MaterialsScience and Engineering, A 107 (1989) 63-69 63
The Influence of Hydrostatic Pressure on the Ductility of AI-SiC
Composites*
A. K VASUDEVANand O. RICHMOND
Alcoa Research ('entre, Pitt~sbur~h (U.S.A.)
F.ZOK and J. D. EMBURY
McMaster University, Hamilton (Canada)
(ReceivedJune 1, 1988)
Abstract
Tensile tests with superimposed hydrostatic
pressures were performed on two types of metal
matrix composite." 2014 Al with 20% SiC particles
and 2124 Al with 14% SiC whiskers. In the mater-
ials with SiC particulate, the ductility increases
rapidly with pressure and the mode of damage
initiation is by particle fracture. Materials contain-
ing SiC whiskers exhibit a different fracture mode
involving whisker matrix decohesion, and strain
localization which results in shear fracture.
1. Introduction
The mechanical response of metal-matrix
composites can be considered in terms of various
microstructural features, such as the par-
ticle-matrix interfaces and the work hardening
characteristics of the matrix, and the process of
damage accumulation which precedes fracture.
Much of the work in the present conference
relates to the detailed characterization of inter-
facial structures and their role in the process of
load transfer in metal-matrix composites. The
present paper explores the pressure dependence
of flow and fracture in both particulate- and
whisker-reinforced Al-matrix composites. The
results suggest that a combination of studies of
the mechanical response under superimposed
pressure, detailed metallographic and fracto-
graphic studies, and micromechanical analyses
can yield information which is complementary to
the detailed structural studies of interfaces. The
*Paper presented at the symposium on Interfacial Phe-
nomena in Composites: Processing, Characterization, and
MechanicalProperties,Newport, RI, June 1-3, 1988.
work serves to delineate some of the critical
damage processes which limit the ductility of
metal-matrix composites.
2. Materials and experimental procedures
Mechanical tests were performed on two types
of SiC-reinforced Al-matrix composites and
compared with the results of tests performed on
the matrix materials without the reinforcing
phase.
One composite was a commercial 2014 AI
alloy containing 20% SiC particles. This material
was heat treated to the T6 condition (Fig. l(a)).
The average particle size was 13 /zm and the
average aspect ratio was 1.23 measured in the
plane containing the tensile axis. Approximately
5% of the SiC particles were greater than 40/zm
in size and had aspect ratios of the order of 4.
The second material was a 2124 A1 alloy con-
taining 14% SiC whiskers which were 1 /~m in
diameter and 5 to 10 /~m in length (Fig. l(b)).
Two ageing treatments were undertaken in order
to examine the influence of precipitates located at
the SiC-matrix interfaces on the ductility of the
composite. The ageing times were selected to
maintain constant matrix strength (as determined
from microhardness measurements) as shown in
Fig. 2. Transmission electron microscopy (TEM)
observations indicated many more intermetallic
compounds precipitated at the interfaces in the
overaged condition than in the underaged
condition.
Tensile tests were conducted in a Harwood
pressure unit with superimposed pressures up to
1000 MPa. The tensile samples had a gauge
length of 15.2 mm and a gauge diameter of 3.2
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