Kt. Park et Fa. Mohamed, CREEP STRENGTHENING IN A DISCONTINUOUS SIC-AL COMPOSITE, Metallurgical and materials transactions. A, Physical metallurgy andmaterials science, 26(12), 1995, pp. 3119-3129
High-temperature strengthening mechanisms in discontinuous metal matri
x composites were examined by performing a close comparison between th
e creep behavior of 30 vol pet SiC-6061 Al and that of its matrix allo
y, 6061 Al. Both materials were prepared by powder metallurgy techniqu
es. The experimental data show that the creep behavior of the composit
e is similar to that of the alloy in regard to the high apparent stres
s exponent and its variation with the applied stress and the strong te
mperature dependence of creep rate. By contrast, the data reveal that
there are two main differences in creep behavior between the composite
and the alloy: the creep rates of the composite are more than one ord
er of magnitude slower than those of the alloy, and the activation ene
rgy for creep in the composite is higher than that in the alloy. Analy
sis of the experimental data indicates that these similarities and dif
ferences in creep behavior can be explained in terms of two independen
t strengthening processes that are related to (a) the existence of a t
emperature-dependent threshold stress for creep, tau(0), in both mater
ials and (b) the occurrence of temperature dependent load transfer fro
m the creeping matrix (6061 Al) to the reinforcement (SiC). This findi
ng is illustrated by two results. First, the high apparent activation
energies for creep in the composite are corrected to a value near the
true activation energy for creep in the unreinforced alloy (160 kJ/mol
e) by considering the temperature dependence of the shear modulus, the
threshold stress, and the load transfer. Second, the normalized creep
data of the composite fall very close to those of the alloy when the
contribution of load transfer to composite strengthening is incorporat
ed in a creep power law in which the applied stress is replaced by the
effective stress, the stress exponent, n, equals 5, and the true acti
vation energy for creep in the composite, Q(c), is equal to that in th
e alloy.