FRICTION AND ABRASION RESISTANCE OF CAST-ALUMINUM ALLOY FLY-ASH COMPOSITES

The abrasive wear properties of-stir-cast A356 aluminum alloy-5 vol pc t fly ash composite were tested against hard SiCp abrasive paper and c ompared to those of the A356 base alloy. The results indicate that the abrasive wear resistance of aluminum-fly ash composite is similar to that of aluminum-alumina fiber composite and is superior to that of th e matrix alloy for low loads up to 8 N (transition load) on a pin. At loads greater than 8 N, the wear resistance of aluminum-fly ash compos ite is reduced by debonding and fracture of fly ash particles. Microsc opic examination of the worn surfaces, wear debris, and subsurface sho ws that the base alloy wears primarily by microcutting, but the compos ite wears by microcutting and delamination caused by crack propagation below the rubbing surface through interfaces between fly ash and sili con particles and the matrix. The decreasing specific wear rates and f riction during abrasion wear with increasing load have been attributed to the accumulation of wear debris in the spaces between the abrading particles, resulting in reduced effective depth of penetration and ev entually changing the mechanism from two-body to three-body wear, whic h is further indicated by the magnitude of wear coefficient.