pointed out that many mechanical limitations caused by connection are the important reasons for the huge gap between the development of C/SiC composite material and the actual thermal structure application. The current situation of preparation and mechanical properties of typical rivet joints on C/SiC composites is summarized. The rational dimension of rivet is given through the test of typical rivet units. Finally, the idea of follow-up research on C/SiC connection by combining analysis with experimental verification is put forward.

You might also be interested in these eBooks

Info:

Periodical:

Materials Science Forum (Volume 1064)

Pages:

9-14

Citation:

Online since:

June 2022

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2022 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] J. Voland RT, Huebner LD, McClinton CR. X-43A Hypersonic Vehicle Technology Development[J]. Acta Astronautica, 2006.59(1-5): 181-191.

DOI: 10.1016/j.actaastro.2006.02.021

Google Scholar

[2] Krenkel W. Carbon Fiber Reinforced CMC for High-Performance Structures[J], International Journal of Applied Ceramic Technology, 2014, 1(2): 188-200.

DOI: 10.1111/j.1744-7402.2004.tb00169.x

Google Scholar

[3] H. Böhrk, U. Beyermann. Secure tightening of a CMC fastener for the heat shield of Re-entry vehicles[J]. Compos. Struct.,92(2010): 107-112.

DOI: 10.1016/j.compstruct.2009.07.002

Google Scholar

[4] Zhang Qiliang, Cao Zengqiang. Study on factors influencing the performance of composite bolted connections[J]. Acta Aeronauticaet Astronautica Sinica, 2012, 33(4): 755-762 (in Chinese).

Google Scholar

[5] Gray PJ, MaCarthy CT. An Analytical Model for the Prediction of Through-thickness Stiffness in Tension-loaded Composite Bolted Joints[J], Composite Structures, 2012, 94(8): 2450-2459.

DOI: 10.1016/j.compstruct.2012.02.011

Google Scholar

[6] Z. Huda, P. Edi. Materials selection in design of structures and engines of supersonic aircrafts: a review[J]. Mater. Des., 46(2014): 552-560.

DOI: 10.1016/j.matdes.2012.10.001

Google Scholar

[7] Zhang Q, Li G. A Review of the Application of C/SiC Composite in Thermal Protection System[J]. Multidiscipline Modeling in Materials and Structures, 2009.5(2): 199-203.

DOI: 10.1163/157361109787959903

Google Scholar

[8] Zhao Libin, Xu Jifeng. Analytical Method for Connecting Structure of Advanced Composite Materials [M]. Beijing: Beihang University Press, 2015(in Chinese).

Google Scholar

[9] Wulz H G. Joining fastening and sealing of hot CMC structures[C]// 33rd Thermophysics Conference, Norfolk, VA, USA: AIAA, 1999: 35-52.

DOI: 10.2514/6.1999-3552

Google Scholar

[10] J.L. Narottam, P. Bansal. Ceramic Matrix Composites: Materials, Modeling and Technology[M]. Canada: John Wiley & Sons, Inc., (2017).

Google Scholar

[11] Zhang Y F, Zhou Z G, Tan Z Y. Experimental and finite element research on the failure mechanism of C/C composite joint structures under out-of-plane loading[J], Materials, 2019, 12(18): 1-16.

DOI: 10.3390/ma12182922

Google Scholar

[12] Li G, WuX, Zhang C, et al. Theoretical simulation and experimental verification of C/SiC joints with pins or bolts[J], Materials and Design,2014, 53(1): 1071-1076.

DOI: 10.1016/j.matdes.2013.08.001

Google Scholar

[13] Li G, Zhang Y, Zhang C, et al. Design, Preparation and Properties of Online-joints of C/SiC-C/SiC with Pins[J]. Composites Part B: Engineering, 2013. 48: 134-139.

DOI: 10.1016/j.compositesb.2012.09.093

Google Scholar

[14] Leone F A, Davila, Carlos G, et al. Progressive damage analysis as a design tool for composite bonded joints [J]. Composites Part B: Engineering, 2015. 77: 474-483.

DOI: 10.1016/j.compositesb.2015.03.046

Google Scholar

[15] Barile C, Casavola C, De Cillis F. Mechanical comparison of new composite materials for aerospace applications[J]. Composites Part B, April 2019. 162: 122-128.

DOI: 10.1016/j.compositesb.2018.10.101

Google Scholar

[16] G. Li, C. Zhang, H. Hu, et al. Preparation and mechanical properies of C/SiC nuts and bolts[J]. Mater. Sci. Eng., 547(2012): 1-5.

Google Scholar

[17] Xuqin Li, Zhiyong Tan, Yi Zhang, et al. Shear bahaviors and failure mechanism of 2D C/SiC pins prepared by chemical vapor infiltration [J]. Ceramics International 46(2020): 16693-16699.

DOI: 10.1016/j.ceramint.2020.03.243

Google Scholar

[18] Tan Zhiyong, Zhang Zhongyuan, Zheng Riheng, et al. The connective technique for a sort of thermal adaptive bolt with split-piece design in vehicle's typical structure[J]. Acta Aeronauticaet Astronautica Sinica, 2020, 41(8): 114062(in Chinese).

Google Scholar

[19] COMAN C D. Numerical analysis for the influence of the geometrical and mechanical parameters on the stiffness and strength of the composite bolted joints[J], INCAS Bulletin, 2018, 10(4): 21-33.

DOI: 10.13111/2066-8201.2018.10.4.3

Google Scholar