Title of article
Consolidation effects on tensile properties of an elemental Al matrix composite
Author/Authors
Tang، نويسنده , , F. and Meeks، نويسنده , , H. and Spowart، نويسنده , , J.E. and Gnaeupel-Herold، نويسنده , , T. and Prask، نويسنده , , H. and Anderson، نويسنده , , I.E.، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2004
Pages
11
From page
194
To page
204
Abstract
In a simplified composite design, an unalloyed Al matrix was reinforced by spherical Al–Cu–Fe alloy particles (30 vol.%), using either commercial purity (99.7%) or high purity (99.99%) fine powders (diameter < 10 μm). This composite material was consolidated by either vacuum hot pressing (VHP) or quasi-isostatic forging. The spatial distribution of reinforcement particles in both VHP and forged samples was shown to be almost the same by quantitative characterization with a multi-scale area fraction analysis technique. The tensile properties of all composite samples were tested and the forged materials showed significantly higher strength, while the elastic modulus values of all composite materials were close to the upper bound of theoretical predictions. Neutron diffraction measurements showed that there were high compressive residual stresses in the Al matrix of the forged samples and relatively low Al matrix residual stresses (predominantly compressive) in the VHP samples. By tensile tests and neutron diffraction measurements of the forged samples after annealing, it was shown that the high compressive residual stresses in the Al matrix were relieved and that tensile strength was also reduced to almost the same level as that of the VHP samples. Therefore, it was deduced that increased compressive residual stresses and enhanced dislocation densities in the forged composites raised the tensile strength to higher values than those of the VHP composites.
Keywords
Metal Matrix composites , Residual stress , Powder metallurgy , strengthening mechanism
Journal title
MATERIALS SCIENCE & ENGINEERING: A
Serial Year
2004
Journal title
MATERIALS SCIENCE & ENGINEERING: A
Record number
2144730
Link To Document