Experimental Research on the Mechanical Behavior of the Cracked Aluminum Plate Bonded by the Graphite/Epoxy Composite Patch

Author:

Zhang Yi Shan1,Wang Zun1,Wang Zhi1

Affiliation:

1. Beijing Aeronautical Technology Research Center

Abstract

The effect of the graphite/epoxy composite patch parameters on the static and fatigue strength of the cracked aluminum plate was investigated experimentally. A series of specimens repaired by six types of composite patches including four different patch lengths and two different patch thicknesses were tested on the material tester. Specimens single-sided repaired and double-sided repaired by the same composite patches were also tested. The experiment results show that composite patches can provide an improvement in static and fatigue strength of the cracked aluminum plate, double-sided repair is more effective than single-sided repair, if the thickness and the length were selected properly, the composite patches can significantly enhance the strength of the repaired specimens.

Publisher

Trans Tech Publications, Ltd.

Subject

General Engineering

Reference5 articles.

1. A.A. Baker: Compos. Struct. Vol. 2 (1984), p.153.

2. A.A. Baker: Journal of Composites Vol. 9 (1987), p.297.

3. A. Kerr and J. Ruddy: Applied Composite Materials Vol. 6 (1999), p.239.

4. S.J. Chen: Aeronautic Engineering and Maintenance Vol. 1 (2000), p.21 (In Chinese).

5. Z. Wang, J.Y. Xiao and D.Z. Jiang: Journal of Reinforced Plastics and Composites Vol. 28 (2009), p.587.

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