The thermal shock resistance of particulate-filled epoxide composites was studied based on our previously proposed test and evaluation methods. Alumina, silica and CTBN (carboxyl-terminated liquid butadiene-acrylonitrile copolymers) particles were used as fillers.
The thermal shock resistance of alumina-particulate-filled epoxide composites increased with the increase of particulate size, and decreased with the increase of filler contents in the range less than 100phr, while it held almost constant value over the content of 100phr.
The remarkable improvement of the resistance was observed for silica filled composites, even in a higher content region. Fracture surface observed with a SEM showed the difference bonding appearance at particulate/matrix interface corresponding to the different thermal shock resistance between alumina and silica filled composites.
In the case of CTBN filled epoxide composites, the improvement of the thermal shock resistance was clearly recognized.
The critical temperature difference (Δ Tc) at which the crack began to grow from the notch of the specimen was discussed theoretically based on fracture mechanics.
Theoretical and experimental results of K
I*corresponded to Δ Tc agreed well for all the filled composites. However, the effect of internal stress at the interface in highly alumina-filled composites, and the effect of craze formation at the notch tip in CTBN filled composites will also have to be considered.
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