Abstract

Abstract Preparation, microstructures and deformation behavior of 12 vol.% SiC P /6066Al composites fabricated by a powder metallurgy (PM) route have been systemically reported in this paper. The experimental results indicated that SiC particles were distributed homogeneously in the aluminum matrix, and that the constituents of the matrix were Al, needle-shaped β′-Mg 2 Si phases and a small amount of dispersoids (Fe, Mn, Cu) 3 Si 2 Al 15 (BCC structure with lattice parameter a ≈ 12.8 A). A well-bonded SiC/Al interface consisting of a thin and clean layer of polycrystalline structure of metal matrix with segregation of Mg element has been observed. The SiC particle cracking and the ductile-tearing of SiC/Al interfaces caused the rupture of the composites. The experimental data coincided well with the theoretical results predicted by an extended effective model assumption (EMA). The current study indicates that load transfer between the matrix and reinforcements, grain refinement of metal matrix, and dislocation strengthening are the main strengthening mechanisms of SiC P /Al composites. The ductile-tearing of SiC P /Al interfaces and the SiC particle cracking are the dominating failure modes and the deformation behavior of SiC P /Al composites strongly depends on the properties of matrix alloy.

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