The fatigue crack growth characteristics of SiC whisker reinforced cast 6061 aluminum alloy matrix composites were investigated. The samples of MMCs were tempered under three aging conditions. The role of crack closure was also appreciated from a compliance measurement. Furthermore in the higher Δ
K region, the fatigue crack growth characteristics were evaluated employing the experimentally obtained and converted
J-integral value.
Fatigue crack growth resistance including fatigue thresholds for MMCs exceeds that for the unreinforced alloy. However, fatigue crack growth rates of MMCs are remarkably accerelated in the stage IIb, and the d
a/d
N-Δ
K curves of MMCs and unreinforced alloy intersect during the stage IIb. Moreover, MMCs fracture unstably and rapidly at much lower growth rates than the unreinforced alloy in the stage IIc. In all the matrix aging conditions, the underaged MMC exhibits superior fatigue crack growth resistance. This is considered primarily due to crack-closure from the d
a/d
N-Δ
Keff plots which subtract out the influence of crack-closure, and also due to crack tip shielding such as damaged zone, crack deflection and uncracked ligament.
In the stage IIa of MMC, the plastic zone is so small that the stresses ahead of major crack are not su・cient to fracture SiC whiskers. Therefore the crack propagates smoothly in the matrix and when it comes at a whisker, the crack tends to avoid a whisker, thereby promoting whisker pull-out. With increasing Δ
K level, the fracture process zone develops within the plastic zone, so the main crack propagates toward subcracks ahead of crack tip and crack deflection becomes remarkable. Therefore in the stages IIb and IIc the fracture surface becomes rough with increasing Δ
K.
抄録全体を表示