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Title: Characterization and defect analysis of high temperature aluminum-based metal matrix composites

Miscellaneous ·
OSTI ID:6631154

There is a need for an aluminum-based material to replace titanium in high temperature aerospace applications. Two powder metallurgy (P/M) matrices, RSP Al-8Fe-4Ce and MA Al-9Ti reinforced with 20 volume percent Al2O3 fibers or SiC whiskers or particles were developed for this purpose. Microstructural and mechanical property evaluations of these systems were performed to determine high temperature viability. Elevated temperature tensile tests demonstrated strengths of 14 ksi (98 MPa) at 450 C in the RSP matrix composites reinforced with SiC whiskers; the MA Al-9Ti materials produced tensile strengths of better than 17 ksi (120 MPa) at 500 C. Processing defects contribute significantly to tensile failure at low temperature; Co/SiC defects that result from a sol gel processing step coarsen with exposure to elevated temperature. At elevated temperatures, the failure of all composites was matrix controlled, although some particulate strengthening is evident. A fracture mechanics approach was utilized to determine the plane strain fracture toughness of Al-9Ti/Co/SiC particle reinforced composites; K(sub IC) at room temperature in the as received condition is 4.7 MPa-m(exp 1/2). Fracture toughness increased with annealing at 500 C for 120 and 400 hours. The growth of the intermetallic reaction zone in the Co/SiC particle reinforced materials was found to be parabolic; the rate constants were determined as a function of temperature. Moving boundary theory was applied to determine the interdiffusion coefficient in the intermetallic region as a function of temperature; diffusion is enhanced by a subgrain structure in the reaction zone although a determination of the pre-exponential factor and activation energy for interdiffusion does not show this effect. The pre-exponential interdiffusion coefficient, D(sub 0) is equal to 7.0 x 10(exp 11) sq m/sec and the activation energy for interdiffusion is Q = 99.9 kcal.

Research Organization:
Virginia Univ., Charlottesville, VA (United States)
OSTI ID:
6631154
Resource Relation:
Other Information: Ph.D. Thesis
Country of Publication:
United States
Language:
English