3D Riveting Process Simulation of Laminated Composites


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Laminated composite plates have lower interlaminar strength making it difficult to apply interference-fit rivet joining. In this paper, a three-dimensional finite element model has been developed in order to simulate the riveting process on composite plates. The finite element model is based on continuum elements and accounts for some important mechanisms involved in a whole riveting process. The stresses around the rivet hole and the deformed shapes of the rivet are presented together with the effects of the interference fit and the geometry of the washer when the rivet joints are subjected to the compressive load. The numerical results show the applicability of an interference-fit riveting in composite laminates.



Key Engineering Materials (Volumes 334-335)

Edited by:

J.K. Kim, D.Z. Wo, L.M. Zhou, H.T. Huang, K.T. Lau and M. Wang




S. J. Kim et al., "3D Riveting Process Simulation of Laminated Composites", Key Engineering Materials, Vols. 334-335, pp. 405-408, 2007

Online since:

March 2007




[1] T.N. Chakherloua, J. Vogwellb, Engrg. Failure Anal. 10 (2003) 13-24.

[2] B.L. Bunin, Critical composite joint subcomponents, N87-10975, (1987).

[3] P. Liu, K. Zhang, ACTA Aeronautica et Astronautica Sinica 12 (1991), pp.545-548.

[4] G. Li and G. Shi, Can. Aeronautics Space J., 50(2) (2003), pp.91-105.

[5] E. Markiewicz, B. Langrand, E. Deleotombe, P. Drazetic and L. Patronelli, L., Int. J. Mater. Prod. Technol., 13(3-6) (1998), pp.123-145.

[6] L. Ryan and J. Monaghan, J. Mater. Process. Technol., 103 (2000), pp.36-43.

[7] P. Linde and H. de Boer, Composite Structures, 73 (2006), pp.221-228.

[8] J. Ekh and J. Schon, Compos. Sci. Technol. 66 (2006), pp.875-885.

[9] Z.Q. Cao and M. Cardew-Hall, Aerospace Science and Technology, 10 (2006), pp.327-330. Fig. 6 Effect of clearance between shaft and aperture wall Fig. 7 Effect of washer dimension.